proyecto f.32065 ” ingenierÍa bÁsica y de detalle … · con el propósito de determinar su...

INSTITUTO MEXICANO DEL PETRÓLEO

DELEGACIÓN REGIONAL ZONA MARINA

PROYECTO : F.32065 PLATAFORMA: SEA PONY KAB-101 FECHA: Marzo/2005.

AV-F.32065-1815-31-MC-REV.0 MEMORIA RU

AV. PERIFERICA NORTE # 75 ESQ. CON CALLE 35 B COL. SAN AGUSTIN DEL PALMAR, C. P. 24118, CD. DEL CARMEN, CAMP. TELMEX (01938) 120-49 MICRO 293-49. FAX: (01938) 120-42 MICRO 293-

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PROYECTO F.32065

” INGENIERÍA BÁSICA Y DE DETALLE POR LA ADICIÓN DE 2 POZOS EN LA PLATAFORMA SEA PONY KAB-101 Y ASISTENCIA TÉCNICA EN REVISIÓN DE INGENIERÍAS

REALIZADAS POR OTRAS COMPAÑÍAS”

3.- MEMORIA DE CÁLCULO DE LA EVALUACIÓN BAJO CONDICIONES DE RESISTENCIA ÚLTIMA

POR OLEAJE






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3.183

ÍNDICE

PÁGINA 3.1. INTRODUCCIÓN ..................................................................................................................................................184 3.2. OBJETIVO ..............................................................................................................................................................184 3.3. ALCANCE...............................................................................................................................................................184 3.4. DATOS DE LA ESTRUCTURA ...........................................................................................................................184 3.5. BASES DE ANÁLISIS ...........................................................................................................................................184 3.6.- JUSTIFICACIÓN DEL ANÁLISIS Y CONSIDERACIONES ESPECÍFICAS .............................................184 3.7. MODELO ESTRUCTURAL .................................................................................................................................184 3.8.- CARGAS CONSIDERADAS ...............................................................................................................................184

3.8.1.- CARGAS GRAVITACIONALES ...................................................................................................................184 3.8.1.2.- Carga muerta..............................................................................................................................................184 3.8.1.3.- Carga viva..................................................................................................................................................184 3.8.1.4.- Carga de equipo .........................................................................................................................................184 3.8.1.5.- Peso del Helicóptero ..................................................................................................................................184 3.8.1.6.- Resumen de cargas gravitacionales ...........................................................................................................184

3.8.2.- CARGAS AMBIENTALES.............................................................................................................................184 3.8.2.1.- Parámetros para la obtención de fuerzas de oleaje, corriente y viento ......................................................184 3.8.2.2.- Fuerzas de oleaje sobre la cubierta ............................................................................................................184 3.8.2.3.- Fuerzas de viento .......................................................................................................................................184

3.9.- ANÁLISIS ESTRUCTURAL ...............................................................................................................................184 3.10.- RESULTADOS DEL ANÁLISIS .......................................................................................................................184

3.10.1.- MECANISMO DE COLAPSO PARA 0° ......................................................................................................184 3.10.2.- MECANISMO DE COLAPSO PARA 30° ....................................................................................................184 3.10.3.- MECANISMO DE COLAPSO PARA 68° ....................................................................................................184 3.10.4.- MECANISMO DE COLAPSO PARA 90° ....................................................................................................184 3.10.5.- MECANISMO DE COLAPSO PARA 120° ..................................................................................................184 3.10.6.- MECANISMO DE COLAPSO PARA 150° ..................................................................................................184 3.10.7.- MECANISMO DE COLAPSO PARA 180° ..................................................................................................184 3.10.8.- MECANISMO DE COLAPSO PARA 210° ..................................................................................................184 3.10.9.- MECANISMO DE COLAPSO PARA 240° ..................................................................................................184 3.10.10.- MECANISMO DE COLAPSO PARA 270° ................................................................................................184 3.10.11.- MECANISMO DE COLAPSO PARA 292° ................................................................................................184 3.10.12.- MECANISMO DE COLAPSO PARA 330° ................................................................................................184 3.10.13.- RESUMEN DEL RSR PARA ANÁLISIS DE RU ......................................................................................184

3.11.- REVISIÓN DE LA CONEXIÓN PIERNA - CEMENTANTE - PILOTE .....................................................184 3.12.- CONCLUSIONES ...............................................................................................................................................184 3.13.- ANEXOS ..............................................................................................................................................................184

3.13.1.- Archivo de entrada para análisis de resistencia última dirección 0°..............................................................184 3.13.2.- Archivo de entrada para calcular el mecanismo de colapso dirección 0°.......................................................184 3.13.3.- Archivo de entrada para calcular el mecanismo de colapso dirección 30°.....................................................184 3.13.4.- Archivo de entrada para calcular el mecanismo de colapso dirección 68°.....................................................184 3.13.5.- Archivo de entrada para calcular el mecanismo de colapso dirección 90°.....................................................184 3.13.6.- Archivo de entrada para calcular el mecanismo de colapso dirección 120°...................................................184 3.13.7.- Archivo de entrada para calcular el mecanismo de colapso dirección 150°...................................................184 3.13.8.- Archivo de entrada para calcular el mecanismo de colapso dirección 180°...................................................184 3.13.9.- Archivo de entrada para calcular el mecanismo de colapso dirección 210°...................................................184 3.13.10.- Archivo de entrada para calcular el mecanismo de colapso dirección 240°.................................................184 3.13.11.- Archivo de entrada para calcular el mecanismo de colapso dirección 270°.................................................184






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3.13.12.- Archivo de entrada para calcular el mecanismo de colapso dirección 292°.................................................184 3.13.13.- Archivo de entrada para calcular el mecanismo de colapso dirección 330°.................................................184

3.14.- ARCHIVO DE RESULTADOS, DIRECCIÓN 0° ...........................................................................................184 3.14.1.- Listado de colapso (CLPLIST).......................................................................................................................184 3.14.2.- Historial de carga y de deformaciones (CLPLOG) ........................................................................................184 3.14.3.-Reportes obtenidos directamente del Collvue .................................................................................................184

3.14.3.1.-Joint Displacement Report (Desplazamientos en nodos)..........................................................................184 3.14.3.2.-Pile Displacement Report (Desplazamientos en pilotes) ..........................................................................184 3.14.3.3.-Pile Internal Force Report (Esfuerzos en pilotes) .....................................................................................184 3.14.3.4.-Pile Capacity Used Report (Capacidad de pilotes en kg) ........................................................................184 3.14.3.5.-Special Event History Report (Elemento plastificado) .............................................................................184




AV-F.32065-1815-31-MC-REV.0 MEMORIA RU AV. PERIFERICA NORTE # 75 ESQ. CON CALLE 35 B COL. SAN AGUSTIN DEL PALMAR, C. P. 24118, CD. DEL CARMEN, CAMP. TELMEX (01938) 120-49 MICRO 293-49. FAX: (01938) 120-42 MICRO 293-77

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3.1. INTRODUCCIÓN Debido a las necesidades de crecimiento de los campos operativos de hidrocarburos y a solicitud de PEP, se realizó la evaluación de resistencia última por oleaje de la Plataforma Recuperadora Sea Pony Kab-101, con el propósito de determinar su capacidad estructural y en caso necesario emitir las soluciones de refuerzo ante las condiciones a que se someterá dicha plataforma una vez que se le adicionen 2 conductores de 30 pulgadas de diámetro (76.20 cm). Este análisis es parte de un conjunto de estudios que permitirán verificar la capacidad estructural del Sea Pony Kab-101, esto de acuerdo con lo establecido en los alcances del proyecto IMP F.32065 denominado “Ingeniería básica y de detalle por la adición de 2 pozos en la plataforma Sea Pony KAB-101 y asistencia técnica en revisión de ingenierías realizadas por otras compañías”. 3.2. OBJETIVO Realizar el análisis estructural de resistencia última por oleaje de la plataforma Sea Pony Kab-101 del campo Kab, a la cual se le adicionarán 2 conductores de 30 pulgadas de diámetro (76.20 cm). 3.3. ALCANCE Realizar el análisis estructural de resistencia última por oleaje de la plataforma Sea Pony Kab-101, con el propósito de determinar su capacidad estructural y en caso necesario, establecer las medidas mitigantes mediante refuerzo estructural y llevar a cabo la ingeniería de detalle que permita a la plataforma cumplir con las especificaciones mínimas de la normatividad aplicable. Dado que uno de los nuevos pozos será instalado en el interior de la columna principal de la estructura, no se considera en el modelo de análisis estructural. 3.4. DATOS DE LA ESTRUCTURA Ver datos de la estructura en el documento AV-F.32065-1815-31-MC-MEMORIA O Y T. 3.5. BASES DE ANÁLISIS Ver bases de analisis en el documento AV-F.32065-1815-31-MC-MEMORIA O Y T. 3.6.- JUSTIFICACIÓN DEL ANÁLISIS Y CONSIDERACIONES ESPECÍFICAS Aún cuando la estructura cumple con la elevación mínima de cubierta inferior para una categoría moderada (H = 14.50 m, de acuerdo a la NRF-003-PEMEX-2000), se tiene que el iniciador principal para esta evaluación fue que la ola de R. U. si alcanza a impactar sobre la cubierta. Es necesario mencionar que para este caso en particular, al realizar una corrida con los parámetros asociados a una ola de H = 21.00 m, el SEASTATE indicó que la ola rompe antes de alcanzar dicha altura. Después de algunas iteraciones se obtuvo una altura de ola con la cual no se presente el rompimiento antes de alcanzar su altura. Esta altura fue de H = 19.50 m y es la que se consideró como la ola de R. U. Mensaje de error generado por el Seastate para H = 21.00 m:





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*** ERROR - SPECIFIED WAVE EXCEEDS BREAKING WAVE OF HEIGHT 64.818 FT. LOADS WILL NOT BE GENERATED Es una práctica común y de relevante consideración en este tipo de análisis el incrementar el esfuerzo de fluencia nominal (Fy) del acero al esfuerzo de fluencia promedio con el propósito de generar datos más verídicos de la capacidad y comportamiento real de la estructura; en la siguiente tabla de equivalencias se muestran los valores empleados en los análisis.

Tabla 3.4.- Esfuerzos de fluencia de aceros utilizados (basados en datos reportados por el

Structural Shapes Producers Council (PSC 1994))

Tipo de acero Fy nominal (Kg/cm2)

Fy medio (Kg/cm2)

A-36 2531 3460 A-572 Grado 50 3515 4050

A36 de 2531 kg/cm2 a 3460 kg/cm2 ⇒ 36.65% inc. A572 de 3515 kg/cm2 a 4050 kg/cm2 ⇒ 15.22% inc.

Por lo anterior, se empleará un incremento del 36% al A35. Entonces el Fy a usar será: 2461 x 1.36 = 3346.96 kg/cm2 3.7. MODELO ESTRUCTURAL En la tabla 3.5, se presentan las características de las secciones utilizadas en el modelo estructural.

Tabla 3.5a.- Propiedades de las secciones utilizadas

GRUPOTIPO DE SECCIÓN ANCHO DE

PATÍN (cm)

ESPESOR DE

PATÍN (cm)

ALTURA

TOTAL (cm)

ESPESOR DE ALMA(cm)

MÓDULO DE ELASTICIDAD E x

1000 (kg/cm2)

MÓDULO AL CORTANTE (G) x

1000 (kg/cm2)

Fy DEL ACERO

(kg/cm2)

DENSIDAD DEL ACERO (ton/m3)

I12 IR (W12X30) 16.561 1.118 31.349 0.66 2100 787.5 3460 7.849I14 IR (W14X30) 17.094 0.978 35.154 0.686 2100 787.5 3460 7.849

W10 IR (W10X30) 10.058 0.533 25.07 0.483 2100 787.5 3460 7.849W12 IR (W12X12) 16.561 1.118 31.344 0.66 2100 787.5 3460 7.849W14 IR (W14X30) 17.094 0.978 35.154 0.686 2100 787.5 3460 7.849W6 IR (W6X16) 10.236 1.029 15.951 0.66 2100 787.5 3460 7.849W8 IR (W8X21) 13.386 1.016 21.031 0.635 2100 787.5 3460 7.849

Tabla 3.5b.- Propiedades de las secciones utilizadas

GRUPOTIPO DE SECCIÓN ALTURA

(cm)

ANCHO

(cm)

ESPESOR DE ALMA

(cm)

ESPESOR DE PATÍN(cm)

MÓDULO DE ELASTICIDAD E x

1000 (kg/cm2)


1000 (kg/cm2)

Fy DEL ACERO

(kg/cm2)


C10 CANAL (C10X153) 25.4 6.604 0.61 1.107 2100 787.5 3460 7.849





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Tabla 3.5c.- Propiedades de las secciones utilizadas

GRUPOTIPO DE SECCIÓN MÓDULO DE

ELASTICIDAD E x 1000 (kg/cm2)


1000 (kg/cm2)

Fy DEL ACERO

(kg/cm2)


10A TUBO 2100 787.5 3347 7.84910B TUBO 2100 787.5 3347 7.84912A TUBO 2100 787.5 3347 7.84912B TUBO 2100 787.5 3347 7.84912C TUBO 2100 787.5 3347 7.84912D TUBO 2100 787.5 3347 7.84924A TUBO 2100 787.5 3347 7.84924B TUBO 2100 787.5 3347 7.84930A TUBO 2100 787.5 4050 7.84930A TUBO 2100 787.5 3347 7.84930B TUBO 2100 787.5 3347 7.84930B TUBO 2100 787.5 4050 7.8494A TUBO 2100 787.5 3347 7.8495A TUBO 2100 787.5 3460 7.8496A TUBO 2100 787.5 3347 7.8496B TUBO 2100 787.5 3460 7.8498A TUBO 2100 787.5 3347 7.8498B TUBO 2100 787.5 3460 7.849

CL2 TUBO 2100 787.5 3347 7.849CL2 TUBO 2100 787.5 4050 7.849CL3 TUBO 2100 787.5 4050 7.849CL3 TUBO 2100 787.5 3347 7.849CL4 TUBO 2100 787.5 3347 7.849CON TUBO 2100 787.5 3347 7.849LG1 TUBO 2100 787.5 4050 7.849LG2 TUBO 2100 787.5 3347 7.849LG2 TUBO 2100 787.5 3347 7.849LG2 TUBO 2100 787.5 4050 7.849LG3 TUBO 2100 787.5 4050 7.849LG3 TUBO 2100 787.5 3347 7.849LG4 TUBO 2100 787.5 3347 7.849LG4 TUBO 2100 787.5 4050 7.849LG5 TUBO 2100 787.5 4050 7.849LG5 TUBO 2100 787.5 4050 7.849LG6 TUBO 2100 787.5 4050 7.849LG7 TUBO 2100 787.5 4050 7.849LG7 TUBO 2100 787.5 4050 7.849LG8 TUBO 2100 787.5 4050 7.849LG9 TUBO 2100 787.5 4050 7.849LG9 TUBO 2100 787.5 4050 7.849LG9 TUBO 2100 787.5 3347 7.849P42 TUBO 2100 787.5 3347 7.849SEA TUBO 2100 787.5 3347 7.849SEA TUBO 2100 787.5 3347 7.849W.B TUBO 2100 787.5 3347 0.001W.C TUBO 2100 787.5 3347 0.001

16.828

DIÁMETRO(cm)

27.305 2.54

32.385 1.427

27.305

32.38532.385

4.1483.1752.54

121.92121.92121.92

76.2121.92 1.905

121.92

1.905

5.6745.726

ESPESOR(cm)

1.27

0.9521.6962.966

1.27

5.08

2.858

5.08

2.858

2.858

106.776.2

2.542.541.9051.9052.8582.858

5.08

121.92

106.7106.68106.68

121.92

121.92

121.92121.92

121.92

121.92121.92121.92

121.92

121.92121.92121.92

60.96

121.92121.92121.92

21.908

76.276.2

5.0741.905

3.1751.905

2.544.445

3.175

1.905

21.908121.92

76.211.43

16.828

76.2

14.1

1.905

1.588

1.588

2.540.602

0.711

0.7931.097

1.271.588

1.587

32.385

60.96

1.905

3.8.- CARGAS CONSIDERADAS





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3.8.1.- CARGAS GRAVITACIONALES 3.8.1.1.- Peso propio Incluye el peso de los elementos estructurales modelados geométricamente tales como pilotes, columnas, vigas, etc., así como el de los elementos no estructurales como defensa de conductores y embarcadero. Se consideró un factor de incremento al peso propio por contingencia del 5% debido a que algunos accesorios secundarios no fueron modelados. El peso de todos los elementos de acero definidos en el modelo estructural, es calculado por el programa de cómputo SACS utilizando una densidad del acero de 7850 kg/m3.

Tabla 3.6.- Peso Propio modelado

PESO PROPIO MODELADO PESO SECO

MODELADO (TON) FLOTACIÓN

(TON) PESO PROPIO DE LA

ESTRUCTURA MODELADA (TON)

174.80 -70.72 104.02 3.8.1.2.- Carga muerta En esta carga se considera el peso de todos los elementos que permanecerán en todo momento actuando sobre la estructura y que no fueron modelados, como son muro contra incendio, placas, escaleras, ánodos de sacrificio, etc. En la tabla siguiente se desglosan las cargas muertas de la cubierta +15.850 m y de la subestructura, consideradas en el análisis estructural.

En la cubierta principal (+15.850 m) de la superestructura, se considera una carga uniformemente distribuida de 100 kg/m2.

Tabla 3.7.- Cargas muertas consideradas en la cubierta elev. +15.850 m y subestructura

DESCRIPCIÓN CARGA MUERTA (TON)

Escaleras que comunican la cub. principal con el helipuerto 0.40 Acceso a cubierta 0.61 Ánodos de sacrificio 2.45 Placa base 0.93 Muro contra incendio 6.80 Carga muerta (100 Kg./m2 ) en cubierta +15.850 m. 13.20 Abrazadera de defensa 1.03 Orejas de superestructura 0.11 Abrazadera de conductores 5.92 Orejas de subestructura 0.57 Descanso 0.30

TOTAL = 32.33 A continuación se presentan las cargas muertas consideradas en el análisis en la zona del helipuerto en la elev. +21.946 m.

Tabla 3.8.-Cargas muertas consideradas en helipuerto (elev. +21.946 m)





3.189

DESCRIPCIÓN CARGA MUERTA (TON)

Escaleras que comunican al helipuerto con la cub. principal 0.41 Placa de 1/2" del sistema de piso del helipuerto (99.6 kg/m2) 7.84 Malla de seguridad del helipuerto (46.5 kg/m) 1.65 Orejas de izaje del helipuerto 0.08

TOTAL = 9.98

El peso total de la carga muerta de toda la plataforma es de 42.31 toneladas.

3.8.1.3.- Carga viva Comprende toda aquella carga de carácter transitorio actuando sobre la estructura, representando la posibilidad de existencia de personal o equipo adicional (recipientes, mobiliario, contenedores, etc.), repartida en áreas como la cubierta principal elev. +15.850 m y el helipuerto elev. +21.946 m. La densidad de carga que se utilizó es de 500.00 kg/m2 para la cubierta principal y de 195.30 kg/m2 para el helipuerto. En la tabla 3.9 se muestra un resumen de las cargas vivas consideradas.

Tabla 3.9.- Carga viva

DESCRIPCIÓN DENSIDAD EN (kg/m2 )

CARGA VIVA EN (TON)

Carga viva en elev. +15.850 m 500.00 54.64 Carga viva en helipuerto 195.30 14.90

TOTAL = 69.54 3.8.1.4.- Carga de equipo Adicional a las cargas vivas y muertas, en el análisis estructural se consideró una carga correspondiente al peso de los equipos que soportará la plataforma, dentro de los cuales se encuentran:

Tabla 3.10.- Carga de equipo

DESCRIPCIÓN CARGA DE EQUIPO (TON)

Radio 0.20 JB de PLC de procesos 0.15 FA-1500 2.00 JB equipo de Telecom 0.15 Rack de instrumentos 0.50 JB de PLC de seguridad 0.30 Banco de baterías 1.80 Tablero de pozos 0.80 Tablero de interfase 0.80 PA-1100 1.50 Micro turbina 2.00 Inyector de químicos 1.50 Trampa de diablos 4.00

TOTAL = 15.70 3.8.1.5.- Peso del Helicóptero





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El peso del helicóptero corresponde al helicóptero “Twin modelo 212” con un peso de 5,080 Kg., dato que fue extraído de la norma API RP-2L-96.

3.8.1.6.- Resumen de cargas gravitacionales A continuación se presenta el resumen de todas las cargas gravitacionales utilizadas en el modelo estructural para el análisis de Resistencia Última.

Tabla 3.11.- Cargas gravitacionales

DESCRIPCIÓN CONDICIÓN DE CARGA

PESO EN (TON)

Peso Propio - Flotación 1 104.02 Carga Muerta en elev. +15.850 m y subestructura 2 32.33 Carga Muerta en helipuerto elev. +21.946 m 3 9.98 Carga Viva en elev. +15.850 m 4 54.64 Carga Viva en helipuerto elev. +21.946 m 5 14.90 Carga de equipo en cubierta elev. +15.850 m 6 15.70 Carga de helicóptero en elev. +21.946 m 7 5.08 TOTAL = 236.85

Debido a que se partió del modelo empleado para el análisis por Operación y Tormenta, se conservan las condiciones de Carga Viva en helipuerto y carga de helicóptero en el archivo de entrada, pero no se consideran para este análisis. La carga viva en la cubierta principal se reduce al 75%. 3.8.2.- CARGAS AMBIENTALES 3.8.2.1.- Parámetros para la obtención de fuerzas de oleaje, corriente y viento Para la secuencia de cargas en el análisis de Resistencia Última, se requiere una condición en la cual, la cresta de la ola “pase rozando” la parte inferior de las trabes de la cubierta de la plataforma. Por lo anterior, y después de algunas iteraciones, se determinó que la altura de ola cuya cresta rosa la cubierta de la plataforma, es de H = 17.50 m. Para este análisis se analizaron las mismas direcciones de incidencia que en el análisis por Operación y Tormenta.

330°

292° 270° 240°

210°

180°

150°

120°90°68°

30°

0°

Figura 3.12.- Direcciones de análisis consideradas.

Los coeficientes de arrastre y de inercia fueron seleccionados de acuerdo a la sección 12.1.2 de la NRF-





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003-PEMEX-2000 y a la sección 2.3.1b-7 del API RP-2A-WSD (Edición 20) y se resume en la tabla siguiente:

Tabla 3.12.- Coeficientes de arrastre y de inercia

Tipo de superficie

Coeficiente de arrastre

Coeficiente de inercia

Lisa o sin crecimiento marino 0.65 1.60

Rugosa o con crecimiento marino 1.05 1.20

Para tomar en cuenta el efecto de dispersión direccional, se consideró un factor de cinemática de ola de 0.85 para condiciones de tormenta según la sección 12.1.2 de la NRF-003-PEMEX-2000. Parámetros para la obtención de fuerzas de oleaje, corriente y viento asociados a una altura de ola H = 17.50 m. Se utilizaron los valores de la tabla que se muestra a continuación:

Tabla 3.13.- Parámetros meteorológicos para H=17.50 m.

Periodo de retorno de ref. (años) 570 Altura de Ola Máxima (m) 17.50 Periodo de la Ola (s) 12.55 Marea Astronómica (m) 0.76 Marea de Tormenta (m) 1.25 Viento 3 s a 10 m (m/s) 61.00 Viento 5 s a 10 m (m/s) 58.95 Viento 15 s a 10 m (m/s) 54.54 Viento 1 min a 10 m (m/s) 48.97 Viento 1 h a 10 m (m/s) 40.92 Corriente (cm/s):

0% 117 50% 112 95% 107

Velocidad del viento a 10 m SNMM:

1 h = 40.92 m/s = 147.31 km/h

Velocidad de corriente:

0 % de la profundidad = 1.17 m/s



Vprom = 1.12 m/s





3.192

0168.0)55.12)(81.9(

00.2422 ==

gTd

0091.0)55.12)(81.9(

12.1==

gTV prom

Figura 3.13.- Efecto Doppler debido a la corriente.

De la figura 3.13, obtengo: 08.1=TTapp

Despejando Tapp nos queda: sTapp 5.13)55.12)(08.1( ==

Por lo tanto:

0098.0)5.13)(81.9(

5.1722 ==

appgTH





3.193

0146.0)5.13)(81.9(

00.2422 ==

appgTd

De las Figuras 2.3.1-2 y 2.3.1-3 del API se determina que la teoría de oleaje a utilizar será Stream Fuction 9° orden, como se muestra en la figura siguiente:

Figura 3.14.- Teoría del oleaje.





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XZ PLANE VIEW AT -9.00

WIND

WINDDIRECTION 0.000 (deg)VELOCITY 40.920 (mps)

WAVEWAVE STREAM DIRECTION 0.000 (deg)HEIGHT 17.500 (m) PERIOD 12.550 (sec)WATER DEPTH 26.01 (m)

CURRENT DIRECTION 0.000 (deg)MAX VEL 1.170 (mps)

LOAD CONDITION 9

N. M. M.NIVEL DE MAREAS

1.88 m.

24.00 m.

17.50 m.

22.04 m.

39.54 m.

Figura 3.15.- Gráfica representativa de la altura de ola

que pasa por debajo de la cubierta H=17.50 m. **** WAVE DESCRIPTION FOR LOAD CASE 9 **** Vto., oleaje y corr. H=17.5m +X WAVE THEORY ************ STREAM FUNCTION WAVE HEIGHT ************ 17.500 M WATER DEPTH ************ 26.010 M WAVE PERIOD ************ 13.531 SECS WAVE LENGTH ************ 222.870 M ANGLE FROM X TOWARD Y ** 0.000 DEGREES MUDLINE ELEVATION ****** -24.000 M WAVE CELERITY ********** 16.472 M /SEC MAX. NO. SEG/MEMBER **** 4 MIN. NO. SEG/MEMBER **** 1 UNMODIFIED WAVE PERIOD 12.550 SECS STREAM FUNCTION ORDER ** 9 BREAKING WAVE HEIGHT 19.237 M WAVE SPREADING FACTOR ** 0.850 CREST POSITION DETERMINED BY MAXIMUM MOMENT STARTING CREST POSITION -50.000 M NO. STEPS ************** 99 STEP SIZE ************** 1.000 M CREST WATER DEPTH ****** 39.54 M TROUGH WATER DEPTH ***** 22.04 M





3.195

Parámetros para la obtención de fuerzas de oleaje, corriente y viento asociados a la ola de Resistencia Ultima, H = 19.50 m.

Se utilizaron los valores de la tabla que se muestra a continuación:

Tabla 3.14.- Parámetros meteorológicos para H=19.50 m.

Periodo de retorno de ref. (años) 1502 Altura de Ola Máxima (m) 19.50 Periodo de la Ola (s) 13.32 Marea Astronómica (m) 0.76 Marea de Tormenta (m) 1.36 Viento 3 s a 10 m (m/s) 68.31 Viento 5 s a 10 m (m/s) 66.01 Viento 15 s a 10 m (m/s) 61.07 Viento 1 min a 10 m (m/s) 54.84 Viento 1 h a 10 m (m/s) 45.82 Corriente (cm/s):

0% 132 50% 127 95% 122

Velocidad del viento a 10 m SNMM:

1 h = 45.82 m/s = 164.95 km/h

Velocidad de corriente:




Vprom = 1.27 m/s

0150.0)32.13)(81.9(

00.2422 ==

gTd

0097.0)32.13)(81.9(

27.1==

gTV prom





3.196

Figura 3.16.- Efecto Doppler debido a la corriente

De la figura 3.16, obtengo: 09.1=TTapp

Despejando Tapp nos queda: sTapp 45.14)32.13)(09.1( ==

Por lo tanto:

0095.0)45.14)(81.9(

50.1922 ==

appgTH

0128.0)45.14)(81.9(

00.2422 ==

appgTd





3.197

De las Figuras 2.3.1-2 y 2.3.1-3 del API se determina que la teoría de oleaje a utilizar será Stream Fuction 9° orden, como se muestra en la figura siguiente:

Figura 3.17.- Teoría del oleaje.





3.198

WIND

WAVE

N. M. M.NIVEL DE MAREAS

2.21 m.

24.00 m.

19.50 m.

22.29 m.

41.79 m.

LOAD CONDITION 10

MAX VEL 1.320 (mps)DIRECTION 0.000 (deg)CURRENT

WATER DEPTH 26.12 (m) PERIOD 13.320 (sec)HEIGHT 19.500 (m) DIRECTION 0.000 (deg)WAVE STREAM

VELOCITY 45.820 (mps)DIRECTION 0.000 (deg)WIND

XZ PLANE VIEW AT -9.00

Figura 3.18.- Grafica representativa de la altura de ola de resistencia ultima H=19.50 m

**** WAVE DESCRIPTION FOR LOAD CASE 10 **** Vto., ole. y corr. H=19.50m +X WAVE THEORY ************ STREAM FUNCTION WAVE HEIGHT ************ 19.500 M WATER DEPTH ************ 26.120 M WAVE PERIOD ************ 14.480 SECS WAVE LENGTH ************ 245.716 M ANGLE FROM X TOWARD Y ** 0.000 DEGREES MUDLINE ELEVATION ****** -24.000 M WAVE CELERITY ********** 16.969 M /SEC MAX. NO. SEG/MEMBER **** 4 MIN. NO. SEG/MEMBER **** 1 UNMODIFIED WAVE PERIOD 13.320 SECS STREAM FUNCTION ORDER ** 9 BREAKING WAVE HEIGHT 19.561 M WAVE SPREADING FACTOR ** 0.850 CREST POSITION DETERMINED BY MAXIMUM MOMENT STARTING CREST POSITION -50.000 M NO. STEPS ************** 99 STEP SIZE ************** 1.000 M CREST WATER DEPTH ****** 41.79 M TROUGH WATER DEPTH ***** 22.29 M





3.199

3.8.2.2.- Fuerzas de oleaje sobre la cubierta Las fuerzas horizontales del oleaje en los sentidos longitudinal y transversal fueron calculadas de acuerdo al procedimiento indicado en la NRF-003-PEMEX-2000, se muestran a continuación:

Tabla 3.15.- Fuerzas del oleaje sobre cubierta

SENTIDO MAGNITUD DE LA FUERZA

HORIZONTAL Fdk (TON) Longitudinal 30.129 Transversal 23.923

Tabla 3.16.-Cálculo de las fuerzas del oleaje sobre cubierta

Alturade

cresta

Largoa

considerar

Anchoa

considerar

Elevación del nivel más bajo del área

mojada

Diferencia entre altura de cresta y nivel más bajo del área mojada

Area expuestaen sentido transversal

Area expuesta en

sentido longitudinal

Angulo de incidencia de

la ola

Proyección del área mojada

(m) (m) (m) (m) (m) (m2) (m2) (Grados) (m2)Sentido

Longitudinal 17.79 10.528 13.259 15.54 2.25 29.833 0 29.833Diagonal 17.79 10.528 13.259 15.54 2.25 23.688 29.833 150 -13.992Transversal 17.79 10.528 13.259 15.54 2.25 23.688 90 23.688

Velocidad de la partícula en la cresta

Velocidad de la corriente

asociada con la ola

Coeficiente de cinemática

Factor de bloqueo para la subestructura

Coeficiente de arrastre máximo Vc2/g

Coeficiente de arrastre a la

altura media del área mojada

Magnitud de la fuerza horizontal

Fuerza por nodo

Momento por nodo

Vc(m/s) U(m/s) αwkf αcbf Cdmax (m) Cd Fdk(Tonf) Ton Ton-m

13.158 1.42 0.85 0.80 2.0 17.649 0.127 30.193 30.193 33.96713.158 1.42 0.85 0.80 1.5 17.649 0.096 -10.621 -10.621 -11.94813.158 1.42 0.85 0.80 2.0 17.649 0.127 23.974 23.974 26.971

g = aceleración de la gravedad Fdk = 1/2 ρ Cd (αwkf V + αcbf U)**2 Ag =(m/s2)= 9.81 ρ(k-s2/m4)= 104.504

17.7913.259

24.00

19.50

ρ=densidad del agua

10.52841.79

Altura de Ola

Tirante de Agua

N.M.A.

Marea de Tormenta

Marea Astronomica+Marea total =

Altura de la Cresta

Elevacion de la Cresta

VISTA EN PLANTA DE LA CUBIERTA

θW

INCIDENCIA DE LA OLA

LARGO A CONSIDERAR

ANCHO A CONSIDERAR

θ W

Figura 3.19.- Parámetros utilizados para el cálculo de las fuerzas del oleaje sobre cubierta

En siguiente listado, se presentan las velocidades horizontales de partícula de la ola. De este listado se





3.200

obtiene la velocidad máxima para el cálculo de las fuerzas por oleaje en cubierta.

HORIZONTAL VELOCITY

THETA 0.000 10.000 20.000 30.000 40.000 50.000 60.000 70.000 80.000 90.000 100.000 110.000

SURFACE 41.786 37.461 33.831 31.092 28.943 27.251 25.947 24.962 24.221 23.665 23.255 22.957

HEIGHT * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *

41.79 13.158 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

41.48 12.866 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

40.97 12.398 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

40.24 11.784 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

39.30 11.063 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

38.16 10.277 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

36.80 9.462 8.242 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

35.23 8.650 7.652 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

33.45 7.866 7.057 5.217 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

31.46 7.128 6.482 4.954 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

29.27 6.447 5.933 4.674 3.212 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

26.86 5.831 5.423 4.388 3.123 1.894 0.807 0.000 0.000 0.000 0.000 0.000 0.000

24.24 5.283 4.956 4.106 3.020 1.919 0.923 0.106 -0.500 0.000 0.000 0.000 0.000

21.40 4.805 4.541 3.840 2.909 1.930 1.019 0.249 -0.351 -0.799 -1.133 -1.373 -1.533

18.36 4.396 4.183 3.599 2.797 1.927 1.094 0.368 -0.220 -0.677 -1.025 -1.281 -1.463

15.11 4.056 3.882 3.386 2.692 1.915 1.151 0.465 -0.110 -0.570 -0.929 -1.200 -1.399

11.65 3.785 3.639 3.211 2.600 1.898 1.192 0.540 -0.021 -0.482 -0.849 -1.131 -1.344

7.98 3.586 3.457 3.081 2.527 1.882 1.218 0.594 0.045 -0.415 -0.787 -1.078 -1.301

4.09 3.462 3.342 2.996 2.480 1.869 1.234 0.627 0.086 -0.373 -0.748 -1.044 -1.273

0.00 3.418 3.299 2.963 2.461 1.864 1.239 0.640 0.102 -0.357 -0.733 -1.032 -1.263

3.8.2.3.- Fuerzas de viento





3.201

Las fuerzas sobre el equipo existente sobre la cubierta del Sea Pony, inducidas por el viento, fueron obtenidas mediante el programa SACS, definiendo las áreas (pantallas) de viento correspondientes al equipo, empleando un coeficiente de forma CS=1.5. 3.9.- ANÁLISIS ESTRUCTURAL Se utilizó el modelo estructural tridimensional del análisis elástico in-situ en condiciones de operación y tormenta realizado en el programa de computo SACS, en donde se detallaron las secciones y elementos estructurales que conforman la superestructura, subestructura, conductores y el helipuerto. La modelación de los elementos no-estructurales, tuvo como objetivo la determinación de las fuerzas laterales de viento, oleaje y corriente que inciden sobre ellos, mismas que contribuyen a incrementar el empuje lateral al cual se somete la plataforma y que contribuyen muy poco en la rigidez global, permitiendo además reducir los tiempos de ejecución del programa ya que se hace más sencillo el proceso. En el modelo se consideraron los siguientes elementos como no-estructurales: El análisis estructural de la plataforma se efectuó mediante un análisis de incremento de carga (pushover), considerando la interacción suelo estructura con el programa de computadora SACS, el cual efectúa un análisis del comportamiento de todos los elementos estructurales hasta abarcar el rango inelástico. Con el fin de simplificar el análisis, se consideraron todos los elementos del helipuerto y de la cubierta principal, así como conductores con comportamiento linealmente elástico. GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A De acuerdo con la Norma de Referencia NRF-003-PEMEX-2000, para el empleo de las propiedades mecánicas del suelo en los análisis de resistencia última ante efectos de oleaje de tormenta se establece un incremento del 20% de la resistencia al esfuerzo cortante de los suelos arcillosos para plataformas con más de 10 años de haber sido instaladas, lo cual es aplicable a esta plataforma, ya que la fecha de instalación reportada es 22 de abril de 1994. Este incremento no es aplicable a suelos arenosos. 3.10.- RESULTADOS DEL ANÁLISIS Debido a que se trata de una estructura poco redundante (únicamente tiene tres piernas), se menciona que la falla por colapso es de tipo frágil, ya que casi desde el instante en que se plastifica el primer elemento estructural al 100%, se define la falla súbita del sistema. 3.10.1.- MECANISMO DE COLAPSO PARA 0°





3.202

Resumen de cargas para 0°

** SEASTATE BASIC LOAD CASE DESCRIPTIONS **

LOAD LOAD ********** DESCRIPTION ***********

CASE LABEL

1 1 Peso Propio y Flotacion

2 2 C. M. en Cub. +15.850 y subestruct.

3 3 C. M. en Helipuerto Elev. +21.946

4 4 C. V. en Cubierta Elev. +15.850

5 5 C. V. en Helipuerto Elev. +21.946

6 6 C. de Equipos en Cub. Elev. +15.850

7 7 Carga de Helicoptero

8 8 Cargas de oleaje en Cub.

9 9 Vto., oleaje y corr. H=17.5m +X

10 10 Vto., ole. y corr. H=19.50m +X

SACS Release 5.1 IMP ID=00660118

*********** EDI/SACS IV SEASTATE PROGRAM *********** DATE 16-FEB-2005 TIME 10:13:42 SEA PAGE

99

****** SEASTATE BASIC LOAD CASE SUMMARY ******

RELATIVE TO MUDLINE ELEVATION

LOAD LOAD FX FY FZ MX MY MZ DEAD LOAD BUOYANCY

CASE LABEL

(KG) (KG) (KG) (KG-M) (KG-M) (KG-M) (KG) (KG)

1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 29999.998 0.000 0.000 0.000 1190789.880 0.000 0.000 0.000

9 9 280866.469 128.828 3686.139 -28190.725 6630383.000 99444.180 0.000 0.000

10 10 350234.063 116.533 10924.667 -33051.605 8687972.000 111687.414 0.000 0.000





3.203

***** SEASTATE COMBINED LOAD CASES *****

COMBINED BASIC PERCENT DESCRIPTION

LOAD LABEL LABEL

CASE

11 11

1 105.00 Peso Propio y Flotacion

2 100.00 C. M. en Cub. +15.850 y subestruct.

3 100.00 C. M. en Helipuerto Elev. +21.946

4 75.00 C. V. en Cubierta Elev. +15.850

6 100.00 C. de Equipos en Cub. Elev. +15.850

12 12

10 100.00 Vto., ole. y corr. H=19.50m +X

8 100.00 Cargas de oleaje en Cub.

9 -100.00 Vto., oleaje y corr. H=17.5m +X

***** SEASTATE COMBINED LOAD CASE SUMMARY *****


LOAD LOAD FX FY FZ MX MY MZ

CASE LABEL

(KG) (KG) (KG) (KG-M) (KG-M) (KG-M)

11 11 0.000 0.000 -209761.594 51591.305 297353.594 0.000

12 12 99367.602 -12.296 7238.528 -4860.881 3248379.250 12243.236

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso:





3.204

El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa 280.87 ton / 100 = 2.81 ton para la dirección X y 0.13 ton / 100 = 0.00 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa 99.37 ton / 100 = 0.99 ton para la dirección X y de -0.01 ton / 100 = 0.00 ton para la dirección Y.

Tabla 3.17.- Incrementos de carga, dirección 0°

FASE CONDICIÓN DE CARGA FUERZA TOTAL (TON)

No. DE INCREMENTOS

FUERZA APLICADA POR INCREMENTO

(TON)

1.- CONDICION 11 (FUERZAS GRAVITACIONALES) -209.76 10 -20.98

2.- CONDICION 9 EN DIR.X (viento, oleaje y corriente 0°. H=17.5 m.) 280.87 100 2.81

CONDICION 9 EN DIR.Y (viento, oleaje y corriente 0°. H=17.5 m.) 0.13 100 0.00

3.- CONDICION 12 EN DIR.X (RU H=19.5 m.) 99.37 100 0.99

CONDICION 12 EN DIR.Y (RU H=19.5 m.) -0.01 100 0.00

Mecanismo: El factor de carga máximo alcanzado es de 0.59 de la condición de carga 12 en el paso 169 (como se puede observar en el historial de carga).

Figura 3.20.- Estado final de la secuencia de carga en dirección 0°.





3.205

Historial de Carga: En la siguiente tabla se muestra un resumen del historial de carga para la dirección 0°.

Tabla 3.18.- Resumen del historial de carga, dirección 0°

DEFLECTION DEFLECTION NSLV. INC. LOOP LOAD CASE

LOAD FACTOR DIFF. JNT DOF

ROTATION DIFFERENCE MAXIMUM JNT DOF

4 2 1 11 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 11 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 11 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 11 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 11 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 60 30 1 9 0.20 0.0237 463 DX 0.0001948 24.547 525 DX

100 50 1 9 0.40 0.0669 319 DX 0.0001854 39.411 525 DX 140 70 1 9 0.60 0.0227 525 DX 0.0001398 55.209 525 DX 180 90 1 9 0.80 0.0256 525 DX 0.0001190 71.750 525 DX 224 110 1 9 1.00 0.0284 525 DX 0.0005803 89.002 525 DX 250 120 1 12 0.10 0.0298 525 DX 0.0007651 95.311 525 DX 280 130 1 12 0.20 0.0366 525 DX 0.0013741 101.773 525 DX 323 140 1 12 0.30 0.0839 463 DX 0.0015461 109.125 525 DX 395 150 1 12 0.40 0.1874 463 DX 0.0015645 120.329 525 DX 584 160 1 12 0.50 0.2132 463 DX 0.0019444 135.294 525 DX 682 165 1 12 0.55 0.5228 841 DY 0.0220734 142.882 525 DX 702 166 1 12 0.56 1.1030 841 DY 0.0459530 144.865 525 DX 722 167 1 12 0.57 2.2924 841 DY 0.0937210 148.860 525 DX 742 168 1 12 0.58 4.7579 841 DY 0.1897142 152.323 525 DX 762 169 1 12 0.59 11.0145 841 DY 0.4139015 155.606 525 DX 780 169 19 12 0.59 12.5801 841 DY 0.4351410 158.256 525 DX 782 170 1 12 0.60 26.0361 841 DY 0.8935081 161.144 525 DX 783 170 2 12 0.60 62.2350 841 DY 1.6542482 165.886 525 DX 784 170 3 12 0.60 44.7170 841 DY 1.1433419 164.429 525 DX

785 170 4 12 0.60 100.8184 841 DY 2.5230856 170.859 525 DX Gráficas de factor de carga-deformación en la dirección 0°:





3.206

Figura 3.21.- Factor de Carga – Deformación en X, en dirección 0° nodo 6.

Figura 3.22.- Factor de Carga – Deformación en X en dirección 0° nodo 459.





3.207


Revisión de la capacidad de carga axial en pilotes: La capacidad de carga es la correspondiente al factor de carga máximo alcanzado hasta antes de que se presente el colapso global del sistema.

Tabla 3.19.- Capacidad de carga axial en pilotes, dirección 0°

PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)

CAPACIDAD TOTAL (kg) CAPACIDAD USADA (%)

169 12 0.59 102 553873.1 1038374.3 53.3 Tensión 169 12 0.59 119 -357998.2 -792154.5 45.2 Compresión 169 12 0.59 199 -358084.4 -792154.5 45.2 Compresión 169 12 0.59 841 9831.6 703213.8 1.4 Tensión 169 12 0.59 722 -18199.7 -651519 2.8 Compresión





3.208

3.10.2.- MECANISMO DE COLAPSO PARA 30° Resumen de cargas para 30°



CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 30°

11 11 Vto., ole. y corr. H=19.50m 30°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 29999.998 0.000 0.000 0.000 1190789.880 0.000 0.000 0.000

9 9 0.000 25000.000 0.000 -992325.000 0.000 0.000 0.000 0.000

10 10 247335.625 145339.438 4225.976 -3376284.500 5835566.500 294630.969 0.000 0.000

11 11 307707.344 179896.422 5905.161 -4395677.500 7643837.000 356078.594 0.000 0.000





3.209



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 30°



10 -100.00 Vto., ole. y corr. H=17.50m 30°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 79871.727 43931.988 1679.185 -1391515.130 2582283.750 61447.633





3.210

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa 247.34 ton / 100 = 2.47 ton para la dirección X y 145.34 ton / 100 = 1.45 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa 79.87 ton / 100 = 0.79 ton para la dirección X y de 43.93 ton / 100 = 0.44 ton para la dirección Y.



No. DE INCREMENTOS


(TON)





CONDICION 13 EN DIR.Y (RU H=19.5 m.) 43.93 100 0.44

Mecanismo: Se presenta la plastificación de elementos, pero el factor de carga máximo alcanzado es de 1.00 de la condición de carga 13 en el paso 110 (como se puede observar en el historial de carga), Esto significa que, aún cuando se tienen secciones plastificadas, la estructura soporta el 100% de la ola de R. U.






3.211






4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 49 20 1 10 0.20 0.0467 463 DX 0.0016828 22.900 525 DX 79 30 1 10 0.40 0.1519 399 DX 0.0022946 35.945 525 DX

113 40 1 10 0.60 0.0728 525 DX 0.0024236 49.703 525 DX 158 50 1 10 0.80 0.0507 525 DX 0.0011360 64.104 525 DX 194 60 1 10 1.00 0.0633 463 DX 0.0015763 79.246 525 DX 195 60 2 10 1.00 0.0388 841 DY 0.0028137 79.249 525 DX 196 60 3 10 1.00 0.0059 842 DY 0.0004875 79.252 525 DX 209 65 1 13 0.10 0.0441 527 DZ 0.0016717 84.519 525 DX 224 70 1 13 0.20 0.0625 525 DX 0.0006500 89.883 525 DX 237 75 1 13 0.30 0.1727 525 DX 0.0003727 95.652 525 DX 261 80 1 13 0.40 0.1798 525 DX 0.0025627 103.073 525 DX 295 85 1 13 0.50 0.2953 525 DX 0.0010156 112.204 525 DX 339 90 1 13 0.60 0.688 525 DX 0.0010963 123.126 525 DX 427 95 1 13 0.70 0.8939 463 DX 0.0023626 143.398 525 DX 527 100 1 13 0.80 0.9371 463 DX 0.0030355 163.522 525 DX 638 105 1 13 0.90 0.2278 484 DZ 0.0011774 194.916 525 DX 722 110 1 13 1.00 0.4075 463 DX 0.0024226 213.348 525 DX 723 110 2 13 1.00 0.3369 525 DX 0.0034595 213.684 525 DX 724 110 3 13 1.00 0.2175 841 DY 0.0060621 213.848 525 DX 725 110 4 13 1.00 0.2817 525 DX 0.0025356 214.048 525 DX 726 110 5 13 1.00 0.2589 525 DX 0.0013419 214.166 525 DX 727 110 6 13 1.00 0.2935 463 DX 0.0024712 214.444 525 DX 728 110 7 13 1.00 0.1532 463 DX 0.0013237 214.443 525 DX 729 110 8 13 1.00 0.2778 525 DX 0.0021335 214.721 525 DX 730 110 9 13 1.00 0.1897 525 DX 0.0010302 214.771 525 DX 731 110 10 13 1.00 0.2269 463 DX 0.0017377 214.995 525 DX 732 110 11 13 1.00 0.1853 525 DX 0.0009122 215.068 525 DX 733 110 12 13 1.00 0.2042 525 DX 0.0015153 215.273 525 DX 734 110 13 13 1.00 0.1762 525 DX 0.0007704 215.347 525 DX 735 110 14 13 1.00 0.2168 463 DX 0.0015491 215.535 525 DX 736 110 15 13 1.00 0.1136 463 DX 0.0008989 215.526 525 DX 737 110 16 13 1.00 0.2108 525 DX 0.0013710 215.737 525 DX 738 110 17 13 1.00 0.1281 463 DX 0.0006892 215.756 525 DX 739 110 18 13 1.00 0.1993 525 DX 0.0012116 215.955 525 DX

740 110 19 13 1.00 0.1283 525 DX 0.0005877 215.984 525 DX





3.212

Gráficas de factor de carga-deformación en la dirección 30°:

Figura 3.25.- Factor de Carga – Deformación en Y en dirección 30° nodo 14.






3.213





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


110 13 1 102 548081.7 1038374.3 52.8 Tensión 110 13 1 119 -18930.1 -792154.5 2.4 Compresión 110 13 1 199 -694648.3 -792154.5 87.7 Compresión 110 13 1 841 -19995.8 -651519 3.1 Compresión 110 13 1 722 -19188.6 -651519 2.9 Compresión





3.214




CASE LABEL










10 10 Vto., oleaje y corr. H=17.5m 68°

11 11 Vto., ole. y corr. H=19.50m 68°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 29999.998 0.000 0.000 0.000 1190789.880 0.000 0.000 0.000

9 9 0.000 25000.000 0.000 -992325.000 0.000 0.000 0.000 0.000

10 10 109162.094 270529.344 -1445.199 -6266681.000 2634095.500 430935.125 0.000 0.000

11 11 132652.906 339031.125 1352.936 -8293209.500 3291413.500 549055.125 0.000 0.000





3.215



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 68°



10 -100.00 Vto., oleaje y corr. H=17.5m 68°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 31920.814 85886.789 2798.135 -2716591.250 991930.063 118120.008





3.216

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa 109.16 ton / 100 = 1.09 ton para la dirección X y 270.53 ton / 100 = 2.71 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa 31.92 ton / 100 = 0.32 ton para la dirección X y de 85.89 ton / 100 = 0.86 ton para la dirección Y.



No. DE INCREMENTOS


(TON)












3.217






4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 49 20 1 10 0.20 0.0793 525 DY 0.0027545 16.909 525 DX 79 30 1 10 0.40 0.079 525 DY 0.0030621 31.681 527 DY

112 40 1 10 0.60 0.0471 399 DX 0.0030045 50.406 527 DY 151 50 1 10 0.80 0.0551 525 DY 0.0016018 70.517 527 DY 200 60 1 10 1.00 0.0841 525 DY 0.0012436 92.150 527 DY 201 60 2 10 1.00 0.0201 527 DY 0.0012205 92.170 527 DY 202 60 3 10 1.00 0.0134 842 DY 0.0010337 92.165 527 DY 203 60 4 10 1.00 0.0111 842 DY 0.0008824 92.169 527 DY 224 65 1 13 0.10 0.0486 527 DZ 0.0029391 99.183 527 DY 249 70 1 13 0.20 0.0491 527 DZ 0.0017546 106.280 527 DY 271 75 1 13 0.30 0.0556 484 DZ 0.0027782 113.574 527 DY 302 80 1 13 0.40 0.1042 525 DY 0.0011441 121.398 527 DY 338 85 1 13 0.50 0.1578 525 DY 0.0018893 130.468 527 DY 367 90 1 13 0.60 0.1883 525 DY 0.0017699 141.059 527 DY 396 95 1 13 0.70 0.1467 525 DY 0.0018841 151.603 527 DY 437 100 1 13 0.80 0.6594 525 DY 0.0019787 166.608 527 DY 526 105 1 13 0.90 0.4955 525 DY 0.0036060 205.810 527 DY 546 106 1 13 0.92 0.4211 484 DZ 0.0034607 213.878 527 DY 557 107 1 13 0.94 0.8843 525 DY 0.0034016 218.648 527 DY 577 108 1 13 0.96 0.9147 525 DY 0.0036695 225.654 527 DY 595 108 19 13 0.96 9.863 399 DY 0.1226948 230.547 527 DY 597 109 1 13 0.98 2.5885 842 DY 0.0933532 233.372 527 DY

598 109 2 13 0.98 695.0645 525 DY 3.4766907 -1469.433 525 DY





3.218








3.219




PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


108 13 0.96 102 -97707.7 -913464.6 10.7 Compresión 108 13 0.96 119 517583.5 839510.2 61.7 Tensión 108 13 0.96 199 -772966.1 -792154.5 97.6 Compresión 108 13 0.96 841 45513.2 703213.8 6.5 Tensión 108 13 0.96 722 -90593.9 -651519 13.9 Compresión





3.220




CASE LABEL









9 9 Vto., oleaje y corr. H=17.5m +Y

10 10 Vto., ole. y corr. H=19.50m +Y




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 0.000 25000.000 0.000 -992325.000 0.000 0.000 0.000 0.000

9 9 -1493.551 285116.094 -7091.757 -6526214.500 31026.264 394625.719 0.000 0.000

10 10 324.569 363428.625 -822.905 -8823544.000 80051.961 531638.938 0.000 0.000





3.221



LOAD LABEL LABEL

CASE

11 11






12 12

10 100.00 Vto., ole. y corr. H=19.50m +Y


9 -100.00 Vto., oleaje y corr. H=17.5m +Y




CASE LABEL


11 11 0.000 0.000 -209761.594 51591.305 297353.594 0.000

12 12 1818.119 103312.539 6268.853 -3289654.750 49025.699 137013.234






3.222

El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -1.49 ton / 100 = -0.02 ton para la dirección X y 285.12 ton / 100 = 2.85 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa 1.82 ton / 100 = 0.02 ton para la dirección X y de 103.31 ton / 100 = 1.03 ton para la dirección Y.



No. DE INCREMENTOS


(TON)


2.- CONDICION 9 EN DIR.X (viento, oleaje y corriente 0°. H=17.5 m.) -1.49 100 -0.02




Mecanismo: Se presenta la plastificación de elementos, pero el factor de carga máximo alcanzado es de 1.00 de la condición de carga 12 en el paso 210 (como se puede observar en el historial de carga). Esto significa que, aún cuando se tienen secciones plastificadas, la estructura soporta el 100% de la ola de R. U.







3.223


DEFLECTION DEFLECTION NSLV. INC. LOOP LOAD

CASE LOAD

FACTOR DIFF. JNT DOF ROTATION

DIFFERENCE MAXIMUM JNT DOF

4 2 1 11 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 11 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 11 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 11 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 11 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 79 30 1 9 0.20 0.0414 525 DY 0.0012306 13.998 527 DY

139 50 1 9 0.40 0.0328 525 DY 0.0012424 31.087 531 DY 199 70 1 9 0.60 0.0119 484 DZ 0.0014795 50.184 525 DY 259 90 1 9 0.80 0.0187 399 DX 0.0016934 70.908 525 DY 305 110 1 9 1.00 0.0264 525 DY 0.0006088 93.706 525 DY 325 120 1 12 0.10 0.0234 484 DZ 0.0007160 101.299 525 DY 345 130 1 12 0.20 0.0256 484 DZ 0.0006717 108.988 525 DY 365 140 1 12 0.30 0.0284 484 DZ 0.0006280 116.831 525 DY 385 150 1 12 0.40 0.0588 527 DY 0.0005687 125.383 527 DY 405 160 1 12 0.50 0.1066 527 DY 0.0005135 134.958 527 DY 443 170 1 12 0.60 0.1121 525 DY 0.0004268 146.687 527 DY 489 180 1 12 0.70 0.1439 525 DY 0.0003993 159.579 527 DY 537 190 1 12 0.80 0.1428 525 DY 0.0004915 173.188 527 DY 595 200 1 12 0.90 0.5771 525 DY 0.0011037 192.224 527 DY 662 210 1 12 1.00 0.6552 525 DY 0.0009553 212.390 527 DY 663 210 2 12 1.00 0.2402 527 DY 0.0004309 212.630 527 DY 664 210 3 12 1.00 0.1623 527 DY 0.0002199 212.793 527 DY

665 210 4 12 1.00 0.0783 527 DY 0.0001015 212.871 527 DY






3.224





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


210 12 1 102 -154530.4 -913464.6 16.9 Compresión 210 12 1 119 694035.5 839510.2 82.7 Tensión 210 12 1 199 -709090.8 -792154.5 89.5 Compresión 210 12 1 841 -19901.8 -651519 3.1 Compresión 210 12 1 722 -18027.4 -651519 2.8 Compresión





3.225




CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 120°

11 11 Vto., ole. y corr. H=19.50m 120°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 -29999.998 0.000 0.000 0.000 -1190789.880 0.000 0.000 0.000

9 9 0.000 25000.000 0.000 -992325.000 0.000 0.000 0.000 0.000

10 10 -143775.000 247856.625 -11668.612 -5760189.000 -3368771.750 311632.625 0.000 0.000

11 11 -177210.938 314395.250 -8090.758 -7691857.500 -4316497.500 400106.750 0.000 0.000





3.226



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 120°



10 -100.00 Vto., ole. y corr. H=17.50m 120°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 -44685.941 82788.633 3577.854 -2576679.750 -1394271.880 88474.133






3.227

El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -143.78 ton / 100 = -1.44 ton para la dirección X y 247.86 ton / 100 = 2.48 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa -44.69 ton / 100 = -0.45 ton para la dirección X y de 82.79 ton / 100 = 0.83 ton para la dirección Y.



No. DE INCREMENTOS


(TON)




3.- CONDICION 13 EN DIR.X (RU H=19.5 m.) -44.69 100 -0.45


Mecanismo: Se presenta la plastificación de elementos, pero el factor de carga máximo alcanzado es de 1.00 de la condición de carga 13 en el paso 210 (como se puede observar en el historial de carga), Esto significa que, aún cuando se tienen secciones plastificadas, la estructura soporta el 100% de la ola de R. U.


Historial de Carga: En la siguiente tabla se muestra un resumen del historial de carga para la dirección





3.228

120°.





4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 68 30 1 10 0.20 0.0427 525 DY 0.0009213 12.578 527 DY

116 50 1 10 0.40 0.0378 525 DY 0.0008299 27.858 527 DY 175 70 1 10 0.60 0.0315 399 DY 0.0020674 44.250 527 DY 237 90 1 10 0.80 0.0173 463 DZ 0.0017022 62.139 525 DY 295 110 1 10 1.00 0.0251 463 DZ 0.0008121 81.600 525 DY 315 120 1 13 0.10 0.0175 463 DZ 0.0002075 87.358 525 DY 335 130 1 13 0.20 0.0191 463 DZ 0.0002098 93.181 525 DY 355 140 1 13 0.30 0.0206 463 DZ 0.0002015 99.091 529 DY 375 150 1 13 0.40 0.0229 463 DZ 0.0001927 105.411 527 DY 395 160 1 13 0.50 0.0406 527 DY 0.0001862 112.037 527 DY 415 170 1 13 0.60 0.0838 527 DY 0.0001928 119.109 527 DY 440 180 1 13 0.70 0.1039 527 DY 0.0002715 126.958 527 DY 474 190 1 13 0.80 0.1085 527 DY 0.0003283 135.848 527 DY 515 200 1 13 0.90 0.1352 527 DY 0.0003703 145.947 527 DY 560 210 1 13 1.00 0.2079 527 DY 0.0005266 156.342 527 DY 561 210 2 13 1.00 0.1306 527 DY 0.0003173 156.472 527 DY

562 210 3 13 1.00 0.0791 527 DY 0.0001830 156.552 527 DY Gráficas de factor de carga-deformación en la dirección 120°:





3.229







3.230





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


210 13 1 102 -552029.8 -913464.6 60.4 Compresión 210 13 1 119 773243 839510.2 92.1 Tensión 210 13 1 199 -399159.7 -792154.5 50.4 Compresión 210 13 1 841 -19034.5 -651519 2.9 Compresión 210 13 1 722 -17820.5 -651519 2.7 Compresión





3.231




CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 150°

11 11 Vto., ole. y corr. H=19.50m 150°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 -29999.998 0.000 0.000 0.000 -1190789.880 0.000 0.000 0.000

9 9 0.000 25000.000 0.000 -992325.000 0.000 0.000 0.000 0.000

10 10 -240994.031 142692.875 -15200.601 -3345979.000 -5768992.500 119259.242 0.000 0.000

11 11 -301536.563 177778.266 -15338.423 -4332461.500 -7513081.500 165446.203 0.000 0.000





3.232



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 150°



10 -100.00 Vto., ole. y corr. H=17.50m 150°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 -80042.539 44460.395 -137.823 -1358604.630 -2518102.750 46186.965





3.233

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -240.99 ton / 100 = -2.41 ton para la dirección X y 142.69 ton / 100 = 1.43 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa -80.04 ton / 100 = -0.80 ton para la dirección X y de 44.46 ton / 100 = 0.45 ton para la dirección Y.



No. DE INCREMENTOS


(TON)






Mecanismo: El factor de carga máximo alcanzado al colapso de la estructura es de 0.71 de la condición de carga 13 en el paso 181 (como se puede observar en el historial de carga).





3.234







4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 60 30 1 10 0.20 0.0293 525 DX 0.0004553 6.802 525 DY

102 50 1 10 0.40 0.0305 527 DX 0.0005418 15.691 525 DY 142 70 1 10 0.60 0.032 484 DX 0.0004961 -28.875 527 DX 182 90 1 10 0.80 0.0178 484 DX 0.0005928 -43.845 527 DX 222 110 1 10 1.00 0.0219 463 DZ 0.0006302 -59.718 527 DX 244 120 1 13 0.10 0.0169 463 DZ 0.0003559 -64.508 527 DX 266 130 1 13 0.20 0.0177 463 DZ 0.0004304 -69.333 527 DX 288 140 1 13 0.30 0.0191 463 DZ 0.0004179 -74.191 527 DX 312 150 1 13 0.40 0.0212 463 DZ 0.0010381 -79.107 527 DX 342 160 1 13 0.50 0.0258 527 DX 0.0006083 -84.110 527 DX 374 170 1 13 0.60 0.0371 484 DX 0.0012771 -89.337 527 DX 752 180 1 13 0.70 7.3602 696 DY 0.1657103 -95.715 527 DX 812 181 1 13 0.71 16.8853 696 DX 0.3411421 -93.472 527 DX 870 181 59 13 0.71 22.5663 696 DX 0.8259178 -94.342 527 DX 872 182 1 13 0.72 51.894 696 DX 1.2925216 -98.100 527 DX

873 182 2 13 0.72 119.375 696 DX 2.7798414 -153.816 696 DX






3.235








3.236




PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


181 13 0.71 102 -774359.9 -913464.6 84.8 Compresión 181 13 0.71 119 593022.9 839510.2 70.6 Tensión 181 13 0.71 199 -5438.2 -792154.5 0.7 Compresión 181 13 0.71 841 -8949.2 -651519 1.4 Compresión 181 13 0.71 722 -18514.3 -651519 2.8 Compresión





3.237




CASE LABEL










10 10 Vto., ole. y corr. H=19.50m 180°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 -29999.998 0.000 0.000 0.000 -1190789.880 0.000 0.000 0.000

9 9 -274027.531 -137.923 -15668.452 31356.176 -6643219.000 -101048.781 0.000 0.000

10 10 -343590.656 -59.445 -15144.641 33983.719 -8634635.000 -112487.445 0.000 0.000





3.238



LOAD LABEL LABEL

CASE

11 11






12 12

10 100.00 Vto., ole. y corr. H=19.50m 180°






CASE LABEL


11 11 0.000 0.000 -209761.594 51591.305 297353.594 0.000

12 12 -99563.133 78.478 523.811 2627.544 -3182206.250 -11438.666





3.239

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -274.03 ton / 100 = -2.74 ton para la dirección X y -0.14 ton / 100 = 0.00 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa -99.56 ton / 100 = -0.99 ton para la dirección X y de 0.08 ton / 100 = 0.00 ton para la dirección Y.



No. DE INCREMENTOS


(TON)



CONDICION 9 EN DIR.Y (viento, oleaje y corriente 0°. H=17.5 m.) -0.14 100 -0.00









3.240






4 2 1 11 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 11 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 11 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 11 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 11 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 60 30 1 9 0.20 0.0316 490 DX 0.0001844 -7.073 727 DX

100 50 1 9 0.40 0.0615 484 DX 0.0001776 -18.648 527 DX 140 70 1 9 0.60 0.0216 484 DX 0.0001822 -34.510 527 DX 180 90 1 9 0.80 0.021 484 DX 0.0001873 -51.322 527 DX 220 110 1 9 1.00 0.0276 484 DX 0.0003289 -69.005 527 DX 244 120 1 12 0.10 0.022 527 DX 0.0001160 -75.464 527 DX 270 130 1 12 0.20 0.0243 527 DX 0.0004360 -81.971 527 DX 302 140 1 12 0.30 0.0263 527 DX 0.0010247 -88.567 527 DX 456 150 1 12 0.40 0.3747 696 DY 0.0204456 -95.202 527 DX 496 151 1 12 0.41 0.9446 696 DY 0.0486897 -95.857 527 DX 536 152 1 12 0.42 2.4931 696 DY 0.1229025 -96.912 527 DX 576 153 1 12 0.43 21.6744 696 DX 0.2023598 -92.425 527 DX 616 154 1 12 0.44 39.0852 696 DX 0.4179827 -100.046 527 DX 654 154 39 12 0.44 15.3904 696 DX 0.5559856 -95.262 527 DX 656 155 1 12 0.45 38.544 696 DX 0.9572027 -101.565 527 DX

657 155 2 12 0.45 80.93 696 DX 2.1218652 -123.465 696 DX






3.241





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


154 12 0.44 102 -808271.6 -913464.6 88.5 Compresión 154 12 0.44 119 309341.8 839510.2 36.8 Tensión 154 12 0.44 199 311861.8 839510.2 37.1 Tensión 154 12 0.44 841 -16339.2 -651519 2.5 Compresión 154 12 0.44 722 -18174.8 -651519 2.8 Compresión

3.10.8.- MECANISMO DE COLAPSO PARA 210°





3.242

Resumen de cargas para 210°



CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 210°

11 11 Vto., ole. y corr. H=19.50m 210°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 -29999.998 0.000 0.000 0.000 -1190789.880 0.000 0.000 0.000

9 9 0.000 -25000.000 0.000 992325.000 0.000 0.000 0.000 0.000

10 10 -241088.672 -141808.078 -14229.404 3399918.250 -5810403.500 -266097.938 0.000 0.000

11 11 -300908.688 -176218.000 -16910.146 4416152.500 -7598591.000 -331684.969 0.000 0.000





3.243



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 210°



10 -100.00 Vto., ole. y corr. H=17.50m 210°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 -79320.023 -43784.926 -2680.742 1388356.380 -2562201.250 -65587.039






3.244

El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -241.09 ton / 100 = 2.41 ton para la dirección X y -141.81 ton / 100 = -1.42 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa -79.32 ton /100 = -0.79 ton para la dirección X y de -43.78 ton /100 = -0.44 ton para la dirección Y.



No. DE INCREMENTOS


(TON)





CONDICION 13 EN DIR.Y (RU H=19.5 m.) -43.78 100 -0.44







3.245




CASE LOAD



4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 60 30 1 10 0.20 0.0338 490 DX 0.0007807 -10.119 484 DY

101 50 1 10 0.40 0.0465 484 DX 0.0007043 -19.489 484 DY 141 70 1 10 0.60 0.0308 527 DX 0.0008155 -29.535 527 DX 182 90 1 10 0.80 0.0174 484 DX 0.0007240 -44.216 527 DX 222 110 1 10 1.00 0.023 525 DZ 0.0007630 -59.657 527 DX 244 120 1 13 0.10 0.0183 525 DZ 0.0006818 -64.955 527 DX 266 130 1 13 0.20 0.0198 525 DZ 0.0003038 -70.276 527 DX 288 140 1 13 0.30 0.0216 525 DZ 0.0003630 -75.633 527 DX 310 150 1 13 0.40 0.0231 525 DZ 0.0003025 -81.028 527 DX 336 160 1 13 0.50 0.0307 484 DX 0.0004317 -86.530 527 DX 364 170 1 13 0.60 0.055 484 DX 0.0009548 -92.288 527 DX 370 172 1 13 0.62 0.0689 524 DX 0.0007703 -93.510 527 DX 392 174 1 13 0.64 0.2908 696 DX 0.0042596 -94.787 527 DX 432 176 1 13 0.66 2.6456 696 DX 0.0207963 -96.332 527 DX 472 178 1 13 0.68 9.484 696 DY 0.1840766 -97.977 527 DX 492 179 1 13 0.69 14.2625 696 DY 0.3860708 -96.776 527 DX 510 179 19 13 0.69 20.5281 696 DY 0.3378398 -96.185 527 DX 512 180 1 13 0.70 44.0783 696 DY 0.7265459 -97.738 527 DX

513 180 2 13 0.70 85.1653 696 DY 2.0328180 -106.812 696 DY





3.246








3.247





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


179 13 0.69 102 -757451.9 -913464.6 82.9 Compresión 179 13 0.69 119 -6260.2 -792154.5 0.8 Compresión 179 13 0.69 199 593270.9 839510.2 70.7 Tensión 179 13 0.69 841 -35128.9 -651519 5.4 Compresión 179 13 0.69 722 -18260.4 -651519 2.8 Compresión





3.248




CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 240°

11 11 Vto., ole. y corr. H=19.50m 240°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 -29999.998 0.000 0.000 0.000 -1190789.880 0.000 0.000 0.000

9 9 0.000 -25000.000 0.000 992325.000 0.000 0.000 0.000 0.000

10 10 -144172.766 -248106.422 -10343.199 5850363.000 -3453113.750 -373919.656 0.000 0.000

11 11 -176555.406 -314676.719 -9439.203 7848155.000 -4397025.000 -482575.531 0.000 0.000





3.249



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 240°



10 -100.00 Vto., ole. y corr. H=17.50m 240°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 -43632.645 -82820.305 903.996 2642803.250 -1390457.380 -108655.883





3.250

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa -144.17 ton / 100 = -1.44 ton para la dirección X y -248.11 ton / 100 = -2.48 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa -43.63 ton /100 = -0.44 ton para la dirección X y de -82.82 ton /100 = -0.83 ton para la dirección Y.



No. DE INCREMENTOS


(TON)











3.251







4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 79 30 1 10 0.20 0.0392 410 DY 0.0011082 -15.876 484 DY

136 50 1 10 0.40 0.0249 484 DY 0.0010289 -31.774 484 DY 196 70 1 10 0.60 0.0314 319 DY 0.0013904 -48.849 484 DY 256 90 1 10 0.80 0.0187 525 DZ 0.0013569 -66.949 484 DY 305 110 1 10 1.00 0.0268 525 DZ 0.0007089 -86.290 484 DY 325 120 1 13 0.10 0.0200 525 DZ 0.0001426 -92.878 484 DY 345 130 1 13 0.20 0.0218 525 DZ 0.0001317 -99.532 484 DY 365 140 1 13 0.30 0.0231 525 DZ 0.0002695 -106.254 484 DY 393 150 1 13 0.40 0.0531 727 DX 0.0017168 -113.097 484 DY 503 160 1 13 0.50 0.8995 727 DY 0.0090552 -120.574 484 DY 703 170 1 13 0.60 15.7422 727 DY 0.1599123 -121.630 484 DY 903 180 1 13 0.70 47.2787 727 DX 0.8515181 -128.580 484 DY

1103 190 1 13 0.80 71.4527 727 DX 1.2287985 -135.092 484 DY 1123 191 1 13 0.81 92.4455 727 DX 1.4265630 -142.521 484 DY 1143 192 1 13 0.82 80.1586 727 DX 1.2324108 -143.395 484 DY 1161 192 19 13 0.82 56.1747 727 DX 0.7627502 -151.005 484 DY 1163 193 1 13 0.83 114.8661 727 DX 1.7298583 -144.739 484 DY

1164 193 2 13 0.83 462.6559 319 DX 84.5166956 7457.388 319 DX





3.252








3.253





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


192 13 0.82 102 -505277.3 -913464.6 55.3 Compresión 192 13 0.82 119 -375424.1 -792154.5 47.4 Compresión 192 13 0.82 199 736072.9 839510.2 87.7 Tensión 192 13 0.82 841 -16776 -651519 2.6 Compresión 192 13 0.82 722 -53508.2 -651519 8.2 Compresión





3.254




CASE LABEL









9 9 Vto., ole.y corr. H=17.50 270°

10 10 Vto., ole. y corr. H=19.50m 270°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 0.000 -25000.000 0.000 992325.000 0.000 0.000 0.000 0.000

9 9 39.868 -287872.500 -5735.627 6606151.500 -20906.990 -392870.406 0.000 0.000

10 10 686.696 -364182.500 -5153.253 8856341.000 -16204.691 -527160.750 0.000 0.000





3.255



LOAD LABEL LABEL

CASE

11 11






12 12

10 100.00 Vto., ole. y corr. H=19.50m 270°


9 -100.00 Vto., ole.y corr. H=17.50 270°




CASE LABEL


11 11 0.000 0.000 -209761.594 51591.305 297353.594 0.000

12 12 646.828 -101310.008 582.373 3242514.750 4702.298 -134290.359





3.256

Secuencia de Carga: Se aplicaron únicamente tres casos de carga de colapso: El primer caso corresponde a la carga gravitacional la cual fue soportada satisfactoriamente por la estructura al 100% y en cuyo caso fue aplicada en 10 incrementos de carga lo cual representa -209.76 ton / 10 = -20.98 ton por cada incremento. Para el segundo caso de carga se consideró la fuerza producida por el viento, corriente y oleaje de 17.50 m, la cual fue aplicada en 100 incrementos de carga lo cual representa 0.04 ton / 100 = 0.00 ton para la dirección X y -287.87 ton / 100 = -2.88 ton para la dirección Y. Y para el tercer caso de carga se consideró la fuerza producida por las cargas de oleaje en cubierta y la fuerza producida por el viento, corriente y oleaje de 19.50 m (y restando las fuerzas correspondientes al segundo caso de carga, previamente aplicadas), la cual fue aplicada en 100 incrementos de carga lo cual representa 0.65 ton / 100 = 0.01 ton para la dirección X y de -101.31 ton / 100 = -1.01 ton para la dirección Y.



No. DE INCREMENTOS


(TON)











3.257







4 2 1 11 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 11 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 11 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 11 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 11 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 79 30 1 9 0.20 0.0449 410 DY 0.0012430 -16.853 484 DY

139 50 1 9 0.40 0.0354 463 DY 0.0010640 -34.165 484 DY 199 70 1 9 0.60 0.0152 410 DY 0.0013197 -53.203 463 DY 253 90 1 9 0.80 0.0184 526 DZ 0.0004631 -74.171 463 DY 293 110 1 9 1.00 0.0278 525 DZ 0.0002480 -97.291 463 DY 313 120 1 12 0.10 0.0243 527 DZ 0.0007267 -104.747 463 DY 333 130 1 12 0.20 0.0266 527 DZ 0.0006823 -112.308 463 DY 353 140 1 12 0.30 0.0434 490 DY 0.0006119 -120.414 483 DY 392 150 1 12 0.40 0.1942 727 DY 0.0007351 -129.521 484 DY 578 160 1 12 0.50 9.5824 727 DX 0.1482137 -137.037 484 DY 778 170 1 12 0.60 100.4106 727 DX 1.5079057 -148.011 484 DY 978 180 1 12 0.70 117.2919 727 DX 1.6926107 -172.828 484 DY

1178 190 1 12 0.80 68.6829 727 DX 0.8234767 -178.473 484 DY 1198 191 1 12 0.81 92.7809 727 DX 1.4908439 -165.451 484 DY 1218 192 1 12 0.82 67.1614 727 DX 0.7635040 -177.168 484 DY 1238 193 1 12 0.83 69.6589 727 DX 0.7445313 -178.937 484 DY 1258 194 1 12 0.84 71.2861 727 DX 0.8282556 -181.828 484 DY 1278 195 1 12 0.85 30.6411 727 DY 0.1384194 -181.922 484 DY 1298 196 1 12 0.86 77.7820 727 DX 0.9517215 -185.384 484 DY 1316 196 19 12 0.86 65.3972 727 DX 0.7157639 -171.474 484 DY 1318 197 1 12 0.87 119.2647 727 DX 1.6645239 -187.997 484 DY

1319 197 2 12 0.87 271.7835 425 DY 90.0498515 5131.207 425 DY





3.258






PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


196 12 0.86 102 -159385.4 -913464.6 17.4 Compresión 196 12 0.86 119 -669035 -792154.5 84.5 Compresión 196 12 0.86 199 657666.3 839510.2 78.3 Tensión 196 12 0.86 841 -19816.3 -651519 3.0 Compresión 196 12 0.86 722 -24912.9 -651519 3.8 Compresión





3.259




CASE LABEL











11 11 Vto., ole. y corr. H=19.50m 292°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 29999.998 0.000 0.000 0.000 1190789.880 0.000 0.000 0.000

9 9 0.000 -25000.000 0.000 992325.000 0.000 0.000 0.000 0.000

10 10 110375.227 -272270.688 -72.201 6232439.000 2577725.750 -386784.469 0.000 0.000

11 11 132832.016 -339344.594 -2121.617 8231855.000 3222718.500 -469586.750 0.000 0.000





3.260



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 292°







CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 30886.791 -84458.914 -2049.416 2689479.250 979604.813 -82802.289





3.261




No. DE INCREMENTOS


(TON)











3.262





CASE LOAD



4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 79 30 1 10 0.20 0.0419 410 DY 0.0012028 16.767 490 DX

137 50 1 10 0.40 0.0221 319 DY 0.0007082 -33.449 484 DY 178 70 1 10 0.60 0.0238 525 DX 0.0007723 -51.733 484 DY 228 90 1 10 0.80 0.0251 463 DY 0.0002652 -71.440 484 DY 268 110 1 10 1.00 0.0448 463 DY 0.0003753 -92.712 484 DY 296 120 1 13 0.10 0.0248 727 DX 0.0014760 -99.401 484 DY 324 130 1 13 0.20 0.0292 527 DZ 0.0009378 -106.194 484 DY 344 140 1 13 0.30 0.0451 463 DY 0.0007514 -113.198 484 DY 374 149 1 13 0.39 0.0610 463 DY 0.0001875 -120.488 484 DY 376 150 1 13 0.40 0.1028 483 DY 0.0010625 -121.276 484 DY 420 160 1 13 0.50 0.1148 727 DY 0.0012791 -130.893 484 DY 563 170 1 13 0.60 16.9802 727 DX 0.2277848 -143.617 484 DY 763 180 1 13 0.70 57.3995 727 DX 0.7244660 -156.536 484 DY 780 180 18 13 0.70 36.4476 727 DX 0.4848338 -151.424 484 DY 781 180 19 13 0.70 76.8841 727 DX 1.0232759 -156.643 484 DY 783 181 1 13 0.71 122.9630 727 DX 1.8356534 -151.290 483 DY

784 181 2 13 0.71 8881.6442 425 DY 149.6096728 8765.856 425 DY





3.263








3.264





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


180 13 0.70 102 120083.6 1038374.3 11.6 Tensión 180 13 0.70 119 -716292.8 -792154.5 90.4 Compresión 180 13 0.70 199 432904.4 839510.2 51.6 Tensión 180 13 0.70 841 -15512.3 -651519 2.4 Compresión 180 13 0.70 722 -37048.1 -651519 5.7 Compresión





3.265




CASE LABEL










10 10 Vto., ole. y corr. H=17.50m 330°

11 11 Vto., ole. y corr. H=19.50m 330°




CASE LABEL


1 1 0.000 0.000 -105155.242 33434.082 119052.133 0.000 175935.188 70779.742

2 2 0.000 0.000 -32673.191 8716.184 62854.477 0.000 0.000 0.000

3 3 0.000 0.000 -9985.375 -62.417 6027.274 0.000 0.000 0.000

4 4 0.000 0.000 -54640.090 2730.811 72227.938 0.000 0.000 0.000

5 5 0.000 0.000 -14921.896 4465.657 8915.115 0.000 0.000 0.000

6 6 0.000 0.000 -15709.974 5783.648 49296.160 0.000 0.000 0.000

7 7 0.000 0.000 -5078.171 3486.165 -3097.685 0.000 0.000 0.000

8 8 29999.998 0.000 0.000 0.000 1190789.880 0.000 0.000 0.000

9 9 0.000 -25000.000 0.000 992325.000 0.000 0.000 0.000 0.000

10 10 247051.984 -146884.422 2871.959 3358368.000 5797577.000 -158210.969 0.000 0.000

11 11 306232.656 -181266.016 4468.359 4350806.000 7545065.500 -198065.188 0.000 0.000





3.266



LOAD LABEL LABEL

CASE

12 12






13 13

11 100.00 Vto., ole. y corr. H=19.50m 330°



10 -100.00 Vto., ole. y corr. H=17.50m 330°




CASE LABEL


12 12 0.000 0.000 -209761.594 51591.305 297353.594 0.000

13 13 78680.680 -43756.598 1596.400 1364560.130 2521502.250 -39854.223





3.267




No. DE INCREMENTOS


(TON)

1.- CONDICION 12 (FUERZAS GRAVITACIONALES) -209.76 10 -20.98 2.- CONDICION 10 EN DIR.X (viento, oleaje y corriente 0°. H=17.5 m.) 247.05 100 2.47









3.268





CASE LOAD



4 2 1 12 0.20 0.0032 463 DX 0.0000156 2.035 490 DX 8 4 1 12 0.40 0.0048 463 DX 0.0000342 4.150 490 DX

12 6 1 12 0.60 0.0067 484 DZ 0.0000651 6.290 490 DX 16 8 1 12 0.80 0.0092 892 DZ 0.0001000 8.453 490 DX 20 10 1 12 1.00 0.0123 892 DZ 0.0001346 10.637 490 DX

****************************************************************************************************************************************** 60 30 1 10 0.20 0.0305 525 DX 0.0004840 22.645 496 DX

101 50 1 10 0.40 0.0322 525 DX 0.0007168 35.669 525 DX 142 70 1 10 0.60 0.0341 490 DX 0.0003189 49.698 525 DX 182 90 1 10 0.80 0.0247 525 DX 0.0002964 64.631 525 DX 224 110 1 10 1.00 0.0365 463 DY 0.0009136 80.509 525 DX 246 120 1 13 0.10 0.0284 463 DX 0.0001113 85.356 525 DX 268 130 1 13 0.20 0.0542 463 DX 0.0002857 90.346 525 DX 300 140 1 13 0.30 0.1028 463 DX 0.0001769 96.494 525 DX 345 150 1 13 0.40 0.1213 463 DX 0.0001007 104.150 525 DX 408 160 1 13 0.50 0.5578 463 DX 0.0005549 114.038 525 DX 532 170 1 13 0.60 0.6869 463 DX 0.0016521 129.973 495 DX 666 180 1 13 0.70 0.5684 463 DX 0.0031206 149.450 463 DX 841 190 1 13 0.80 0.4261 525 DX 0.0008974 181.109 463 DX 853 191 1 13 0.81 0.4200 525 DX 0.0006553 183.355 463 DX 864 192 1 13 0.82 0.4052 525 DX 0.0009987 185.445 463 DX 876 193 1 13 0.83 0.4029 525 DX 0.0005896 187.608 463 DX 896 194 1 13 0.84 0.9075 463 DY 0.0118484 190.314 463 DX 916 195 1 13 0.85 2.4767 727 DX 0.0413937 192.129 463 DX 936 196 1 13 0.86 5.9632 727 DY 0.0922244 193.381 463 DX 956 197 1 13 0.87 14.8888 727 DX 0.2374806 197.592 463 DX 976 198 1 13 0.88 16.1507 727 DX 0.2887875 194.774 463 DX 996 199 1 13 0.89 36.4570 727 DX 0.7328132 197.108 463 DX

1014 199 19 13 0.89 27.8488 727 DY 0.5529279 198.750 463 DX 1016 200 1 13 0.90 63.2997 727 DY 1.2766875 198.986 463 DX

1017 200 2 13 0.90 112.7448 727 DX 2.2633621 209.735 463 DX





3.269








3.270





PASO DE CARGA

CONDICIÓN DE CARGA

FACTOR DE CARGA

JUNTA DE PILOTE

CARGA AXIAL (kg)


199 13 0.89 102 536630.4 1038374.3 51.7 Tensión 199 13 0.89 119 -662869.9 -792154.5 83.7 Compresión 199 13 0.89 199 -18518.8 -792154.5 2.3 Compresión 199 13 0.89 841 -21048.8 -651519 3.2 Compresión 199 13 0.89 722 -41844 -651519 6.4 Compresión





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3.10.13.- RESUMEN DEL RSR PARA ANÁLISIS DE RU

Tabla 3.53.- Resumen de RSR para análisis de RU de todas la direcciones

0 ° 30 ° 68 ° 90 ° 120 ° 150 °

V1 280.87 286.88 291.72 285.12 286.53 280.07Factor1 1.00 1.00 1.00 1.00 1.00 1.00VH=17.50 = (V1 * Factor1) 280.87 286.88 291.72 285.12 286.53 280.07


VRU = (VH=17.50 + VH=19.50) 339.50 378.04 379.68 388.43 380.60 345.08

RSR = (VRU / Vref) 1.73 1.92 1.93 1.97 1.96 1.80

180 ° 210 ° 240 ° 270 ° 292 ° 330 °



VRU = (VH=17.50 + VH=19.50) 1.68 1.78 1.87 1.89 1.79 1.85

RSR = (VRU / Vref) 1.68 1.78 1.87 1.89 1.79 1.85 Por lo tanto, el mínimo RSR obtenido es de 1.68 en la dirección 180°





3.272

3.11.- REVISIÓN DE LA CONEXIÓN PIERNA - CEMENTANTE - PILOTE Revisión para pilote de 91.44 cm (36 plg): Información de la conexión:

Datos de la pierna: Datos del pilote:

Diámetro (DS) = 42.000 plg. = 106.68 cm Diámetro (DP) = 36.000 plg. = 91.44 cmEspesor (tS) = 0.625 plg. = 1.59 cm Espesor (tP) = 1.000 plg. = 2.54 cmEspaciamiento entre llaves (sS) = 6.000 plg. = 15.24 cm Espaciamiento entre llaves (sP) = 6.000 plg. = 15.24 cmAlto de la llave (hS) = 0.250 plg. = 0.635 cm Alto de la llave (hP) = 0.250 plg. = 0.635 cmAncho de la llave (wS) = 0.500 plg. = 1.270 cm Ancho de la llave (wP) = 0.500 plg. = 1.270 cm

Datos del anillo de cementante:

Diámetro (Dg) = 40.75 plg. = 103.51 cmEspesor (tg) = 2.38 plg. = 6.03 cm

Longitud efectiva de contacto entre la pierna y el pilote (Lc) = 144.00 plg. = 365.76 cm

Resistencia a la Compresión del cementante (fcu) = 3600 psi = 253.11 kg/cm² Revisión de las limitantes (Punto 7.4.4.c):

2500 psi (17.25 MPa) ≤ fcu ≤ 16000 psi (110 MPa) ∴ Pasa

Geometría de la pierna:DS/tS ≤ 80 DS/tS = 67.20 ∴ Pasa

Geometría del pilote:DP/tP ≤ 40 DP/tP = 36.00 ∴ Pasa

Geometría del anillo de cementante:7 ≤ Dg/tg ≤ 45 Dg/tg = 17.16 ∴ Pasa

Espaciamiento entre las llaves de cortante (sólo para llaves helicoidales):2.5* ≤ DS/sS ≤ 8 ∴ No aplica2.5* ≤ DP/sP ≤ 8 ∴ No aplica

Relación de las llaves de cortante:hS/sS ≤ 0.10 hS/sS = 0.04 ∴ PasahP/sP ≤ 0.10 hP/sP = 0.04 ∴ Pasa

Factor de forma de las llaves de cortante:1.5 ≤ wS/hS ≤ 3 wS/hS = 2.00 ∴ Pasa1.5 ≤ wP/hP ≤ 3 wP/hP = 2.00 ∴ Pasa

Producto:fcu * (hS/sS) ≤ 800 psi (5.5 MPa) fcu*(hS/sS) = 150 psi ∴ Pasafcu * (hP/sP) ≤ 800 psi (5.5 MPa) fcu*(hP/sP) = 150 psi ∴ Pasa





3.273

Determinación de la máxima fuerza axial permisible:

Para la pierna:fba = 26.7 psi (0.184 MPa) + 0.67 * fcu * (hS/sS) = 127 psi

Para el pilote:fba = 26.7 psi (0.184 MPa) + 0.67 * fcu * (hP/sP) = 127 psi

Usando el valor mínimo de fba = 127 psi

Área:A = π * DP * Lc = 16286.02 plg²

Fba = fba * A = 2072 kips = 940 ton

= 105070.86 cm²

Revisión para pilote de 106.68 cm (42 plg): Información de la conexión:

Datos de la pierna: Datos del pilote:

Diámetro (DS) = 48.000 plg. = 121.92 cm Diámetro (DP) = 42.000 plg. = 106.68 cmEspesor (tS) = 0.750 plg. = 1.91 cm Espesor (tP) = 1.250 plg. = 3.18 cmEspaciamiento entre llaves (sS) = 6.000 plg. = 15.24 cm Espaciamiento entre llaves (sP) = 6.000 plg. = 15.24 cmAlto de la llave (hS) = 0.250 plg. = 0.635 cm Alto de la llave (hP) = 0.250 plg. = 0.635 cmAncho de la llave (wS) = 0.500 plg. = 1.270 cm Ancho de la llave (wP) = 0.500 plg. = 1.270 cm

Datos del anillo de cementante:

Diámetro (Dg) = 46.50 plg. = 118.11 cmEspesor (tg) = 2.25 plg. = 5.72 cm

Longitud efectiva de contacto entre la pierna y el pilote (Lc) = 144.00 plg. = 365.76 cm

Resistencia a la Compresión del cementante (fcu) = 3600 psi = 253.11 kg/cm²





3.274

Revisión de las limitantes (Punto 7.4.4.c):

2500 psi (17.25 MPa) ≤ fcu ≤ 16000 psi (110 MPa) ∴ Pasa

Geometría de la pierna:DS/tS ≤ 80 DS/tS = 64.00 ∴ Pasa

Geometría del pilote:DP/tP ≤ 40 DP/tP = 33.60 ∴ Pasa

Geometría del anillo de cementante:7 ≤ Dg/tg ≤ 45 Dg/tg = 20.67 ∴ Pasa

Espaciamiento entre las llaves de cortante (sólo para llaves helicoidales):2.5* ≤ DS/sS ≤ 8 ∴ No aplica2.5* ≤ DP/sP ≤ 8 ∴ No aplica

Relación de las llaves de cortante:hS/sS ≤ 0.10 hS/sS = 0.04 ∴ PasahP/sP ≤ 0.10 hP/sP = 0.04 ∴ Pasa

Factor de forma de las llaves de cortante:1.5 ≤ wS/hS ≤ 3 wS/hS = 2.00 ∴ Pasa1.5 ≤ wP/hP ≤ 3 wP/hP = 2.00 ∴ Pasa

Producto:fcu * (hS/sS) ≤ 800 psi (5.5 MPa) fcu*(hS/sS) = 150 psi ∴ Pasafcu * (hP/sP) ≤ 800 psi (5.5 MPa) fcu*(hP/sP) = 150 psi ∴ Pasa

Determinación de la máxima fuerza axial permisible:

Para la pierna:fba = 26.7 psi (0.184 MPa) + 0.67 * fcu * (hS/sS) = 127 psi

Para el pilote:fba = 26.7 psi (0.184 MPa) + 0.67 * fcu * (hP/sP) = 127 psi

Usando el valor mínimo de fba = 127 psi

Área:A = π * DP * Lc = 19000.35 plg²

Fba = fba * A = 2417 kips = 1096 ton

= 122582.67 cm²

En resumen, se tiene que: Capacidad máxima en conexión con pilote de 106.68 cm (42 plg) = 1096 ton Capacidad máxima en conexión con pilote de 91.44 cm (36 plg) = 940 ton





3.275

Tabla 3.54.- Revisión de la conexión pierna – cementante – pilotes, en todas las direcciones

Dirección

Pilehead CapacidadUsada (%)

Tensión oCompresión

Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

102 ( = 42") 53.3 T 553873 52.8 T 548082 10.7 C 97708119 ( = 36") 45.2 C 357998 2.4 C 18930 61.7 T 517584199 ( = 36") 45.2 C 358084 87.7 C 694648 97.6 C 772966

0° 30° 68°

Dirección



Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

102 ( = 42") 16.9 C 154530 60.4 C 552030 84.8 C 774360

119 ( = 36") 82.7 T 694036 92.1 T 773243 70.6 T 593023

199 ( = 36") 89.5 C 709091 50.4 C 399160 0.7 C 5438

90° 120° 150°

Dirección



Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

102 ( = 42") 88.5 C 808272 82.9 C 757452 55.3 C 505277

119 ( = 36") 36.8 T 309342 0.8 C 6260 47.4 C 375424

199 ( = 36") 37.1 T 311862 70.7 T 593271 87.7 T 736073

180° 210° 240°

Dirección



Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

CapacidadUsada (%)


Fuerza(kg)

102 ( = 42") 17.4 C 159385 11.6 T 120084 51.7 T 536630

119 ( = 36") 84.5 C 669035 90.4 C 716293 83.7 C 662870

199 ( = 36") 78.3 T 657666 51.6 T 432904 2.3 C 18519

270° 292° 330°

Nota: Se indica con T a la Tensión y con C a la compresión. De la tabla anterior se observan las fuerzas máximas actuantes siguientes: Máxima fuerza actuante en pilote de 106.68 cm (42 plg) = 808.27 ton. Máxima fuerza actuante en pilote de 91.44 cm (36 plg) = 773.24 ton. Comparando las fuerzas actuantes con las resistentes (1096.00 ton y 940.00 ton respectivamente), observamos que en ambos casos la fuerza actuante es menor que la capacidad máxima en la conexión. Cabe aclarar que no se está considerando ningún factor de carga. Por lo anterior, se considera satisfactorio el comportamiento de la conexión pierna-pilote en condiciones de Resistencia Última.





3.276

3.12.- CONCLUSIONES Los resultados obtenidos del análisis por resistencia última muestran que la plataforma Sea Pony Kab-101 cumple las recomendaciones mínimas establecidas por la normatividad aplicable bajo las premisas consideradas. De las direcciones analizadas, se presenta la condición más crítica a 180°, donde se obtiene un RSR = 1.68. Sin embargo, este valor es mayor al mínimo requerido por la NRF-003-PEMEX-2000, que es de 1.50 (ya que se está considerando carga por oleaje en la cubierta). El efecto del pandeo local que muy probablemente se podría presentar en la columna principal, no se toma en cuenta ya que se está considerando que en el interior de dicha columna se encontrará otro conductor. Adicionalmente, el espacio anular entre el conductor y la columna será rellenado con cementante. Sin embargo, y aún cuando no se incluye en esta memoria, se revisó el posible pandeo local de alguno de los otros elementos de la subestructura, encontrándose que este efecto no es significativo. Lo anterior es debido a que en la condición crítica considerando pandeo local, que es la dirección de 68°, se obtiene un RSR mayor al mínimo encontrado (a 180°) sin considerar este efecto. En el caso de la cimentación se encontró que los resultados son satisfactorios siempre y cuando el reporte final de hincado de pilotes correspondiente a la instalación no tenga diferencias con la ingeniería de diseño original, de lo contrario deberá evaluarse la estructura bajo las condiciones reales.





3.277

3.13.- ANEXOS 3.13.1.- Archivo de entrada para análisis de resistencia última dirección 0° A continuación se presenta el archivo de entrada para el análisis de resistencia última utilizado para la dirección 0° LDOPT SF NF+Z 1.030 7.85 -24.00 25.88 ME OPTIONS ME SDUC 1 1 PTPTPTPTPT PT PT GRUP GRUP 10A 27.305 1.270 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 10B 27.305 2.540 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 12A 32.385 0.952 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 12B 32.385 1.696 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP 12C 32.385 2.966 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP 12D 32.385 1.427 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP 24A 60.960 1.587 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 24B 60.960 1.588 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 30A 76.200 1.905 2100.787.54050. 1 1.001.00 0.50N 7.8496.10 GRUP 30A 76.200 1.905 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 30B 76.200 1.905 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 30B 76.200 2.540 2100.787.54050. 1 1.001.00 0.50N 7.8494.57 GRUP 4A 11.430 0.602 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 5A 14.100 1.270 2100.787.53460. 1 1.001.00 0.50N 7.849 GRUP 6A 16.828 0.711 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 6B 16.828 1.097 2100.787.53460. 1 1.001.00 0.50N 7.849 GRUP 8A 21.908 0.793 2100.787.53347. 1 1.001.00 0.50N 7.849 GRUP 8B 21.908 1.270 2100.787.53460. 1 1.001.00 0.50N 7.849 GRUP C10 C10X153 2100.787.53460. 1 1.001.00 N 7.849 GRUP CL2 121.92 1.588 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP CL2 121.92 3.175 2100.787.54050. 1 1.001.00 0.50F 7.8490.76 GRUP CL3 121.92 3.175 2100.787.54050. 1 1.001.00 0.50F 7.8490.76 GRUP CL3 121.92 1.905 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP CL4 121.92 1.905 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP CON 76.200 2.540 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP I12 W12X30 2100.787.53460. 1 1.001.00 N 7.849 GRUP I14 W14X30 2100.787.53460. 1 1.001.00 N 7.849 GRUP LG1 121.92 4.445 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG2 121.92 5.074 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP LG2 121.92 1.905 2100.787.53347. 1 1.001.00 0.50F 7.8493.46 GRUP LG2 121.92 2.540 2100.787.54050. 1 1.001.00 0.50F 7.8490.61 GRUP LG3 121.92 2.540 2100.787.54050. 1 1.001.00 0.50F 7.8490.61 GRUP LG3 121.92 1.905 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP LG4 121.92 1.905 2100.787.53347. 1 1.001.00 0.50F 7.8491.22 GRUP LG4 121.92 2.858 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG5 121.92 2.858 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG5 121.92 5.080 2100.787.54050. 1 1.001.00 0.50F 7.8490.15 GRUP LG6 121.92 5.080 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG7 121.92 5.080 2100.787.54050. 1 1.001.00 0.50F 7.8490.91 GRUP LG7 121.92 2.858 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG8 121.92 2.858 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG9 121.92 2.858 2100.787.54050. 1 1.001.00 0.50F 7.8491.22 GRUP LG9 121.92 1.905 2100.787.54050. 1 1.001.00 0.50F 7.849 GRUP LG9 121.92 1.588 2100.787.53347. 1 1.001.00 0.50F 7.849.762 GRUP P42 106.70 5.674 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP SEA 106.68 5.726 2100.787.53347. 1 1.001.00 0.50F 7.8492.28 GRUP SEA 106.68 4.148 2100.787.53347. 1 1.001.00 0.50F 7.849 GRUP W.B 106.70 3.175 2100.787.53347. 1 1.001.00 0.50F 0.001 GRUP W.C 76.200 2.540 2100.787.53347. 1 1.001.00 0.50F 0.001 GRUP W10 W10X12 2100.787.53460. 1 1.001.00 N 7.849 GRUP W12 W12X30 2100.787.53460. 1 1.001.00 N 7.849 GRUP W14 W14X30 2100.787.53460. 1 1.001.00 N 7.849 GRUP W6 W6X16 2100.787.53460. 1 1.001.00 N 7.849 GRUP W8 W8X21 2100.787.53460. 1 1.001.00 N 7.849 MEMBER MEMBER1 17 479 10A MEMBER OFFSETS 15.65 -17.60 MEMBER1 408 463 10A MEMBER OFFSETS 15.65 -17.60 MEMBER1 426 460 10A MEMBER OFFSETS 15.65 -17.60 MEMBER1 433 482 10A MEMBER OFFSETS 15.65 -17.60 MEMBER1 459 408 10A MEMBER OFFSETS -43.13 43.13 -15.70

MEMBER1 459 426 10A MEMBER OFFSETS -43.13-43.13 -15.70 MEMBER1 459 873 10A MEMBER OFFSETS 43.13-43.13 35.07-33.65 17.18 MEMBER1 459 875 10A MEMBER OFFSETS 43.13 43.13 35.07 33.66 17.18 MEMBER1 873 434 10B 1.001.00 MEMBER OFFSETS 35.07-33.65 17.18 -15.70 MEMBER1 875 18 10B 1.001.00 MEMBER OFFSETS 35.07 33.66 17.18 -15.70 MEMBER1 3 5 12A 0.800.80 MEMBER OFFSETS 52.80-30.48 0.06-40.68 23.49 0.73





3.278

MEMBER1 4 3 12A 0.800.80 MEMBER OFFSETS -40.68-23.48 0.73 52.80 30.48 0.06 MEMBER1 5 4 12A 0.800.80 MEMBER OFFSETS 39.77 -39.76 MEMBER1 101 4 12A 0.800.80 MEMBER OFFSETS 52.80 30.48 87.21-19.86-11.46-33.69 MEMBER1 101 5 12A 0.800.80 MEMBER OFFSETS 52.80-30.48 87.21-19.86 11.47-33.69 MEMBER 251 868 12B MEMBER 253 250 12B MEMBER 253 255 12B MEMBER 255 251 12B MEMBER 256 257 12B MEMBER 257 869 12B MEMBER 259 260 12B MEMBER 260 262 12B MEMBER 868 256 12B MEMBER 869 258 12B MEMBER 258 259 12C MEMBER1 101 199 24A 0.800.80 MEMBER OFFSETS 52.80 34.29 -46.19-26.66 MEMBER1 119 101 24A 0.800.80 MEMBER OFFSETS -46.19 26.67 52.80-34.28 MEMBER1 199 119 24A 0.800.80 MEMBER OFFSETS -53.34 53.34 MEMBER1 6 845 24B MEMBER OFFSETS -61.00 38.10 MEMBER1 101 842 24B 000000000001 MEMBER OFFSETS -61.00 38.10 MEMBER2 201 402 24B MEMBER OFFSETS 61.00 -38.10 MEMBER1 459 850 24B MEMBER OFFSETS -60.96 38.10 MEMBER 538 846 24B MEMBER2 747 848 24B MEMBER OFFSETS 61.00 -38.10 MEMBER2 861 871 24B MEMBER OFFSETS 61.00 -38.10 MEMBER1 119 5 30A MEMBER OFFSETS -46.19 26.67101.53 3.30 -8.25 7.61 MEMBER1 199 4 30A MEMBER OFFSETS -46.19-26.66101.54 3.30 8.26 7.61 MEMBER1 4 6 30B MEMBER OFFSETS 3.30 8.26 7.61 52.80 43.18-86.33 MEMBER1 5 6 30B MEMBER OFFSETS 3.30 -8.25 7.61 52.80-43.17-86.32 MEMBER 542 576 4A MEMBER 543 579 4A MEMBER 544 577 4A MEMBER 549 604 4A MEMBER 571 542 4A MEMBER 571 544 4A MEMBER 578 549 4A MEMBER 596 543 4A MEMBER 600 544 4A MEMBER 609 542 4A MEMBER2 707 864 5A 1.001.00 MEMBER OFFSETS 15.70 MEMBER2 708 867 5A 1.001.00 MEMBER OFFSETS 15.70 MEMBER2 862 16 5A 1.001.00 MEMBER OFFSETS -15.70 MEMBER2 862 17 5A 1.001.00 MEMBER OFFSETS 7.05 -15.65 MEMBER1 862 18 5A 1.001.00 MEMBER OFFSETS 19.10 7.10-27.40 -15.70 MEMBER1 864 18 5A 1.001.00 MEMBER OFFSETS -19.10 7.10 27.40 -15.70 MEMBER2 864 19 5A 1.001.00 MEMBER OFFSETS 7.05 -15.65 MEMBER 864 862 5A 1.001.00 MEMBER2 865 432 5A 1.001.00 MEMBER OFFSETS -15.70 MEMBER2 865 433 5A 1.001.00 MEMBER OFFSETS 7.05 -15.65 MEMBER1 865 434 5A 1.001.00 MEMBER OFFSETS 19.10 7.10-27.40 -15.70 MEMBER1 867 434 5A 1.001.00 MEMBER OFFSETS -19.10 7.10 27.40 -15.70 MEMBER2 867 435 5A 1.001.00 MEMBER OFFSETS 7.05 -15.65 MEMBER 867 865 5A 1.001.00 MEMBER 542 543 6A

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3.279

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3.280

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3.281

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3.282

MEMBER OFFSETS 5.15 5.15 MEMBER1 818 821 W8 MEMBER OFFSETS 5.15 5.15 MEMBER1 820 815 W8 MEMBER OFFSETS 5.15 5.15 MEMBER1 821 708 W8 MEMBER OFFSETS 5.15 5.15 MEMBER1 821 822 W8 MEMBER OFFSETS 5.15 5.15 MEMBER1 822 710 W8 MEMBER OFFSETS 5.15 5.15 MEMBER 822 897 W8 MEMBER 897 898 W8 MEMBER 898 899 W8 MEMBER 899 900 W8 MEMBER 900 901 W8 MEMBER 901 903 W8 MEMBER1 903 709 W8 MEMBER OFFSETS 5.15 5.15 JOINT JOINT 3 0. 0. -12. JOINT 4 7. 4. -12. 25.900 19.100 JOINT 5 7. -4. -12. 25.900-19.100 JOINT 6 0. 0. 0. JOINT 14 0. 0. 15. 69.300 JOINT 15 0. 3. 15. 50.500 69.300 JOINT 16 1. 3. 15. 21.900 50.500 69.300 JOINT 17 2. 3. 15. 43.800 50.500 69.300 JOINT 18 3. 3. 15. 65.700 50.500 69.300 JOINT 19 5. 3. 15. 2.900 50.500 69.300 JOINT 30 -3. 0. 1.-20.000 82.900 JOINT 31 -3. 0. 1.-20.000 85.700 82.900 JOINT 32 -3. 0. 1.-20.000-85.700 82.900 JOINT 33 -2. 1. 1.-77.120 60.000 82.900 JOINT 34 -2. -2. 1.-26.770-26.770 82.900 JOINT 35 0. -3. 1. -40.000 82.900 JOINT 36 0. -3. 1.-85.700-40.000 82.900 JOINT 37 0. -3. 1. 85.700-40.000 82.900 JOINT 38 1. -2. 1. 70.000-94.450 82.900 JOINT 39 -2. -1. 1.-73.385-56.235 82.900 JOINT 40 -1. -2. 1.-56.235-83.385 82.900 JOINT 41 -3. 0. -3.-20.000 -96.200 JOINT 42 -3. 0. -3.-20.000 85.700-96.200 JOINT 43 -3. 0. -3.-20.000-85.700-96.200 JOINT 44 -2. 1. -3.-77.120 60.000-96.200 JOINT 45 -2. -2. -3.-26.770-26.770-96.200 JOINT 46 0. -3. -3.-85.700-40.000-96.200 JOINT 47 -2. -1. -3.-73.385-56.235-96.200 JOINT 48 -1. -2. -3.-56.235-83.385-96.200 JOINT 49 0. -3. -3. -40.000-96.200 JOINT 50 0. -3. -3. 85.700-40.000-96.200 JOINT 51 1. -2. -3. 70.000-94.450-96.200 JOINT 52 -3. 0. 0.-20.000 38.100 JOINT 53 -3. 0. 0.-20.000 85.700 38.100 JOINT 54 -3. 0. 0.-20.000-85.700 38.100 JOINT 55 -2. 1. 0.-77.120 60.000 38.100 JOINT 56 -2. -2. 0.-26.770-26.770 38.100 JOINT 57 0. -3. 0.-85.700-40.000 38.100 JOINT 58 -2. -1. 0.-73.385-56.235 38.100 JOINT 59 -1. -2. 0.-56.235-83.385 38.100 JOINT 60 -3. 0. -1.-20.000 -6.700 JOINT 61 -3. 0. -1.-20.000 85.700 -6.700 JOINT 62 -3. 0. -1.-20.000-85.700 -6.700 JOINT 63 -2. -2. -1.-26.770-26.770 -6.700 JOINT 64 0. -3. -1.-85.700-40.000 -6.700 JOINT 65 -2. -1. -1.-73.385-56.235 -6.700 JOINT 66 -1. -2. -1.-56.235-83.385 -6.700 JOINT 67 -3. 0. -2.-20.000 -51.500 JOINT 68 -3. 0. -2.-20.000 85.700-51.500 JOINT 69 -3. 0. -2.-20.000-85.700-51.500 JOINT 70 -2. 1. -2.-77.120 60.000-51.500 JOINT 71 -2. -2. -2.-26.770-26.770-51.500 JOINT 72 0. -3. -2.-85.700-40.000-51.500 JOINT 73 -2. -1. -2.-73.385-56.235-51.500 JOINT 74 -1. -2. -2.-56.235-83.385-51.500 JOINT 75 0. -3. 0. -40.000 38.100 JOINT 76 0. -3. 0. 85.700-40.000 38.100 JOINT 77 1. -2. 0. 70.000-94.450 38.100 JOINT 78 0. -3. -1. -40.000 -6.700 JOINT 79 0. -3. -1. 85.700-40.000 -6.700 JOINT 80 1. -2. -1. 70.000-94.450 -6.700 JOINT 81 0. -3. -2. -40.000-51.500 JOINT 82 0. -3. -2. 85.700-40.000-51.500

JOINT 83 1. -2. -2. 70.000-94.450-51.500 JOINT 84 -2. 1. -1.-77.120 60.000 -6.700 JOINT 85 -1. 0. -1.-38.560 80.000 -6.650 JOINT 86 -1. -1. -1.-13.385-13.385 -6.650 JOINT 87 0. -1. -1. 85.000-47.225 -6.650 JOINT 101 0. 0. -24. JOINT 102 0. 0. -24. PILEHD JOINT 119 14. -8. -24. 51.900-38.200 PILEHD JOINT 199 14. 8. -24. 51.800 38.100 PILEHD JOINT 201 0. 0. -21. -71.400 JOINT 250 14. 7. -23. 51.800 16.100-10.000 JOINT 251 1. 0. -23. 23.447 -0.048-10.000 JOINT 253 12. 7. -23. 40.662 16.202-10.000 JOINT 255 6. 4. -23. 99.392 3.709-10.000 JOINT 256 1. 0. -16. 23.400 -30.600 JOINT 257 1. 0. -10. 23.400 -28.700 JOINT 258 0. 1. -3. 76.200 29.500-35.300 JOINT 259 0. 1. 2. 76.200 29.500 89.000 JOINT 260 0. 1. 4. 76.200 29.500 41.400 JOINT 262 0. 1. 15. 76.200 29.500 54.300 JOINT 319 14. -8. -18. 51.900-38.200 -5.600 JOINT 399 14. 8. -18. 51.800 38.100 -5.600 JOINT 401 0. -2. -21. -28.600-71.400 JOINT 402 0. -2. -21. -28.600-71.400 JOINT 406 -1. 3. 15.-21.900 50.500 69.300 JOINT 407 -2. 3. 15.-28.600 50.500 69.300 JOINT 408 -3. 3. 15.-65.800 50.500 69.300 JOINT 409 -5. 3. 15. -3.000 50.500 69.300 JOINT 410 -5. 4. 15. -3.000 82.600 69.300 JOINT 411 -3. 4. 15.-65.800 82.600 69.300 JOINT 412 -5. 1. 15. -3.000 52.400 69.300 JOINT 413 -3. 1. 15.-65.800 52.400 69.300 JOINT 414 -2. 1. 15.-28.600 52.400 69.300 JOINT 415 -1. 1. 15.-21.900 52.400 69.300 JOINT 416 -3. 0. 15.-65.800 69.300 JOINT 418 -1. 0. 15.-21.900 69.300 JOINT 421 -5. -1. 15. -3.000-52.400 69.300 JOINT 422 -3. -1. 15.-65.800-52.400 69.300 JOINT 423 -2. -1. 15.-28.600-52.400 69.300 JOINT 424 -1. -1. 15.-21.900-52.400 69.300 JOINT 425 -5. -3. 15. -3.000-50.500 69.300 JOINT 426 -3. -3. 15.-65.800-50.500 69.300 JOINT 427 -2. -3. 15.-28.600-50.500 69.300 JOINT 428 -1. -3. 15.-21.900-50.500 69.300 JOINT 432 1. -3. 15. 21.900-50.500 69.300 JOINT 433 2. -3. 15. 43.800-50.500 69.300 JOINT 434 3. -3. 15. 65.700-50.500 69.300 JOINT 435 5. -3. 15. 2.900-50.500 69.300 JOINT 436 0. -3. 15. 45.700-50.500 69.300 JOINT 437 0. -3. 15.-45.700-50.500 69.300 JOINT 439 0. -1. 15.-45.700-13.000 69.300 JOINT 440 0. -1. 15. 45.700-13.000 69.300 JOINT 444 -1. -1. 15.-21.900-16.800 69.300 JOINT 445 -1. -1. 15.-59.000-52.400 69.300 JOINT 446 -2. -2. 15.-28.600-19.100 69.300 JOINT 447 2. -2. 15. 43.800-33.700 69.300 JOINT 448 1. -1. 15. 21.900-16.900 69.300 JOINT 449 2. 2. 15. 43.800 33.600 69.300 JOINT 450 1. 1. 15. 21.900 16.800 69.300 JOINT 451 -1. 1. 15.-21.900 16.800 69.300 JOINT 452 -2. 2. 15.-28.600 19.000 69.300 JOINT 453 -1. 1. 15.-59.000 52.400 69.300 JOINT 457 0. 0. 15.-45.700-43.800 69.300 JOINT 458 0. 0. 15. 45.700-43.800 69.300 JOINT 459 0. 0. 12. 19.200 JOINT 460 -3. -3. 21.-65.800-50.500 77.000 JOINT 463 -3. 3. 21.-65.800 50.500 77.000 JOINT 464 -3. -2. 21.-65.800-74.300 77.000 JOINT 467 -3. 2. 21.-65.800 74.300 77.000 JOINT 476 -1. 3. 21.-84.500 50.500 77.000 JOINT 477 -1. 2. 21.-84.500 74.300 77.000 JOINT 478 0. 2. 21.-15.300 74.300 77.000 JOINT 479 2. 3. 21. 43.800 50.500 77.000 JOINT 480 2. 2. 21. 43.800 74.300 77.000 JOINT 481 2. -2. 21. 43.800-74.300 77.000 JOINT 482 2. -3. 21. 43.800-50.500 77.000 JOINT 483 2. 4. 21. 43.800 80.000 77.000 JOINT 484 4. 4. 21. 57.200 80.000 77.000 JOINT 485 4. 3. 21. 57.200 50.500 77.000 JOINT 486 4. 2. 21. 57.200 74.300 77.000





3.283

JOINT 487 4. -2. 21. 57.200-74.300 77.000 JOINT 488 4. -3. 21. 57.200-50.500 77.000 JOINT 489 0. 3. 21.-15.300 50.500 77.000 JOINT 490 0. 4. 21.-15.300 80.000 77.000 JOINT 491 -3. -2. 21.-65.800 -5.800 77.000 JOINT 492 -3. -1. 21.-65.800-37.200 77.000 JOINT 493 -3. 0. 21.-65.800-68.600 77.000 JOINT 494 -3. 0. 21.-65.800 77.000 JOINT 495 -3. 0. 21.-65.800 68.500 77.000 JOINT 496 -3. 1. 21.-65.800 37.100 77.000 JOINT 497 -3. 2. 21.-65.800 5.700 77.000 JOINT 498 2. -2. 21. 43.800 -5.800 77.000 JOINT 499 2. -1. 21. 43.800-37.200 77.000 JOINT 500 2. 0. 21. 43.800-68.600 77.000 JOINT 501 2. 0. 21. 43.800 77.000 JOINT 502 2. 0. 21. 43.800 68.500 77.000 JOINT 503 2. 1. 21. 43.800 37.100 77.000 JOINT 504 2. 2. 21. 43.800 5.700 77.000 JOINT 505 4. -2. 21. 57.200 -5.800 77.000 JOINT 506 4. -1. 21. 57.200-37.200 77.000 JOINT 507 4. 0. 21. 57.200-68.600 77.000 JOINT 508 4. 0. 21. 57.200 77.000 JOINT 509 4. 0. 21. 57.200 68.500 77.000 JOINT 510 4. 1. 21. 57.200 37.100 77.000 JOINT 511 4. 2. 21. 57.200 5.700 77.000 JOINT 512 -3. -3. 21. -4.800-50.500 77.000 JOINT 513 -3. -2. 21. -4.800-74.300 77.000 JOINT 514 -3. 2. 21. -4.800 74.300 77.000 JOINT 515 -3. 3. 21. -4.800 50.500 77.000 JOINT 516 1. 2. 21. 82.800 74.300 77.000 JOINT 517 1. 3. 21. 82.800 50.500 77.000 JOINT 518 1. -2. 21. 82.800-74.300 77.000 JOINT 521 1. -3. 21. 82.800-50.500 77.000 JOINT 522 -3. -4. 21.-65.800-11.500 77.000 JOINT 523 2. -4. 21. 43.800-11.500 77.000 JOINT 524 4. -4. 21. 57.200-11.500 77.000 JOINT 525 -3. -4. 21.-65.800-72.500 77.000 JOINT 526 2. -4. 21. 43.800-72.500 77.000 JOINT 527 4. -4. 21. 57.200-72.500 77.000 JOINT 528 -1. -4. 21.-63.900-11.500 77.000 JOINT 529 -1. -4. 21.-63.900-72.500 77.000 JOINT 530 0. -4. 21. 45.700-11.500 77.000 JOINT 531 0. -4. 21. 45.700-72.500 77.000 JOINT 532 0. 0. -1. -98.000 JOINT 533 0. -2. -1. 61.000 -4.500-98.000 JOINT 534 0. 2. -1. 61.000 4.500-98.000 JOINT 536 2. 0. -1. 13.400 -98.000 JOINT 538 0. 0. 2. 74.300 JOINT 539 0. -2. 2. 61.000 -4.500 74.300 JOINT 540 2. 0. 2. 13.400 74.300 JOINT 541 0. 2. 2. 61.000 4.500 74.300 JOINT 542 0. -2. 0. 61.000 -4.500 30.500 JOINT 543 2. 0. 0. 13.400 30.500 JOINT 544 0. 2. 0. 61.000 4.500 30.500 JOINT 549 0. 2. 0.-61.000 4.500 30.500 JOINT 552 0. -3. 0. 91.500 -6.700 30.500 JOINT 554 0. 3. 0. 91.500 6.700 30.500 JOINT 555 0. 3. 0.-61.000 6.700 30.500 JOINT 556 3. 0. 0. 20.100 30.500 JOINT 557 2. 1. 0. 43.900 2.200 30.500 JOINT 558 1. 2. 0. 67.700 4.400 30.500 JOINT 559 1. -2. 0. 67.700 -4.500 30.500 JOINT 560 2. -1. 0. 43.900 -2.300 30.500 JOINT 570 0. -2. 1. 61.000 -4.500 55.400 JOINT 571 2. 0. 1. 13.400 55.400 JOINT 572 0. 2. 1. 61.000 4.500 55.400 JOINT 574 0. 2. 1.-61.000 4.500 55.400 JOINT 576 0. -3. 1. 91.500 -6.700 55.400 JOINT 577 0. 3. 1. 91.500 6.700 55.400 JOINT 578 0. 3. 1.-61.000 6.700 55.400 JOINT 579 3. 0. 1. 20.100 55.400 JOINT 580 2. 1. 1. 43.900 2.200 55.400 JOINT 581 1. 2. 1. 67.700 4.400 55.400 JOINT 582 1. -2. 1. 67.700 -4.500 55.400 JOINT 583 2. -1. 1. 43.900 -2.300 55.400 JOINT 584 1. -1. 1. 17.800-28.300 55.400 JOINT 587 0. 3. 1. 15.300 6.700 55.400 JOINT 594 1. -2. 0. 67.700 -4.500-91.400 JOINT 595 2. -1. 0. 43.900 -2.300-91.400 JOINT 596 3. 0. 0. 20.100 -91.400 JOINT 597 2. 1. 0. 43.900 2.200-91.400 JOINT 598 1. 2. 0. 67.700 4.400-91.400 JOINT 600 0. 3. 0. 91.500 6.700-91.400

JOINT 603 0. 3. 0. 15.300 6.700-91.400 JOINT 604 0. 3. 0.-61.000 6.700-91.400 JOINT 606 3. 0. -1. 20.100 -52.400 JOINT 607 0. 3. -1. 91.500 6.700-52.400 JOINT 608 0. 3. -1.-61.000 6.700-52.400 JOINT 609 0. -3. 0. 91.500 -6.700-91.400 JOINT 610 0. -3. -1. 91.500 -6.700-52.400 JOINT 612 0. 3. 0. 15.300 6.700 30.500 JOINT 613 0. 0. 1. 82.900 JOINT 614 0. 0. -3. -96.200 JOINT 669 -2. 0. 12.-28.600 19.200 JOINT 676 0. 2. 3. 61.000 4.500 4.800 JOINT 677 2. 0. 3. 13.400 4.800 JOINT 678 0. -2. 3. 61.000 -4.500 4.800 JOINT 679 2. 0. -2. 13.400 -20.900 JOINT 680 0. -2. -2. 61.000 -4.500-20.900 JOINT 681 0. 2. -2. 61.000 4.500-20.900 JOINT 695 -2. 0. 0.-28.600 JOINT 696 -2. 0. 15.-28.600 85.000 JOINT 697 -2. 5. 15.-28.600 50.500 69.300 JOINT 698 -1. 5. 15.-21.900 50.500 69.300 JOINT 700 0. 5. 15. 50.500 69.300 JOINT 703 1. 5. 15. 21.900 50.500 69.300 JOINT 704 2. 5. 15. 43.800 50.500 69.300 JOINT 705 3. 5. 15. 65.700 50.500 69.300 JOINT 706 5. 5. 15. 2.900 50.500 69.300 JOINT 707 6. 3. 15. 2.900 50.500 69.300 JOINT 708 6. -3. 15. 2.900-50.500 69.300 JOINT 709 7. 3. 15. 2.900 50.500 69.300 JOINT 710 7. -3. 15. 2.900-50.500 69.300 JOINT 711 6. 1. 15. 2.900 16.700 69.300 JOINT 712 7. 1. 15. 2.900 16.700 69.300 JOINT 715 6. -1. 15. 2.900-16.800 69.300 JOINT 716 7. -1. 15. 2.900-16.800 69.300 JOINT 717 6. 5. 15. 2.900 50.500 69.300 JOINT 718 7. 5. 15. 2.900 50.500 69.300 JOINT 722 0. -2. -24. -28.600 PILEHD JOINT 723 0. -2. 2. -28.600 74.300 JOINT 725 0. -2. 10. -28.600 66.800 JOINT 727 0. -2. 15. -28.600 85.000 JOINT 732 5. 1. 15. 2.900 16.700 69.300 JOINT 734 5. -1. 15. 2.900-16.800 69.300 JOINT 747 0. 0. 10. 66.800 JOINT 812 -3. -5. 15.-65.800-52.300 69.300 JOINT 813 -2. -5. 15.-28.600-52.300 69.300 JOINT 814 -1. -5. 15.-21.900-52.300 69.300 JOINT 815 1. -5. 15. 21.900-52.300 69.300 JOINT 816 2. -5. 15. 43.800-52.300 69.300 JOINT 817 3. -5. 15. 65.700-52.300 69.300 JOINT 818 5. -5. 15. 2.900-52.300 69.300 JOINT 820 0. -5. 15. -52.300 69.300 JOINT 821 6. -5. 15. 2.900-52.300 69.300 JOINT 822 7. -5. 15. 2.900-52.300 69.300 JOINT 823 0. -3. 15. -50.500 69.300 JOINT 841 -2. 0. -24.-28.600 PILEHD JOINT 842 -2. 0. -24.-28.600 JOINT 845 -2. 0. 0.-28.600 JOINT 846 0. -2. 2. -28.600 74.300 JOINT 848 0. -2. 10. -28.600 66.800 JOINT 850 -2. 0. 12.-28.600 19.200 JOINT 855 2. 0. 15. 43.800-52.050 69.300 JOINT 856 3. 0. 15. 65.700-52.050 69.300 JOINT 857 2. 0. 15. 43.800 52.050 69.300 JOINT 858 3. 0. 15. 65.700 52.050 69.300 JOINT 859 3. -1. 15. 65.700-16.840 69.300 JOINT 860 3. 1. 15. 65.700 16.830 69.300 JOINT 861 0. 0. -6. -40.200 JOINT 862 2. 3. 14. 43.800 50.500 77.950 JOINT 864 5. 3. 14. 2.900 50.500 77.950 JOINT 865 2. -3. 14. 43.800-50.500 77.950 JOINT 867 5. -3. 14. 2.900-50.500 77.950 JOINT 868 1. 0. -22. 23.400 -32.500 JOINT 869 0. 1. -7. 76.200 29.500-78.700 JOINT 871 0. -2. -6. -28.600-40.200 JOINT 872 0. -2. -6. -28.600-40.200 JOINT 873 3. -3. 15. 21.955 -8.573 27.421 JOINT 874 0. 0. 15. 27.400 JOINT 875 3. 3. 15. 21.955 8.573 27.421 JOINT 880 -2. 0. 15.-97.600 69.000 69.300 JOINT 881 -2. 0. 15.-97.600-69.000 69.300 JOINT 882 -1. 0. 15.-59.600 69.000 69.300





3.284

JOINT 883 -1. 0. 15.-59.600-69.000 69.300 JOINT 884 -2. 0. 15.-28.600 69.000 69.300 JOINT 885 -2. 0. 15.-28.600-69.000 69.300 JOINT 886 -2. 0. 15.-97.600 69.300 JOINT 887 -1. 0. 15.-59.600 69.300 JOINT 889 0. -3. 15. 75.000 -3.600 69.300 JOINT 890 0. -3. 15.-75.000 -3.600 69.300 JOINT 891 0. -1. 15.-75.000-53.600 69.300 JOINT 892 0. -1. 15. 75.000-53.600 69.300 JOINT 893 0. -3. 15.-45.700 -3.600 69.300 JOINT 894 0. -3. 15. 45.700 -3.600 69.300 JOINT 895 0. -1. 15.-45.700-53.600 69.300 JOINT 896 0. -1. 15. 45.700-53.600 69.300 JOINT 897 8. -5. 15. 2.900-52.300 69.300 JOINT 898 8. -3. 15. 2.900-50.500 69.300 JOINT 899 8. -1. 15. 2.900-16.800 69.300 JOINT 900 8. 1. 15. 2.900 16.700 69.300 JOINT 901 8. 1. 15. 2.900 82.500 69.300 JOINT 903 7. 1. 15. 2.900 82.300 69.300 AREA AREAX1 3.0 2.44 -4.26 16.85 1.00 816 433 F AREAX2 42.6 2.44 0.00 18.85 1.50 433 447 857 449 503 482 F AREAX3 4.0 2.44 4.51 16.85 1.00 17 704 F AREAY1 12.2 -0.61 -3.51 16.85 1.00 426 427 428 823 432 433 F AREAY2 11.2 4.73 -3.51 16.85 1.00 433 434 435 708 710 898 F AREAY3 12.2 -0.61 3.51 16.85 1.00 408 407 406 15 16 17 F AREAY4 9.2 4.73 3.51 16.85 1.00 17 18 19 707 709 F CDM CDM AP MGROV MGROV -24.000 -20.000 4.000 1.400 MGROV -20.000 1.000 6.000 1.400 GRPOV GRPOV W.C 0.001 0.001 0.001 0.001 0.001 GRPOV W.B 0.001 0.001 0.001 0.001 0.001 GRPOV W14 0.001 0.001 GRPOV W12 0.001 0.001 GRPOV W10 0.001 0.001 GRPOV W8 0.001 0.001 GRPOV W6 0.001 0.001 GRPOV C10 0.001 0.001 GRPOV P42 .010.010.010.010 REPORT REPLBL PIERNAS DETALLES DE PIERNAS REPGRP LG1 LG2 LG3 LG4 LG5 LG6 LG7 LG8 LG9 SEA REPORT REPLBL DIAGS DIAGONALES Y PLANTAS REPGRP 12A 24A 30A 30B DUMMY DEF KEEP 613 614 DELETE 30 31 32 33 34 35 36 37 38 39 40 41 42 43 DELETE 44 45 46 47 48 49 50 51 52 53 54 55 56 57 DELETE 58 59 60 61 62 63 64 65 66 67 68 69 70 71 DELETE 72 73 74 75 76 77 78 79 80 81 82 83 84 85 DELETE 86 87 DUMMY ATRAC KEEP 538 532 DELETE 676 541 677 540 678 539 534 681 536 679 533 680 578 587 DELETE 577 581 580 579 583 582 576 570 584 571 572 574 555 612 DELETE 554 558 557 556 560 559 552 542 543 544 549 604 603 600 DELETE 598 597 596 595 594 609 606 607 608 610 DELGRP 12B 12C DELJNT 250 101 199 253 199 119 255 101 199 251 101 199 DELJNT 868 101 201 256 201 3 257 3 861

869 3 861 DELJNT 258 614 532 259 538 747 260 538 747 262 874 14 LOAD LOADCN 1 LOADLB 1 Peso Propio y Flotacion DEAD DEAD -Z M LOADCN 2 LOADLB 2 C. M. en Cub. +15.850 y subestruct. LOAD 411 -203.00 GLOB JOIN ESCPPHP LOAD 408 -203.00 GLOB JOIN ESCPPHP LOAD 857 -94.500 GLOB JOIN ESCEMPP LOAD 858 -94.500 GLOB JOIN ESCEMPP LOAD 538 -189.00 GLOB JOIN ESCEMPP LOAD Z 199 4 6.75213-245.00 GLOB CONC ANODOS LOAD Z 4 6 6.78648-245.00 GLOB CONC ANODOS LOAD Z 5 6 6.78657-245.00 GLOB CONC ANODOS LOAD Z 4 3 3.65131-245.00 GLOB CONC ANODOS LOAD Z 3 5 3.65129-245.00 GLOB CONC ANODOS LOAD Z 5 4 3.79335-245.00 GLOB CONC ANODOS LOAD Z 101 199 7.81024-245.00 GLOB CONC ANODOS LOAD Z 199 119 7.84810-245.00 GLOB CONC ANODOS LOAD Z 119 101 7.81092-245.00 GLOB CONC ANODOS LOAD Z 119 5 6.75251-245.00 GLOB CONC ANODOS LOAD Z 119 101 0.53300-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 199 119 0.53300-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 101 199 0.61000-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 119 101 13.1000-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 199 119 13.1000-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 101 199 13.1000-63.3202.44000-63.320 GLOB UNIF P-BASE LOAD Z 410 409 -68.600 -68.600 GLOB UNIF CM15850 LOAD Z 408 411 -68.600 -68.600 GLOB UNIF CM15850 LOAD Z 407 697 -68.600 -68.600 GLOB UNIF CM15850 LOAD Z 426 812 -68.600 -68.600 GLOB UNIF CM15850 LOAD Z 409 412 -137.20 -137.20 GLOB UNIF CM15850 LOAD Z 412 421 -68.600 -68.600 GLOB UNIF CM15850 LOAD Z 426 422 -137.20 -137.20 GLOB UNIF CM15850 LOAD Z 422 416 -137.20 -137.20 GLOB UNIF CM15850 LOAD Z 416 413 -137.20 -137.20 GLOB UNIF CM15850 LOAD Z 413 408 -137.20 -137.20 GLOB UNIF CM15850 LOAD Z 813 427 -122.00 -122.00 GLOB UNIF CM15850 LOAD Z 446 427 -122.00 -122.00 GLOB UNIF CM15850 LOAD Z 423 446 -122.00 -122.00 GLOB UNIF CM15850 LOAD Z 414 884 -122.00 -122.00 GLOB UNIF CM15850 LOAD Z 452 414 -122.00 -122.00 GLOB UNIF CM15850





3.285

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GLOB UNIF CVHELIP LOAD Z 502 495 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 508 501 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 501 494 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 507 500 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 500 493 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 506 499 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 499 492 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 505 498 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 498 491 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 487 481 -201.00 -201.00 GLOB UNIF CVHELIP LOAD Z 518 481 -201.00 -201.00 GLOB UNIF CVHELIP LOAD Z 513 518 -201.00 -201.00 GLOB UNIF CVHELIP LOAD Z 464 513 -201.00 -201.00 GLOB UNIF CVHELIP LOAD Z 488 482 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 521 482 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 512 521 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 460 512 -134.00 -134.00 GLOB UNIF CVHELIP LOAD Z 523 524 -119.00 -119.00 GLOB UNIF CVHELIP LOAD Z 530 523 -119.00 -119.00 GLOB UNIF CVHELIP LOAD Z 528 530 -119.00 -119.00 GLOB UNIF CVHELIP LOAD Z 522 528 -119.00 -119.00 GLOB UNIF CVHELIP LOAD Z 526 527 -60.000 -60.000 GLOB UNIF CVHELIP LOAD Z 531 526 -60.000 -60.000 GLOB UNIF CVHELIP LOAD Z 529 531 -60.000 -60.000 GLOB UNIF CVHELIP LOAD Z 525 529 -60.000 -60.000 GLOB UNIF CVHELIP LOADCN 6 LOADLB 6 C. de Equipos en Cub. Elev. +15.850 LOAD Z 734 435 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 734 732 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 19 732 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 860 18 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 858 860 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 856 858 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 859 856 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 434 859 -286.00 -286.00 GLOB UNIF TRAM-DIA LOAD Z 407 697 -97.6001.02500-97.560 GLOB UNIF RADIO LOAD Z 406 698 -97.6001.02500-97.560 GLOB UNIF RADIO LOAD Z 406 698 1.39000-123.00 -123.00 GLOB UNIF JBPLC LOAD Z 15 700 1.39000-123.00 -123.00 GLOB UNIF JBPLC LOAD Z 15 700 0.50000-444.45 -444.45 GLOB UNIF FA-1500 LOAD Z 16 703 0.50000-444.45 -444.45 GLOB UNIF FA-1500 LOAD Z 17 704 0.50000-444.45 -444.45 GLOB UNIF FA-1500





3.289

LOAD Z 17 704 1.39000-123.00 -123.00 GLOB UNIF JBTCOM LOAD Z 18 705 1.39000-123.00 -123.00 GLOB UNIF JBTCOM LOAD Z 18 705 1.39000-273.23 -273.23 GLOB UNIF RACKINS LOAD Z 19 706 1.39000-273.23 -273.23 GLOB UNIF RACKINS LOAD Z 707 717 1.39000-273.23 -273.23 GLOB UNIF RACKINS LOAD Z 707 717 0.97000-145.63 -145.63 GLOB UNIF JBPLCSE LOAD Z 709 718 0.97000-145.63 -145.63 GLOB UNIF JBPLCSE LOAD Z 707 709 -900.00 -900.00 GLOB UNIF BANBAT LOAD Z 712 711 -900.00 -900.00 GLOB UNIF BANBAT LOAD Z 712 711 -400.00 -400.00 GLOB UNIF CONBAKER LOAD Z 716 715 -400.00 -400.00 GLOB UNIF CONBAKER LOAD Z 716 715 -400.00 -400.00 GLOB UNIF TAINTER LOAD Z 708 710 -400.00 -400.00 GLOB UNIF TAINTER LOAD Z 816 433 -535.721.40000-535.72 GLOB UNIF PA-1100 LOAD Z 817 434 -535.721.40000-535.72 GLOB UNIF PA-1100 LOAD Z 815 432 -444.451.50000-444.45 GLOB UNIF MICROTUB LOAD Z 820 823 -444.451.50000-444.45 GLOB UNIF MICROTUB LOAD Z 814 428 -444.451.50000-444.45 GLOB UNIF MICROTUB LOAD Z 813 427 -384.621.30000-384.62 GLOB UNIF INYQUIM LOAD Z 814 428 -384.621.30000-384.62 GLOB UNIF INYQUIM LOAD Z 820 823 -384.621.30000-384.62 GLOB UNIF INYQUIM LOADCN 7 LOADLB 7 Carga de Helicoptero LOAD Z 494 495 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 493 494 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 492 493 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 491 492 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 501 502 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 500 501 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 499 500 -925.66 -925.66 GLOB UNIF HELI-212 LOAD Z 498 499 -925.66 -925.66 GLOB UNIF HELI-212

LOADCN 8 1000.00 LOADLB 8 Cargas de oleaje en Cub. LOAD 14 30.0000 GLOB JOIN OLAENCUB LOADCN 9 LOADLB 9 Vto., oleaje y corr. H=17.5m +X WIND WIND1 W 40.92 10.00 0.0 26.01AP08X1X2X3 WAVE WAVE0.85STRE 17.50 26.01 12.55 0.00 L -50.00 1.00 99MM 4 1 3 9 CURR CURR 5.000 1.070 0.000 BC NL WDP AWP CURR 50.000 1.120 0.000 CURR 100.000 1.170 0.000 LOADCN 10 LOADLB 10 Vto., ole. y corr. H=19.50m +X WIND WIND1 W 45.82 10.00 0.0 26.12AP08X1X2X3 WAVE WAVE0.85STRE 19.50 26.12 13.32 0.00 L -50.00 1.00 99MM 4 1 3 9 CURR CURR 5.000 1.220 0.000 BC NL WDP AWP CURR 50.000 1.270 0.000 CURR 100.000 1.320 0.000 LCOMB LCOMB 11 1 1.050 2 1.000 3 1.000 40.7500 6 1.000 LCOMB 12 10 1.000 8 1.000 9-1.000 END

3.13.2.- Archivo de entrada para calcular el mecanismo de colapso dirección 0° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 11 10 0.0 1.0 9 100 0.0 1.0 12 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.3.- Archivo de entrada para calcular el mecanismo de colapso dirección 30° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END





3.290

3.13.4.- Archivo de entrada para calcular el mecanismo de colapso dirección 68° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.5.- Archivo de entrada para calcular el mecanismo de colapso dirección 90° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 11 10 0.0 1.0 9 100 0.0 1.0 12 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.6.- Archivo de entrada para calcular el mecanismo de colapso dirección 120° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.7.- Archivo de entrada para calcular el mecanismo de colapso dirección 150° CLPOPT 60 8 40 NSCN JFPPJS 0.10.001 0.011000.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.8.- Archivo de entrada para calcular el mecanismo de colapso dirección 180° CLPOPT 40 8 40 NSCN JFPPJS 0.10.001 0.015000.0.005 CLPRPT P0M0R0 LDSEQ LDS1 11 10 0.0 1.0 9 100 0.0 1.0 12 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.9.- Archivo de entrada para calcular el mecanismo de colapso dirección 210° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.10.- Archivo de entrada para calcular el mecanismo de colapso dirección 240° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.11.- Archivo de entrada para calcular el mecanismo de colapso dirección 270° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 11 10 0.0 1.0 9 100 0.0 1.0 12 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A





3.291

END 3.13.12.- Archivo de entrada para calcular el mecanismo de colapso dirección 292° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.13.13.- Archivo de entrada para calcular el mecanismo de colapso dirección 330° CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 CLPRPT P0M0R0 LDSEQ LDS1 12 10 0.0 1.0 10 100 0.0 1.0 13 100 0.0 1.0 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A END 3.14.- ARCHIVO DE RESULTADOS, DIRECCIÓN 0° A continuación se presenta el archivo de resultados correspondiente a la dirección 0°.

3.14.1.- Listado de colapso (CLPLIST) *** INPUT ECHO REPORT *** 1 2 3 4 5 6 7 8 LINE 12345678901234567890123456789012345678901234567890123456789012345678901234567890 1 CLPOPT 20 8 40 NSCN JFPPJS 0.10.001 0.01 900.0.005 2 CLPRPT P0M0R0 3 LDSEQ LDS1 11 10 1.0 9 100 1.0 12 100 1.0 4 GRPELA W.B W.C CON 24B I12 I14 W6 W8 W12 W14 10A 5A 5 END PROBLEM PARAMETERS NO. JOINTS 204 NO. BEAMS 337 NO. PLATES 0 NO. CONDITIONS 12 PRINT CONTROL 0 NO. SPRUNG JOINTS 0 NO. REDUCED DOF 1224 NO. RETAINED DOF 0 NO. RECORDS 1 MAX. NO. ROWS / RECORD 1224 NO. SHELL ELEMENTS 0 *** WARNING - MEMBER 479- 483 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 28.97 28.76 CM**2 TORSION MOMENT OF INERTIA . 8.74 7.52 CM**4 Y-Y MOMENT OF INERTIA ..... 2805.41 2792.60 CM**4 Z-Z MOMENT OF INERTIA ..... 94.90 118.17 CM**4 *** WARNING - MEMBER 880- 884 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 881- 886 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 882- 887 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 883- 885 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES





3.292

MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 884- 882 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 885- 881 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 886- 880 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 *** WARNING - MEMBER 887- 883 HAS CROSS-SECTION PROPERTIES THAT DIFFER FROM THE CALCULATED PROPERTIES MEMBER HAS BEEN CONVERTED TO ELASTIC ** INPUT ** CALCULATED AXIAL AREA ................ 22.84 22.31 CM**2 TORSION MOMENT OF INERTIA . 2.08 2.28 CM**4 Y-Y MOMENT OF INERTIA ..... 2239.33 2171.43 CM**4 Z-Z MOMENT OF INERTIA ..... 90.74 90.69 CM**4 * * * * * * * * * * * * * * * * * * * * * * * * * * * * P S I * * PILE-SOIL INTERACTION * * STRUCTURAL ANALYSIS * * * * DEVELOPED AND SUPPORTED * * BY * * ENGINEERING DYNAMICS INC. * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * O P T I O N S * * ANALYSIS UNITS . . . . . . . . . METRIC-KG VERTICAL COORDINATE . . +Z CONVERGENCE -DISPLACEMENT . . . . 0.00254 CM -ROTATION . . . . . . 0.00010 RAD -FORCE . . . . . . . 0.50000 PERCENT ITERATIONS . . . . . . 20 MAX PILE INCREMENTS . . . . 100 PILE MATERIAL DENSITY 7.850 SPG EXECUTE LINEAR STRUCTURE STIFFNESS REDUCTION LINEAR STRUCTURE FORCE REDUCTION PILEHEAD STIFFNESS TABLE GENERATION PILE-TO-STRUCTURE FOUNDATION ANALYSIS LINEAR STRUCTURE ANALYSIS PILE ANALYSIS SAVE LINEAR STRUCTURE STIFFNESS REDUCTION RECOVER PRINT PILE SUMMARY ONLY * * P I L E G R O U P D E S C R I P T I O N * * LABELS TUBE SECTION MATERIAL PROPERTIES SEGMENT SURFACE DIMENSIONS T BEARING GROUP SECTION O.D. TW E*10-3 G*10-3 FY LENGTH AS BS FACTOR AREA CM CM KGSCM KGSCM KGSCM M CM CM M**2 P42 106.70 5.670 2100.00 787.50 3347.00 3.05 106.70 5.67 1.00 0.00 P42 106.70 4.410 2100.00 787.50 3347.00 35.05 106.70 4.41 1.00 0.00 P42 106.70 5.670 2100.00 787.50 3347.00 1.52 106.70 5.67 1.00 0.00 P42 106.70 4.410 2100.00 787.50 3347.00 13.72 106.70 4.41 1.00 0.00 P42 106.70 5.670 2100.00 787.50 3347.00 1.52 106.70 5.67 1.00 0.89 P36 91.40 2.540 2100.00 787.50 3347.00 3.05 91.40 2.54 1.00 0.00 P36 91.40 1.900 2100.00 787.50 3347.00 32.00 91.40 1.90 1.00 0.00 P36 91.40 2.540 2100.00 787.50 3347.00 1.52 91.40 2.54 1.00 0.00 P36 91.40 1.900 2100.00 787.50 3347.00 16.76 91.40 1.90 1.00 0.00 P36 91.40 2.540 2100.00 787.50 3347.00 1.52 91.40 2.54 1.00 0.66 C30 76.20 2.540 2100.00 787.50 3347.00 56.30 76.20 2.54 1.00 0.46 * * P I L E D E S C R I P T I O N * * * PILE JOINTS * GROUP * * BATTER INCREMENTS * * CHORD SOIL TABLES





3.293

HEAD BATTER LABEL X Y Z ANGLE XZ XY M M M DEG 102 201 P42 0.00 SOL1 119 319 P36 0.00 SOL2 199 399 P36 0.00 SOL2 841 695 C30 0.00 SOL3 722 723 C30 0.00 SOL3 * * AXIAL SOIL STIFFNESS TABLE * * SOIL TABLE ID SOL1 NUMBER OF SOIL STRATA = 56 NUMBER OF POINTS/CURVE = 30 RES. AXIAL

** SACS COLLAPSE PILE DETAIL REPORT ** *** FINAL *** PILEHEAD JOINT 102 **** DEFLECTIONS **** ***** ROTATIONS ***** ************** ELASTIC INTERNAL LOADS *************** PLASTIC INCR DISTANCE X Y Z X Y Z FX FY FZ MX MY MZ RATIO M CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 1 0.00 -0.481 19.091 0.000 0.0014 -0.0001 -0.0069 553865.16135652.91 1016.38 1657.2****************** 0.000 2 0.51 -0.477 18.708 0.006 0.0014 -0.0001 -0.0078 552454.74133569.57 1008.57 1564.3****************** 0.000 3 1.02 -0.473 18.284 0.012 0.0014 -0.0001 -0.0085 551259.48131284.28 1000.47 1486.0****************** 0.000 4 1.53 -0.469 17.824 0.018 0.0014 -0.0001 -0.0092 549984.26128822.41 991.94 1420.8****************** 0.000 5 2.03 -0.467 17.330 0.022 0.0014 -0.0001 -0.0098 548629.43126190.57 982.89 1367.2-955166.7********* 0.000 6 2.54 -0.465 16.807 0.026 0.0014 -0.0001 -0.0104 547195.26123395.68 973.23 1323.6-905213.1********* 0.000 7 3.05 -0.463 16.257 0.030 0.0014 -0.0001 -0.0109 545717.65120275.28 961.60 1298.4-855750.2********* 0.000 8 3.60 -0.460 15.634 0.033 0.0014 -0.0001 -0.0114 544156.52116783.63 948.17 1263.7-803097.0********* 0.000 9 4.15 -0.458 14.982 0.035 0.0014 -0.0001 -0.0119 542336.71112342.20 932.02 1236.7-751178.6********* 0.000 10 4.69 -0.456 14.308 0.037 0.0014 0.0000 -0.0123 540259.31106984.12 912.79 1215.7-700144.4********* 0.000 11 5.24 -0.455 13.615 0.039 0.0014 0.0000 -0.0126 538059.57101347.00 891.90 1199.7-650163.2********* 0.000 12 5.79 -0.454 12.909 0.040 0.0014 0.0000 -0.0128 535909.39 96201.89 871.64 1187.9-601325.9********* 0.000 13 6.34 -0.454 12.193 0.040 0.0014 0.0000 -0.0130 533814.42 91550.80 852.25 1178.9-553598.37557457.6 0.000 14 6.88 -0.454 11.472 0.040 0.0014 0.0000 -0.0130 531842.70 87591.29 834.65 1171.6-506932.42544482.1 0.000 15 7.43 -0.453 10.750 0.039 0.0014 0.0000 -0.0130 529994.83 84299.62 819.03 1165.0-461230.4********* 0.000 16 7.98 -0.453 10.029 0.039 0.0014 0.0000 -0.0130 528185.26 81374.01 804.48 1157.9-416383.8********* 0.000 17 8.53 -0.453 9.314 0.038 0.0014 0.0000 -0.0128 526068.86 77705.90 786.67 1148.7-372333.7********* 0.000 18 9.07 -0.452 8.609 0.036 0.0014 0.0000 -0.0126 523659.69 73346.00 765.56 1136.8-329258.9********* 0.000 19 9.62 -0.451 7.915 0.035 0.0014 0.0000 -0.0124 521208.57 68699.90 742.72 1122.1-287339.8********* 0.000 20 10.17 -0.450 7.237 0.033 0.0014 0.0000 -0.0121 518718.64 63833.90 718.35 1104.0-246671.7********* 0.000 21 10.72 -0.448 6.577 0.031 0.0014 0.0000 -0.0117 516232.99 59134.89 694.22 1082.6-207337.5********* 0.000 22 11.26 -0.446 5.939 0.029 0.0014 0.0000 -0.0113 513755.86 54616.40 670.45 1057.8-169324.6********* 0.000 23 11.81 -0.444 5.324 0.026 0.0014 0.0000 -0.0109 511289.07 50270.45 647.06 1029.3-132613.1********* 0.000 24 12.36 -0.441 4.735 0.024 0.0014 0.0000 -0.0104 508834.45 46088.58 624.06 997.1 -97182.4********* 0.000 25 12.91 -0.437 4.173 0.022 0.0014 0.0000 -0.0099 506393.78 42061.94 601.46 961.4 -63010.8********* 0.000 26 13.46 -0.433 3.642 0.020 0.0014 0.0000 -0.0093 503968.92 38198.75 579.35 922.1 -30076.5********* 0.000 27 14.00 -0.428 3.142 0.017 0.0014 0.0000 -0.0088 501562.16 34567.06 558.14 879.5 1646.8********* 0.000 28 14.55 -0.423 2.676 0.015 0.0014 0.0000 -0.0081 498337.06 29521.74 528.64 833.0 32209.0********* 0.000 29 15.10 -0.417 2.244 0.013 0.0014 0.0000 -0.0075 495130.63 24813.57 500.57 783.7 61155.8********* 0.000 30 15.65 -0.411 1.849 0.011 0.0014 0.0000 -0.0068 491944.61 20413.05 473.84 732.1 88565.7********* 0.000 31 16.19 -0.404 1.490 0.009 0.0014 0.0000 -0.0062 488780.56 16290.04 448.34 678.5 114511.9********* 0.000 32 16.74 -0.397 1.169 0.007 0.0014 0.0000 -0.0055 485640.71 12567.35 424.87 623.3 139061.9********* 0.000 33 17.29 -0.390 0.887 0.006 0.0014 0.0000 -0.0048 482526.36 9287.67 403.78 567.0 162326.7********* 0.000 34 17.84 -0.382 0.644 0.004 0.0014 0.0000 -0.0041 475538.47-26108.26 176.65 498.2 184436.9********* 0.000 35 18.38 -0.374 0.443 0.003 0.0014 0.0000 -0.0034 468395.30-56620.89 -24.64 434.5 194109.8********* 0.000 36 18.93 -0.366 0.283 0.002 0.0014 0.0000 -0.0027 461082.12-81928.22 -198.06 379.2 192760.9********* 0.000 37 19.48 -0.358 0.161 0.001 0.0014 0.0000 -0.0021 453582.47********* -343.26 334.3 181915.7********* 0.000 38 20.03 -0.349 0.072 0.001 0.0014 0.0000 -0.0015 445882.86********* -438.87 301.1 163120.0********* 0.000 39 20.58 -0.341 0.013 0.000 0.0014 0.0000 -0.0011 435886.32********* -504.09 277.1 139089.0********* 0.000 40 21.12 -0.333 -0.023 0.000 0.0014 0.0000 -0.0007 425537.91********* -496.30 261.8 111486.6********* 0.000 41 21.67 -0.325 -0.041 0.000 0.0014 0.0000 -0.0004 414830.04-96147.00 -445.89 252.0 84311.3********* 0.000 42 22.22 -0.318 -0.047 0.000 0.0014 0.0000 -0.0002 403763.77-80275.87 -376.10 245.4 59896.0********* 0.000 43 22.77 -0.310 -0.045 0.000 0.0014 0.0000 0.0000 392343.09-64643.16 -303.50 240.4 39302.0********* 0.000 44 23.31 -0.303 -0.038 0.000 0.0014 0.0000 0.0000 380571.98-50976.26 -238.87 236.2 22683.3********* 0.000 45 23.86 -0.296 -0.029 0.000 0.0014 0.0000 0.0001 365718.43-30846.11 -144.05 232.2 9603.9********* 0.000 46 24.41 -0.289 -0.021 0.000 0.0014 0.0000 0.0001 350446.28-16110.55 -75.55 228.2 1716.2 39466.2 0.000 47 24.96 -0.283 -0.014 0.000 0.0014 0.0000 0.0001 334755.78 -6111.50 -30.00 224.2 -2420.6 921619.1 0.000 48 25.50 -0.277 -0.008 0.000 0.0014 0.0000 0.0001 318646.60 79.69 -2.55 220.2 -4063.51256261.8 0.000 49 26.05 -0.271 -0.004 0.000 0.0014 0.0000 0.0001 302118.32 3422.73 11.80 216.2 -4203.01251898.1 0.000 50 26.60 -0.265 -0.002 0.000 0.0014 0.0000 0.0000 288256.69 4136.78 14.76 212.3 -3556.71064482.4 0.000 51 27.15 -0.260 0.000 0.000 0.0014 0.0000 0.0000 274102.40 4108.30 14.62 208.3 -2748.5 837967.9 0.000 52 27.69 -0.255 0.001 0.000 0.0014 0.0000 0.0000 259655.41 3588.65 12.59 204.4 -1947.7 613013.0 0.000 53 28.24 -0.250 0.002 0.000 0.0014 0.0000 0.0000 245126.07 2748.83 9.46 200.5 -1258.1 416512.1 0.000 54 28.79 -0.246 0.002 0.000 0.0014 0.0000 0.0000 230564.28 1688.45 5.65 196.5 -740.2 265996.7 0.000 55 29.34 -0.241 0.003 0.000 0.0014 0.0000 0.0000 215964.92 449.90 1.32 192.6 -430.9 173543.3 0.000 56 29.89 -0.237 0.003 0.000 0.0014 0.0000 0.0000 211259.74 414.73 1.19 188.7 -358.9 148908.4 0.000 57 30.43 -0.234 0.003 0.000 0.0014 0.0000 0.0000 206691.73 378.06 1.07 184.8 -293.5 126199.4 0.000 58 30.98 -0.230 0.003 0.000 0.0014 0.0000 0.0000 202257.63 341.03 0.94 180.8 -235.0 105498.5 0.000 59 31.53 -0.226 0.003 0.000 0.0014 0.0000 0.0000 197954.27 304.57 0.82 176.9 -183.4 86824.8 0.000 60 32.08 -0.222 0.003 0.000 0.0014 0.0000 0.0000 193778.58 269.36 0.71 173.0 -138.4 70147.6 0.000 61 32.62 -0.219 0.003 0.000 0.0014 0.0000 0.0000 189727.61 235.92 0.60 169.0 -99.6 55398.5 0.000 62 33.17 -0.215 0.003 0.000 0.0014 0.0000 0.0000 185798.46 204.60 0.50 165.1 -66.8 42480.6 0.000 63 33.72 -0.212 0.003 0.000 0.0014 0.0000 0.0000 181988.35 175.64 0.41 161.2 -39.3 31277.5 0.000 64 34.27 -0.209 0.003 0.000 0.0014 0.0000 0.0000 178294.57 149.17 0.33 157.2 -16.7 21660.0 0.000 65 34.81 -0.205 0.002 0.000 0.0014 0.0000 0.0000 174714.51 125.24 0.26 153.3 1.6 13491.7 0.000 66 35.36 -0.202 0.002 0.000 0.0014 0.0000 0.0000 171245.61 103.82 0.20 149.4 16.0 6634.0 0.000 67 35.91 -0.199 0.002 0.000 0.0014 0.0000 0.0000 167885.42 84.84 0.15 145.4 27.0 949.3 0.000 68 36.46 -0.196 0.002 0.000 0.0014 0.0000 0.0000 164631.53 68.18 0.10 141.5 35.2 -3696.1 0.000 69 37.00 -0.193 0.002 0.000 0.0014 0.0000 0.0000 161481.64 53.71 0.07 137.6 40.9 -7429.3 0.000 70 37.55 -0.190 0.001 0.000 0.0014 0.0000 0.0000 158433.47 41.26 0.04 133.6 44.6 -10370.1 0.000 71 38.10 -0.187 0.001 0.000 0.0014 0.0000 0.0000 155519.15 31.07 0.01 125.8 46.5 -12629.6 0.000 72 38.61 -0.185 0.001 0.000 0.0014 0.0000 0.0000 152718.61 22.68 -0.01 121.9 47.0 -14203.6 0.000 73 39.11 -0.183 0.001 0.000 0.0014 0.0000 0.0000 149997.52 15.53 -0.02 117.9 46.6 -15352.6 0.000





3.294

74 39.62 -0.181 0.001 0.000 0.0014 0.0000 0.0000 147327.07 9.27 -0.04 110.1 45.4 -16139.3 0.000 75 40.17 -0.178 0.001 0.000 0.0014 0.0000 0.0000 144723.92 3.97 -0.05 106.1 43.3 -16647.9 0.000 76 40.72 -0.175 0.001 0.000 0.0014 0.0000 0.0000 142213.62 -0.26 -0.05 102.2 40.7 -16865.7 0.000 77 41.27 -0.173 0.000 0.000 0.0014 0.0000 0.0000 139794.25 -3.57 -0.06 98.3 37.7 -16851.2 0.000 78 41.82 -0.170 0.000 0.000 0.0014 0.0000 0.0000 134855.37 -10.28 -0.07 94.3 34.4 -16655.5 0.000 79 42.36 -0.168 0.000 0.000 0.0014 0.0000 0.0000 129969.07 -15.44 -0.07 90.4 30.7 -16091.4 0.000 80 42.91 -0.165 0.000 0.000 0.0014 0.0000 0.0000 125133.38 -19.21 -0.07 86.5 26.8 -15244.1 0.000 81 43.46 -0.163 0.000 0.000 0.0014 0.0000 0.0000 120346.31 -21.75 -0.07 82.5 22.8 -14190.1 0.000 82 44.01 -0.161 0.000 0.000 0.0014 0.0000 0.0000 115605.89 -23.22 -0.07 78.6 18.8 -12996.7 0.000 83 44.56 -0.159 0.000 0.000 0.0014 0.0000 0.0000 110910.15 -23.80 -0.06 74.7 15.1 -11722.3 0.000 84 45.11 -0.157 0.000 0.000 0.0014 0.0000 0.0000 106257.12 -23.63 -0.06 70.8 11.6 -10416.5 0.000 85 45.66 -0.155 0.000 0.000 0.0014 0.0000 0.0000 101644.85 -22.85 -0.05 66.8 8.5 -9120.0 0.000 86 46.21 -0.153 0.000 0.000 0.0014 0.0000 0.0000 97071.37 -21.62 -0.04 62.9 5.8 -7866.0 0.000 87 46.75 -0.151 0.000 0.000 0.0014 0.0000 0.0000 92534.74 -20.03 -0.04 59.0 3.4 -6680.0 0.000 88 47.30 -0.149 0.000 0.000 0.0014 0.0000 0.0000 88033.00 -18.21 -0.03 55.0 1.5 -5580.8 0.000 89 47.85 -0.148 0.000 0.000 0.0014 0.0000 0.0000 83564.19 -16.25 -0.02 51.1 -0.1 -4581.5 0.000 90 48.40 -0.146 0.000 0.000 0.0014 0.0000 0.0000 79126.37 -14.23 -0.02 47.2 -1.3 -3689.7 0.000 91 48.95 -0.145 0.000 0.000 0.0014 0.0000 0.0000 74717.58 -12.22 -0.01 43.2 -2.1 -2908.8 0.000 92 49.50 -0.143 0.000 0.000 0.0014 0.0000 0.0000 70335.87 -10.28 -0.01 39.3 -2.7 -2238.0 0.000 93 50.05 -0.142 0.000 0.000 0.0014 0.0000 0.0000 65979.28 -8.46 0.00 35.4 -3.0 -1673.6 0.000 94 50.60 -0.141 0.000 0.000 0.0014 0.0000 0.0000 61645.85 -6.79 0.00 31.4 -3.1 -1209.4 0.000 95 51.14 -0.140 0.000 0.000 0.0014 0.0000 0.0000 57333.62 -5.30 0.01 27.5 -2.9 -836.9 0.000 96 51.69 -0.139 0.000 0.000 0.0014 0.0000 0.0000 53040.62 -4.02 0.01 23.6 -2.7 -546.1 0.000 97 52.24 -0.138 0.000 0.000 0.0014 0.0000 0.0000 48764.87 -2.96 0.01 19.7 -2.3 -325.7 0.000 98 52.79 -0.137 0.000 0.000 0.0014 0.0000 0.0000 44504.40 -2.14 0.01 15.7 -1.8 -163.2 0.000 99 53.34 -0.136 0.000 0.000 0.0014 0.0000 0.0000 39325.88 -1.46 0.01 7.9 -1.3 -45.8 0.000 100 54.10 -0.135 0.000 0.000 0.0014 0.0000 0.0000 31829.01 0.86 0.01 3.9 -0.5 65.3 0.000 101 54.86 -0.134 0.000 0.000 0.0014 0.0000 0.0000 31829.01 -0.86 -0.01 3.9 0.0 0.0 0.000 ** SACS COLLAPSE PILE DETAIL REPORT ** *** FINAL *** PILEHEAD JOINT 119 **** DEFLECTIONS **** ***** ROTATIONS ***** ************** ELASTIC INTERNAL LOADS *************** PLASTIC INCR DISTANCE X Y Z X Y Z FX FY FZ MX MY MZ RATIO M CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 1 0.00 1.259 20.351 -0.879 -0.0027 -0.0021 -0.0159-364347.00 64681.53 2053.33 -908.2****************** 0.000 2 0.51 1.232 19.512 -0.772 -0.0027 -0.0020 -0.0166-363603.56 63515.26 2157.18 -891.9****************** 0.000 3 1.02 1.205 18.644 -0.671 -0.0027 -0.0019 -0.0171-363160.83 62071.77 2262.79 -887.2****************** 0.000 4 1.53 1.176 17.751 -0.576 -0.0027 -0.0018 -0.0176-362637.39 60345.67 2369.25 -891.9****************** 0.000 5 2.03 1.148 16.839 -0.488 -0.0027 -0.0016 -0.0179-362031.89 58331.97 2475.04 -903.5*********7759540.9 0.000 6 2.54 1.118 15.914 -0.406 -0.0027 -0.0015 -0.0181-361342.85 56025.89 2578.55 -920.2*********4794841.0 0.000 7 3.05 1.089 14.981 -0.330 -0.0027 -0.0014 -0.0182-360500.13 53452.59 2686.98 -757.5*********1947346.7 0.000 8 3.59 1.053 13.978 -0.257 -0.0027 -0.0012 -0.0182-359476.94 50492.75 2796.38 -787.9*********-951278.6 0.000 9 4.13 1.017 12.979 -0.192 -0.0027 -0.0011 -0.0181-358151.05 46609.04 2905.58 -825.4****************** 0.000 10 4.68 0.981 11.990 -0.134 -0.0027 -0.0010 -0.0179-356515.42 41854.34 3007.72 -866.5****************** 0.000 11 5.22 0.947 11.019 -0.084 -0.0027 -0.0008 -0.0175-354712.39 36781.85 3092.55 -903.1****************** 0.000 12 5.76 0.913 10.071 -0.041 -0.0027 -0.0007 -0.0171-352961.94 32132.56 3154.85 -926.9****************** 0.000 13 6.30 0.880 9.151 -0.005 -0.0027 -0.0006 -0.0165-351309.97 27891.99 3197.77 -938.7****************** 0.000 14 6.85 0.849 8.264 0.026 -0.0027 -0.0005 -0.0159-349839.44 24276.16 3224.89 -937.2****************** 0.000 15 7.39 0.818 7.414 0.050 -0.0027 -0.0004 -0.0152-348544.33 21253.85 3240.54 -923.7****************** 0.000 16 7.93 0.789 6.605 0.070 -0.0027 -0.0003 -0.0145-347361.00 18660.41 3247.34 -900.7****************** 0.000 17 8.47 0.762 5.838 0.084 -0.0027 -0.0002 -0.0136-345836.39 15454.85 3233.59 -876.9****************** 0.000 18 9.02 0.735 5.117 0.095 -0.0027 -0.0001 -0.0128-343977.85 11728.20 3195.70 -851.9****************** 0.000 19 9.56 0.710 4.444 0.101 -0.0027 -0.0001 -0.0119-342089.71 7840.98 3136.79 -823.7****************** 0.000 20 10.10 0.687 3.821 0.104 -0.0027 0.0000 -0.0110-340191.61 3816.56 3055.27 -793.2****************** 0.000 21 10.64 0.664 3.249 0.104 -0.0027 0.0000 -0.0101-338317.16 -113.77 2956.11 -760.0-923102.3********* 0.000 22 11.19 0.643 2.728 0.101 -0.0027 0.0001 -0.0091-336471.88 -3827.43 2843.43 -724.6-762796.4********* 0.000 23 11.73 0.623 2.259 0.097 -0.0027 0.0001 -0.0082-334654.75 -7334.41 2717.43 -688.3-608600.2********* 0.000 24 12.27 0.603 1.840 0.091 -0.0027 0.0001 -0.0073-332864.93-10637.94 2578.33 -652.3-461236.8********* 0.000 25 12.81 0.585 1.472 0.083 -0.0027 0.0002 -0.0064-331101.61-13698.72 2428.47 -617.3-321416.3********* 0.000 26 13.36 0.567 1.151 0.074 -0.0027 0.0002 -0.0056-329364.72-16544.09 2266.57 -584.4-189722.4********* 0.000 27 13.90 0.549 0.877 0.065 -0.0027 0.0002 -0.0047-327654.10-19154.78 2093.79 -554.2 -66808.2********* 0.000 28 14.44 0.532 0.646 0.056 -0.0027 0.0002 -0.0040-325065.46-22294.54 1843.73 -531.2 46736.3********* 0.000 29 14.98 0.516 0.457 0.047 -0.0027 0.0002 -0.0032-322508.68-25117.63 1577.47 -511.5 146719.9********* 0.000 30 15.52 0.500 0.306 0.038 -0.0027 0.0002 -0.0026-319998.08-27285.91 1332.87 -493.8 232264.6********* 0.000 31 16.07 0.484 0.188 0.029 -0.0027 0.0001 -0.0020-317534.72-28676.01 1141.10 -477.1 304544.6********* 0.000 32 16.61 0.469 0.101 0.022 -0.0027 0.0001 -0.0015-315120.16-29481.15 997.45 -462.0 366424.7********* 0.000 33 17.15 0.454 0.040 0.015 -0.0027 0.0001 -0.0011-312755.39-29868.03 896.14 -448.8 420515.0********* 0.000 34 17.69 0.438 0.001 0.009 -0.0027 0.0001 -0.0007-307727.87-30120.34 -374.38 -471.7 469111.3********* 0.000 35 18.24 0.424 -0.021 0.005 -0.0027 0.0001 -0.0004-302515.22-27214.37 -1092.35 -482.5 448809.9********* 0.000 36 18.78 0.409 -0.030 0.002 -0.0027 0.0000 -0.0002-297118.59-22773.08 -1409.63 -486.0 389573.9********* 0.000 37 19.32 0.395 -0.032 0.000 -0.0027 0.0000 -0.0001-291537.31-17959.19 -1461.60 -485.1 313132.3********* 0.000 38 19.86 0.380 -0.028 -0.001 -0.0027 0.0000 0.0000-285770.33-13532.88 -1359.80 -481.5 233872.9********* 0.000 39 20.41 0.367 -0.022 -0.001 -0.0027 0.0000 0.0001-279816.85 -9925.47 -1189.54 -476.1 160133.6-580313.1 0.000 40 20.95 0.353 -0.016 -0.001 -0.0027 0.0000 0.0001-271841.91 -5103.10 -857.99 -470.7 95627.2 -42075.1 0.000 41 21.49 0.340 -0.010 -0.001 -0.0027 0.0000 0.0001-263576.28 -1905.58 -565.36 -464.3 49100.3 234655.6 0.000 42 22.03 0.327 -0.006 -0.001 -0.0027 0.0000 0.0001-255020.04 -5.75 -336.54 -457.3 18442.0 337991.3 0.000 43 22.58 0.315 -0.003 0.000 -0.0027 0.0000 0.0000-246173.32 958.10 -176.02 -450.2 192.1 338302.8 0.000 44 23.12 0.303 -0.001 0.000 -0.0027 0.0000 0.0000-237036.21 1314.88 -76.71 -442.9 -9353.2 286346.9 0.000 45 23.66 0.292 0.000 0.000 -0.0027 0.0000 0.0000-225313.49 1339.11 17.66 -435.6 -13513.0 215043.9 0.000 46 24.20 0.281 0.000 0.000 -0.0027 0.0000 0.0000-213238.49 1083.41 54.15 -428.2 -12555.2 142426.5 0.000 47 24.74 0.270 0.000 0.000 -0.0027 0.0000 0.0000-200811.22 758.24 58.54 -420.8 -9618.5 83675.4 0.000 48 25.29 0.261 0.000 0.000 -0.0027 0.0000 0.0000-188031.65 466.83 48.17 -413.5 -6443.8 42557.7 0.000 49 25.83 0.252 0.000 0.000 -0.0027 0.0000 0.0000-175029.71 244.88 33.19 -406.1 -3831.6 17242.6 0.000 50 26.37 0.243 0.000 0.000 -0.0027 0.0000 0.0000-162135.25 91.39 18.51 -398.7 -2031.8 3963.0 0.000 51 26.91 0.235 0.000 0.000 -0.0027 0.0000 0.0000-151819.05 37.17 11.72 -391.3 -1028.0 -993.1 0.000 52 27.46 0.228 0.000 0.000 -0.0027 0.0000 0.0000-141611.00 5.48 6.53 -383.9 -392.7 -3008.6 0.000 53 28.00 0.221 0.000 0.000 -0.0027 0.0000 0.0000-131502.26 -9.49 2.98 -376.5 -38.5 -3305.9 0.000 54 28.54 0.215 0.000 0.000 -0.0027 0.0000 0.0000-121482.77 -12.58 0.80 -369.2 122.9 -2791.6 0.000 55 29.08 0.209 0.000 0.000 -0.0027 0.0000 0.0000-111541.26 -7.06 -0.31 -361.8 166.5 -2109.4 0.000 56 29.63 0.203 0.000 0.000 -0.0027 0.0000 0.0000-107435.64 -5.25 -0.35 -354.4 150.0 -1726.5 0.000 57 30.17 0.198 0.000 0.000 -0.0027 0.0000 0.0000-104287.86 -4.84 -0.35 -347.0 130.8 -1441.8 0.000 58 30.71 0.193 0.000 0.000 -0.0027 0.0000 0.0000-101275.94 -4.36 -0.33 -339.6 112.0 -1179.5 0.000 59 31.25 0.188 0.000 0.000 -0.0027 0.0000 0.0000 -98395.25 -3.84 -0.31 -332.2 94.1 -943.3 0.000 60 31.80 0.184 0.000 0.000 -0.0027 0.0000 0.0000 -95641.39 -3.33 -0.28 -324.9 77.5 -734.8 0.000





3.295

61 32.34 0.179 0.000 0.000 -0.0027 0.0000 0.0000 -93010.13 -2.83 -0.25 -317.5 62.6 -554.2 0.000 62 32.88 0.174 0.000 0.000 -0.0027 0.0000 0.0000 -90497.42 -2.37 -0.21 -310.1 49.3 -400.6 0.000 63 33.42 0.170 0.000 0.000 -0.0027 0.0000 0.0000 -88099.39 -1.94 -0.18 -302.7 37.7 -272.3 0.000 64 33.97 0.166 0.000 0.000 -0.0027 0.0000 0.0000 -85812.33 -1.56 -0.15 -295.3 27.8 -167.2 0.000 65 34.51 0.162 0.000 0.000 -0.0027 0.0000 0.0000 -83632.68 -1.22 -0.13 -287.9 19.4 -82.9 0.000 66 35.05 0.158 0.000 0.000 -0.0027 0.0000 0.0000 -81660.12 -0.94 -0.10 -273.2 12.6 -16.8 0.000 67 35.56 0.155 0.000 0.000 -0.0027 0.0000 0.0000 -79869.87 -0.70 -0.08 -265.8 7.3 30.7 0.000 68 36.06 0.152 0.000 0.000 -0.0027 0.0000 0.0000 -78156.93 -0.51 -0.07 -258.4 3.0 66.3 0.000 69 36.57 0.149 0.000 0.000 -0.0027 0.0000 0.0000 -76397.07 -0.33 -0.05 -243.6 -0.3 91.9 0.000 70 37.13 0.146 0.000 0.000 -0.0027 0.0000 0.0000 -74615.03 -0.19 -0.04 -236.3 -3.1 110.5 0.000 71 37.69 0.142 0.000 0.000 -0.0027 0.0000 0.0000 -72943.00 -0.07 -0.02 -228.9 -5.2 120.8 0.000 72 38.25 0.138 0.000 0.000 -0.0027 0.0000 0.0000 -71376.82 0.02 -0.02 -221.5 -6.5 124.8 0.000 73 38.80 0.135 0.000 0.000 -0.0027 0.0000 0.0000 -69913.71 0.08 -0.01 -214.1 -7.4 123.8 0.000 74 39.36 0.131 0.000 0.000 -0.0027 0.0000 0.0000 -68550.34 0.13 0.00 -206.7 -7.8 119.2 0.000 75 39.92 0.128 0.000 0.000 -0.0027 0.0000 0.0000 -67282.96 0.16 0.00 -199.3 -7.9 111.9 0.000 76 40.48 0.124 0.000 0.000 -0.0027 0.0000 0.0000 -66107.95 0.19 0.01 -192.0 -7.8 102.8 0.000 77 41.04 0.121 0.000 0.000 -0.0027 0.0000 0.0000 -65021.80 0.20 0.01 -184.6 -7.4 92.4 0.000 78 41.60 0.118 0.000 0.000 -0.0027 0.0000 0.0000 -64021.16 0.20 0.01 -177.2 -7.0 81.4 0.000 79 42.16 0.115 0.000 0.000 -0.0027 0.0000 0.0000 -61270.60 0.20 0.01 -169.8 -6.4 70.1 0.000 80 42.72 0.112 0.000 0.000 -0.0027 0.0000 0.0000 -58592.03 0.20 0.01 -162.4 -5.7 58.7 0.000 81 43.27 0.109 0.000 0.000 -0.0027 0.0000 0.0000 -55982.37 0.18 0.01 -155.0 -5.0 47.7 0.000 82 43.83 0.106 0.000 0.000 -0.0027 0.0000 0.0000 -53438.59 0.16 0.01 -147.7 -4.2 37.6 0.000 83 44.39 0.103 0.000 0.000 -0.0027 0.0000 0.0000 -50957.73 0.14 0.01 -140.3 -3.4 28.6 0.000 84 44.95 0.101 0.000 0.000 -0.0027 0.0000 0.0000 -48536.90 0.12 0.01 -132.9 -2.7 20.7 0.000 85 45.51 0.098 0.000 0.000 -0.0027 0.0000 0.0000 -46173.24 0.10 0.01 -125.5 -2.1 14.1 0.000 86 46.07 0.096 0.000 0.000 -0.0027 0.0000 0.0000 -43863.95 0.08 0.01 -118.1 -1.5 8.7 0.000 87 46.63 0.094 0.000 0.000 -0.0027 0.0000 0.0000 -41606.30 0.06 0.01 -110.7 -1.0 4.5 0.000 88 47.18 0.092 0.000 0.000 -0.0027 0.0000 0.0000 -39397.56 0.04 0.01 -103.4 -0.7 1.3 0.000 89 47.74 0.090 0.000 0.000 -0.0027 0.0000 0.0000 -37235.10 0.03 0.00 -96.0 -0.4 -1.1 0.000 90 48.30 0.088 0.000 0.000 -0.0027 0.0000 0.0000 -35116.27 0.02 0.00 -88.6 -0.1 -2.7 0.000 91 48.86 0.086 0.000 0.000 -0.0027 0.0000 0.0000 -33038.51 0.01 0.00 -81.2 0.0 -3.6 0.000 92 49.42 0.085 0.000 0.000 -0.0027 0.0000 0.0000 -30999.27 0.00 0.00 -73.8 0.2 -4.1 0.000 93 49.98 0.083 0.000 0.000 -0.0027 0.0000 0.0000 -28996.01 0.00 0.00 -66.4 0.2 -4.2 0.000 94 50.54 0.082 0.000 0.000 -0.0027 0.0000 0.0000 -27026.26 -0.01 0.00 -59.1 0.3 -4.0 0.000 95 51.10 0.080 0.000 0.000 -0.0027 0.0000 0.0000 -25087.55 -0.01 0.00 -51.7 0.3 -3.6 0.000 96 51.65 0.079 0.000 0.000 -0.0027 0.0000 0.0000 -23177.44 -0.01 0.00 -44.3 0.2 -3.1 0.000 97 52.21 0.078 0.000 0.000 -0.0027 0.0000 0.0000 -21293.51 -0.01 0.00 -36.9 0.2 -2.5 0.000 98 52.77 0.077 0.000 0.000 -0.0027 0.0000 0.0000 -19433.35 -0.01 0.00 -29.5 0.2 -1.9 0.000 99 53.33 0.076 0.000 0.000 -0.0027 0.0000 0.0000 -17315.39 -0.01 0.00 -14.8 0.1 -1.3 0.000 100 54.09 0.075 0.000 0.000 -0.0027 0.0000 0.0000 -14685.28 -0.01 0.00 -7.4 0.0 -0.4 0.000 101 54.85 0.074 0.000 0.000 -0.0027 0.0000 0.0000 -14685.28 0.01 0.00 -7.4 0.0 0.0 0.000 ** SACS COLLAPSE PILE DETAIL REPORT ** *** FINAL *** PILEHEAD JOINT 199 **** DEFLECTIONS **** ***** ROTATIONS ***** ************** ELASTIC INTERNAL LOADS *************** PLASTIC INCR DISTANCE X Y Z X Y Z FX FY FZ MX MY MZ RATIO M CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 1 0.00 1.188 19.163 -1.043 0.0011 0.0000 -0.0147-353598.34 63662.40 -6262.39 213.33919694.9********* 0.000 2 0.51 1.164 18.388 -1.042 0.0011 -0.0001 -0.0153-352840.65 62471.44 -6227.05 210.13601410.5********* 0.000 3 1.02 1.139 17.583 -1.034 0.0011 -0.0002 -0.0159-352387.10 61003.38 -6170.55 212.03284921.6********* 0.000 4 1.53 1.113 16.752 -1.020 0.0011 -0.0003 -0.0163-351851.86 59254.08 -6091.97 218.02971304.7********* 0.000 5 2.03 1.087 15.902 -1.002 0.0011 -0.0004 -0.0167-351233.69 57218.97 -5990.04 227.22661681.98377163.7 0.000 6 2.54 1.060 15.037 -0.978 0.0011 -0.0005 -0.0169-350529.87 54967.84 -5868.27 238.22357240.05469032.4 0.000 7 3.05 1.033 14.163 -0.951 0.0011 -0.0006 -0.0171-349670.81 52471.36 -5729.22 151.92058987.22675314.1 0.000 8 3.59 1.000 13.222 -0.916 0.0011 -0.0007 -0.0171-348629.65 49598.08 -5560.36 170.61748303.1-170101.5 0.000 9 4.13 0.967 12.282 -0.878 0.0011 -0.0007 -0.0171-347282.78 45817.43 -5318.72 193.61446775.7********* 0.000 10 4.68 0.934 11.351 -0.835 0.0011 -0.0008 -0.0169-345623.69 41179.62 -5004.36 219.51158350.8********* 0.000 11 5.22 0.902 10.435 -0.790 0.0011 -0.0009 -0.0165-343815.57 36226.30 -4654.77 243.8 886971.8********* 0.000 12 5.76 0.870 9.539 -0.742 0.0011 -0.0009 -0.0161-342106.38 31685.11 -4325.25 262.0 634549.0********* 0.000 13 6.30 0.840 8.670 -0.693 0.0011 -0.0009 -0.0156-340492.68 27541.70 -4016.50 274.5 399993.6********* 0.000 14 6.85 0.810 7.831 -0.642 0.0011 -0.0009 -0.0150-339055.92 24008.99 -3747.67 280.6 182179.4********* 0.000 15 7.39 0.782 7.026 -0.591 0.0011 -0.0009 -0.0144-337790.42 21057.43 -3518.88 280.9 -21058.2********* 0.000 16 7.93 0.755 6.259 -0.541 0.0011 -0.0009 -0.0137-336633.97 18526.06 -3318.76 276.7-211890.9********* 0.000 17 8.47 0.729 5.532 -0.490 0.0011 -0.0009 -0.0129-335142.88 15406.06 -3059.77 272.8-391872.7********* 0.000 18 9.02 0.704 4.848 -0.441 0.0011 -0.0009 -0.0121-333332.99 11778.90 -2746.36 269.0-557810.9********* 0.000 19 9.56 0.680 4.210 -0.394 0.0011 -0.0009 -0.0113-331494.64 7986.93 -2407.68 263.9-706754.1********* 0.000 20 10.10 0.658 3.618 -0.348 0.0011 -0.0008 -0.0104-329645.84 4052.81 -2044.58 257.9-837331.2********* 0.000 21 10.64 0.636 3.076 -0.304 0.0011 -0.0008 -0.0096-327819.35 224.26 -1680.17 250.4-948217.9********* 0.000 22 11.19 0.616 2.581 -0.263 0.0011 -0.0007 -0.0087-326020.86 -3390.66 -1325.27 241.7****************** 0.000 23 11.73 0.596 2.136 -0.225 0.0011 -0.0007 -0.0078-324249.50 -6809.62 -978.40 232.2****************** 0.000 24 12.27 0.578 1.739 -0.190 0.0011 -0.0006 -0.0069-322504.37-10016.74 -641.48 222.4****************** 0.000 25 12.81 0.560 1.390 -0.157 0.0011 -0.0006 -0.0061-320784.89-12993.91 -316.71 212.6****************** 0.000 26 13.36 0.543 1.086 -0.128 0.0011 -0.0005 -0.0053-319090.98-15767.20 -1.24 203.3****************** 0.000 27 13.90 0.526 0.826 -0.102 0.0011 -0.0005 -0.0045-317422.38-18290.12 299.43 194.6****************** 0.000 28 14.44 0.510 0.608 -0.080 0.0011 -0.0004 -0.0037-314908.08-21341.83 687.21 189.1****************** 0.000 29 14.98 0.494 0.429 -0.060 0.0011 -0.0003 -0.0031-312438.61-24094.90 1060.96 184.6****************** 0.000 30 15.52 0.479 0.286 -0.044 0.0011 -0.0003 -0.0024-310013.65-26121.75 1358.07 179.9****************** 0.000 31 16.07 0.463 0.176 -0.030 0.0011 -0.0002 -0.0019-307634.55-27415.68 1567.23 174.9****************** 0.000 32 16.61 0.448 0.094 -0.019 0.0011 -0.0002 -0.0014-305302.71-28159.88 1705.78 170.1-946677.4********* 0.000 33 17.15 0.434 0.037 -0.011 0.0011 -0.0001 -0.0010-303019.04-28512.16 1789.58 165.6-854177.1********* 0.000 34 17.69 0.419 0.000 -0.005 0.0011 -0.0001 -0.0006-297992.70-28601.68 2494.02 179.4-757132.2********* 0.000 35 18.24 0.404 -0.020 -0.001 0.0011 -0.0001 -0.0004-292781.17-25753.66 2659.49 186.5-621886.8********* 0.000 36 18.78 0.390 -0.029 0.001 0.0011 0.0000 -0.0002-287385.40-21493.14 2491.90 189.5-477668.1********* 0.000 37 19.32 0.376 -0.030 0.002 0.0011 0.0000 -0.0001-281804.74-16909.58 2153.02 190.0-342537.5********* 0.000 38 19.86 0.363 -0.027 0.002 0.0011 0.0000 0.0000-276038.24-12712.56 1760.98 189.1-225783.7********* 0.000 39 20.41 0.349 -0.021 0.002 0.0011 0.0000 0.0001-270085.16 -9302.15 1394.60 187.3-130289.6-533673.4 0.000 40 20.95 0.336 -0.015 0.002 0.0011 0.0000 0.0001-262110.70 -4755.09 849.19 185.4 -54663.1 -29236.6 0.000 41 21.49 0.324 -0.009 0.001 0.0011 0.0000 0.0001-253845.58 -1748.28 448.61 182.9 -8613.0 228622.2 0.000 42 22.03 0.311 -0.005 0.001 0.0011 0.0000 0.0001-245289.87 32.11 181.20 180.3 15714.0 323428.2 0.000 43 22.58 0.300 -0.003 0.000 0.0011 0.0000 0.0000-236443.69 930.43 21.75 177.5 25540.0 321686.8 0.000 44 23.12 0.288 -0.001 0.000 0.0011 0.0000 0.0000-227307.13 1258.53 -58.63 174.6 26719.6 271231.3 0.000 45 23.66 0.277 0.000 0.000 0.0011 0.0000 0.0000-215585.09 1271.17 -111.05 171.8 23540.3 202983.8 0.000 46 24.20 0.267 0.000 0.000 0.0011 0.0000 0.0000-203510.77 1024.10 -111.17 168.9 17518.2 134050.8 0.000 47 24.74 0.257 0.000 0.000 0.0011 0.0000 0.0000-191084.17 714.51 -88.83 166.0 11489.7 78516.0 0.000





3.296

48 25.29 0.248 0.000 0.000 0.0011 0.0000 0.0000-178631.69 438.62 -61.16 163.0 6672.8 39769.7 0.000 49 25.83 0.239 0.000 0.000 0.0011 0.0000 0.0000-166289.54 229.25 -36.31 160.1 3356.3 15984.3 0.000 50 26.37 0.231 0.000 0.000 0.0011 0.0000 0.0000-154049.48 84.92 -16.82 157.2 1387.5 3552.3 0.000 51 26.91 0.223 0.000 0.000 0.0011 0.0000 0.0000-144259.09 34.09 -9.08 154.3 475.3 -1052.6 0.000 52 27.46 0.217 0.000 0.000 0.0011 0.0000 0.0000-134571.49 4.53 -3.91 151.4 -17.0 -2901.4 0.000 53 28.00 0.210 0.000 0.000 0.0011 0.0000 0.0000-124978.30 -9.33 -0.87 148.5 -228.9 -3146.9 0.000 54 28.54 0.204 0.000 0.000 0.0011 0.0000 0.0000-115469.99 -12.04 0.52 145.6 -276.3 -2641.1 0.000 55 29.08 0.198 0.000 0.000 0.0011 0.0000 0.0000-106035.88 -6.68 0.70 142.7 -248.0 -1988.1 0.000 56 29.63 0.193 0.000 0.000 0.0011 0.0000 0.0000-102111.76 -4.96 0.59 139.8 -210.3 -1625.8 0.000 57 30.17 0.188 0.000 0.000 0.0011 0.0000 0.0000 -99093.58 -4.56 0.55 136.8 -178.5 -1357.1 0.000 58 30.71 0.184 0.000 0.000 0.0011 0.0000 0.0000 -96205.29 -4.11 0.50 133.9 -148.7 -1109.7 0.000 59 31.25 0.179 0.000 0.000 0.0011 0.0000 0.0000 -93442.51 -3.62 0.45 131.0 -121.3 -887.0 0.000 60 31.80 0.174 0.000 0.000 0.0011 0.0000 0.0000 -90801.01 -3.14 0.40 128.1 -96.7 -690.5 0.000 61 32.34 0.170 0.000 0.000 0.0011 0.0000 0.0000 -88276.78 -2.67 0.34 125.2 -75.1 -520.4 0.000 62 32.88 0.166 0.000 0.000 0.0011 0.0000 0.0000 -85865.95 -2.23 0.29 122.3 -56.4 -375.8 0.000 63 33.42 0.162 0.000 0.000 0.0011 0.0000 0.0000 -83564.84 -1.82 0.24 119.4 -40.6 -255.1 0.000 64 33.97 0.158 0.000 0.000 0.0011 0.0000 0.0000 -81369.91 -1.46 0.20 116.5 -27.4 -156.2 0.000 65 34.51 0.154 0.000 0.000 0.0011 0.0000 0.0000 -79277.77 -1.15 0.16 113.5 -16.6 -76.9 0.000 66 35.05 0.150 0.000 0.000 0.0011 0.0000 0.0000 -77385.53 -0.88 0.13 107.7 -7.9 -14.7 0.000 67 35.56 0.147 0.000 0.000 0.0011 0.0000 0.0000 -75669.58 -0.66 0.10 104.8 -1.5 29.9 0.000 68 36.06 0.145 0.000 0.000 0.0011 0.0000 0.0000 -74033.31 -0.47 0.07 101.9 3.4 63.3 0.000 69 36.57 0.142 0.000 0.000 0.0011 0.0000 0.0000 -72360.56 -0.31 0.05 96.1 7.1 87.3 0.000 70 37.13 0.138 0.000 0.000 0.0011 0.0000 0.0000 -70678.20 -0.17 0.03 93.2 10.0 104.6 0.000 71 37.69 0.135 0.000 0.000 0.0011 0.0000 0.0000 -69100.24 -0.06 0.02 90.3 11.9 114.3 0.000 72 38.25 0.131 0.000 0.000 0.0011 0.0000 0.0000 -67622.75 0.02 0.01 87.3 12.9 117.9 0.000 73 38.80 0.128 0.000 0.000 0.0011 0.0000 0.0000 -66243.10 0.08 0.00 84.4 13.3 116.9 0.000 74 39.36 0.125 0.000 0.000 0.0011 0.0000 0.0000 -64958.16 0.12 -0.01 81.5 13.1 112.5 0.000 75 39.92 0.122 0.000 0.000 0.0011 0.0000 0.0000 -63764.35 0.16 -0.01 78.6 12.6 105.6 0.000 76 40.48 0.118 0.000 0.000 0.0011 0.0000 0.0000 -62658.26 0.18 -0.02 75.7 11.9 96.9 0.000 77 41.04 0.115 0.000 0.000 0.0011 0.0000 0.0000 -61636.58 0.19 -0.02 72.8 10.9 87.1 0.000 78 41.60 0.112 0.000 0.000 0.0011 0.0000 0.0000 -60696.11 0.19 -0.02 69.9 9.8 76.7 0.000 79 42.16 0.109 0.000 0.000 0.0011 0.0000 0.0000 -58090.73 0.19 -0.02 67.0 8.7 66.0 0.000 80 42.72 0.106 0.000 0.000 0.0011 0.0000 0.0000 -55553.58 0.18 -0.02 64.0 7.4 55.2 0.000 81 43.27 0.104 0.000 0.000 0.0011 0.0000 0.0000 -53081.74 0.17 -0.02 61.1 6.2 44.9 0.000 82 43.83 0.101 0.000 0.000 0.0011 0.0000 0.0000 -50672.34 0.15 -0.02 58.2 5.0 35.3 0.000 83 44.39 0.098 0.000 0.000 0.0011 0.0000 0.0000 -48322.59 0.13 -0.02 55.3 4.0 26.8 0.000 84 44.95 0.096 0.000 0.000 0.0011 0.0000 0.0000 -46029.73 0.11 -0.01 52.4 3.0 19.4 0.000 85 45.51 0.094 0.000 0.000 0.0011 0.0000 0.0000 -43791.07 0.09 -0.01 49.5 2.2 13.2 0.000 86 46.07 0.091 0.000 0.000 0.0011 0.0000 0.0000 -41603.95 0.07 -0.01 46.6 1.5 8.2 0.000 87 46.63 0.089 0.000 0.000 0.0011 0.0000 0.0000 -39465.78 0.05 -0.01 43.7 0.9 4.2 0.000 88 47.18 0.087 0.000 0.000 0.0011 0.0000 0.0000 -37374.00 0.04 -0.01 40.8 0.4 1.1 0.000 89 47.74 0.086 0.000 0.000 0.0011 0.0000 0.0000 -35326.09 0.03 0.00 37.8 0.1 -1.1 0.000 90 48.30 0.084 0.000 0.000 0.0011 0.0000 0.0000 -33319.56 0.02 0.00 34.9 -0.1 -2.5 0.000 91 48.86 0.082 0.000 0.000 0.0011 0.0000 0.0000 -31351.97 0.01 0.00 32.0 -0.3 -3.4 0.000 92 49.42 0.081 0.000 0.000 0.0011 0.0000 0.0000 -29420.91 0.00 0.00 29.1 -0.4 -3.9 0.000 93 49.98 0.079 0.000 0.000 0.0011 0.0000 0.0000 -27524.00 0.00 0.00 26.2 -0.4 -4.0 0.000 94 50.54 0.078 0.000 0.000 0.0011 0.0000 0.0000 -25658.87 -0.01 0.00 23.3 -0.4 -3.8 0.000 95 51.10 0.076 0.000 0.000 0.0011 0.0000 0.0000 -23823.19 -0.01 0.00 20.4 -0.4 -3.4 0.000 96 51.65 0.075 0.000 0.000 0.0011 0.0000 0.0000 -22014.65 -0.01 0.00 17.5 -0.4 -2.9 0.000 97 52.21 0.074 0.000 0.000 0.0011 0.0000 0.0000 -20230.97 -0.01 0.00 14.6 -0.3 -2.4 0.000 98 52.77 0.073 0.000 0.000 0.0011 0.0000 0.0000 -18469.85 -0.01 0.00 11.6 -0.2 -1.8 0.000 99 53.33 0.072 0.000 0.000 0.0011 0.0000 0.0000 -16467.52 -0.01 0.00 5.8 -0.2 -1.2 0.000 100 54.09 0.071 0.000 0.000 0.0011 0.0000 0.0000 -13981.65 0.00 0.00 2.9 -0.1 -0.4 0.000 101 54.85 0.071 0.000 0.000 0.0011 0.0000 0.0000 -13981.65 0.00 0.00 2.9 0.0 0.0 0.000 ** SACS COLLAPSE PILE DETAIL REPORT ** *** FINAL *** PILEHEAD JOINT 841 **** DEFLECTIONS **** ***** ROTATIONS ***** ************** ELASTIC INTERNAL LOADS *************** PLASTIC INCR DISTANCE X Y Z X Y Z FX FY FZ MX MY MZ RATIO M CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 1 0.00 0.056 36.748 0.000 0.8174 -0.0044 -0.0062 271060.09 54843.76-33385.38-490249.3****************** 0.833 2 0.56 0.122 36.153 -0.059 0.8174 -0.0102 -0.0158 271275.91 60911.44-33086.90 226659.8****************** 0.667 3 1.13 0.145 35.217 -0.167 0.8173 -0.0128 -0.0199 271377.87 71987.31-31737.19 667645.6****************** 0.250 4 1.69 0.143 34.116 -0.297 0.8172 -0.0143 -0.0223 271526.01 75650.41-31156.33 737268.2****************** 0.167 5 2.25 0.130 32.908 -0.438 0.8171 -0.0155 -0.0241 271640.14 74730.59-31071.41 726622.3****************** 0.000 6 2.82 0.112 31.613 -0.587 0.8170 -0.0166 -0.0256 271714.80 72803.77-31055.97 703607.8****************** 0.000 7 3.38 0.090 30.244 -0.738 0.8170 -0.0175 -0.0268 271733.69 70702.47-31007.98 687102.5****************** 0.000 8 3.94 0.066 28.815 -0.888 0.8169 -0.0184 -0.0277 271685.99 67848.78-30906.47 675731.3****************** 0.000 9 4.50 0.039 27.337 -1.034 0.8168 -0.0191 -0.0284 271532.50 63977.32-30730.27 668156.29925041.48197435.9 0.000 10 5.07 0.011 25.822 -1.172 0.8167 -0.0197 -0.0288 271229.17 59213.77-30469.19 663124.38195463.54595994.3 0.000 11 5.63 -0.019 24.283 -1.299 0.8166 -0.0202 -0.0290 270785.31 54797.23-30174.85 659519.96480449.31262674.3 0.000 12 6.19 -0.050 22.730 -1.414 0.8166 -0.0206 -0.0290 270210.79 50746.30-29853.18 656450.44781883.2********* 0.000 13 6.76 -0.081 21.172 -1.514 0.8165 -0.0208 -0.0288 269534.66 47200.51-29519.65 653173.43101314.1********* 0.000 14 7.32 -0.112 19.620 -1.598 0.8164 -0.0210 -0.0284 268786.15 44211.62-29186.99 649070.21439417.6********* 0.000 15 7.88 -0.142 18.083 -1.665 0.8164 -0.0210 -0.0278 268005.97 41773.54-28864.80 643612.1-203849.0********* 0.000 16 8.44 -0.170 16.568 -1.714 0.8163 -0.0209 -0.0271 266993.30 38506.60-28419.93 636301.8****************** 0.000 17 9.01 -0.197 15.085 -1.744 0.8163 -0.0208 -0.0262 265719.79 34374.72-27826.69 626769.2****************** 0.000 18 9.57 -0.222 13.641 -1.755 0.8162 -0.0205 -0.0251 264330.74 30526.80-27209.22 614831.2****************** 0.000 19 10.13 -0.245 12.244 -1.747 0.8162 -0.0201 -0.0240 262849.15 26877.81-26560.74 600354.5****************** 0.000 20 10.70 -0.265 10.900 -1.720 0.8161 -0.0196 -0.0227 261310.19 23115.41-25834.21 583263.8****************** 0.000 21 11.26 -0.282 9.616 -1.675 0.8161 -0.0190 -0.0214 259725.68 19231.00-25020.55 563579.4****************** 0.000 22 11.82 -0.297 8.397 -1.612 0.8161 -0.0183 -0.0199 258105.17 15232.00-24112.07 541402.7****************** 0.000 23 12.39 -0.309 7.249 -1.533 0.8160 -0.0175 -0.0184 256462.63 11351.95-23147.69 516923.9****************** 0.000 24 12.95 -0.318 6.175 -1.440 0.8160 -0.0167 -0.0169 254809.81 7779.25-22168.81 490376.3****************** 0.000 25 13.51 -0.324 5.180 -1.334 0.8160 -0.0157 -0.0153 253153.55 4492.47-21174.75 461996.0****************** 0.000 26 14.07 -0.327 4.267 -1.217 0.8159 -0.0147 -0.0137 251500.28 1470.32-20162.81 432023.2****************** 0.000 27 14.64 -0.328 3.439 -1.091 0.8159 -0.0136 -0.0121 249194.43 -2730.95-18674.27 400591.0****************** 0.000 28 15.20 -0.327 2.698 -0.959 0.8159 -0.0124 -0.0105 246900.78 -6552.47-17156.22 368206.9****************** 0.000 29 15.76 -0.323 2.046 -0.824 0.8159 -0.0111 -0.0089 244627.10 -9940.26-15626.47 335246.8****************** 0.000 30 16.33 -0.318 1.484 -0.689 0.8158 -0.0098 -0.0073 242379.21-12894.82-14080.44 302046.7****************** 0.000 31 16.89 -0.311 1.012 -0.556 0.8158 -0.0085 -0.0058 240161.76-15425.61-12497.84 268900.3****************** 0.000 32 17.45 -0.303 0.629 -0.429 0.8158 -0.0070 -0.0043 235282.37-42145.88 5971.84 234080.8****************** 0.000 33 18.02 -0.294 0.341 -0.311 0.8158 -0.0056 -0.0029 230351.52-61424.93 23846.57 203550.9****************** 0.000 34 18.58 -0.285 0.139 -0.205 0.8158 -0.0042 -0.0018 225327.94-72442.77 40528.32 179464.3****************** 0.000





3.297

35 19.14 -0.275 0.013 -0.117 0.8158 -0.0030 -0.0008 220171.33-73778.20 55063.44 162480.3****************** 0.000 36 19.70 -0.265 -0.053 -0.049 0.8158 -0.0019 -0.0002 214848.06-64999.49 62868.47 151849.0****************** 0.000 37 20.27 -0.255 -0.075 -0.001 0.8157 -0.0010 0.0002 209334.21-52272.37 63022.46 145596.4****************** 0.000 38 20.83 -0.246 -0.071 0.027 0.8157 -0.0004 0.0003 202284.56-29737.93 54415.27 142037.0*********-825941.6 0.000 39 21.39 -0.237 -0.054 0.039 0.8157 0.0000 0.0003 195229.23-11928.74 41629.15 139422.3********* 848045.6 0.000 40 21.96 -0.228 -0.035 0.039 0.8157 0.0002 0.0002 188188.56 -88.51 28346.89 137085.1*********1519535.2 0.000 41 22.52 -0.219 -0.018 0.032 0.8157 0.0003 0.0001 181176.81 6271.96 16978.61 134793.3-376484.21524524.1 0.000 42 23.08 -0.211 -0.006 0.023 0.8157 0.0003 0.0001 174203.43 8491.82 8737.72 132497.9 579259.31171473.1 0.000 43 23.65 -0.203 0.001 0.013 0.8157 0.0002 0.0000 165689.23 7810.57 -388.82 130198.81071118.7 693459.6 0.000 44 24.21 -0.195 0.004 0.006 0.8157 0.0001 0.0000 157239.58 5174.22 -4517.90 127917.91049238.0 253793.5 0.000 45 24.77 -0.188 0.004 0.001 0.8156 0.0001 0.0000 148855.99 2421.46 -5350.48 125656.1 794926.6 -37470.1 0.000 46 25.33 -0.181 0.003 -0.001 0.8156 0.0000 0.0000 140539.15 420.23 -4428.31 123405.6 493746.4-173778.5 0.000 47 25.90 -0.175 0.001 -0.002 0.8156 0.0000 0.0000 132288.67 -642.60 -2865.58 121159.7 244474.4-197434.9 0.000 48 26.46 -0.169 0.000 -0.002 0.8156 0.0000 0.0000 124102.95 -946.60 -1308.54 118915.1 83169.2-161263.7 0.000 49 27.02 -0.163 0.000 -0.002 0.8156 0.0000 0.0000 117481.88 -864.03 -627.81 116670.8 9510.5-107979.4 0.000 50 27.59 -0.158 0.000 -0.001 0.8156 0.0000 0.0000 110932.12 -656.36 -165.86 114426.6 -25829.8 -59342.6 0.000 51 28.15 -0.153 -0.001 -0.001 0.8156 0.0000 0.0000 104450.81 -413.35 79.95 112182.4 -35166.6 -22395.7 0.000 52 28.71 -0.148 0.000 0.000 0.8156 0.0000 0.0000 98034.50 -186.50 144.70 109938.3 -30666.1 872.0 0.000 53 29.28 -0.144 0.000 0.000 0.8156 0.0000 0.0000 91679.05 7.18 70.45 107694.2 -22521.0 11370.4 0.000 54 29.84 -0.139 0.000 0.000 0.8155 0.0000 0.0000 88819.73 11.28 65.98 105450.2 -18555.6 10966.5 0.000 55 30.40 -0.135 0.000 0.000 0.8155 0.0000 0.0000 86071.31 14.45 59.91 103206.1 -14841.8 10331.5 0.000 56 30.96 -0.131 0.000 0.001 0.8155 0.0000 0.0000 83429.70 16.68 52.93 100962.1 -11469.4 9518.2 0.000 57 31.53 -0.128 0.000 0.001 0.8155 0.0000 0.0000 80891.02 18.04 45.58 98718.2 -8489.7 8579.2 0.000 58 32.09 -0.124 0.000 0.001 0.8155 0.0000 0.0000 78451.53 18.60 38.27 96474.2 -5923.8 7563.9 0.000 59 32.65 -0.120 0.000 0.001 0.8155 0.0000 0.0000 76115.61 18.50 31.27 94230.3 -3769.8 6516.7 0.000 60 33.22 -0.117 0.000 0.001 0.8155 0.0000 0.0000 73888.44 17.83 24.81 91986.4 -2009.3 5475.6 0.000 61 33.78 -0.114 0.000 0.001 0.8155 0.0000 0.0000 71765.46 16.75 19.01 89742.5 -612.5 4471.7 0.000 62 34.34 -0.110 0.000 0.000 0.8155 0.0000 0.0000 69742.30 15.35 13.92 87498.7 457.6 3529.1 0.000 63 34.91 -0.107 0.000 0.000 0.8155 0.0000 0.0000 67814.79 13.75 9.57 85254.9 1241.3 2665.3 0.000 64 35.47 -0.104 0.000 0.000 0.8155 0.0000 0.0000 65978.93 12.04 5.94 83011.1 1780.1 1891.4 0.000 65 36.03 -0.101 0.000 0.000 0.8155 0.0000 0.0000 64230.90 10.31 2.98 80767.3 2114.4 1213.5 0.000 66 36.59 -0.098 0.000 0.000 0.8154 0.0000 0.0000 62567.05 8.63 0.63 78523.5 2282.2 633.0 0.000 67 37.16 -0.095 0.000 0.000 0.8154 0.0000 0.0000 60983.87 7.03 -1.17 76279.8 2317.9 147.4 0.000 68 37.72 -0.092 0.000 0.000 0.8154 0.0000 0.0000 59478.00 5.56 -2.50 74036.0 2252.1 -248.3 0.000 69 38.28 -0.090 0.000 0.000 0.8154 0.0000 0.0000 58046.21 4.25 -3.44 71792.3 2111.2 -561.5 0.000 70 38.85 -0.087 0.000 0.000 0.8154 0.0000 0.0000 56686.28 3.10 -4.06 69548.6 1917.5 -800.8 0.000 71 39.41 -0.084 0.000 0.000 0.8154 0.0000 0.0000 55395.47 2.11 -4.43 67305.0 1688.8 -975.2 0.000 72 39.97 -0.082 0.000 0.000 0.8154 0.0000 0.0000 54170.85 1.28 -4.60 65061.3 1439.5 -1094.0 0.000 73 40.54 -0.079 0.000 0.000 0.8154 0.0000 0.0000 53009.61 0.62 -4.62 62817.7 1180.7 -1166.3 0.000 74 41.10 -0.077 0.000 0.000 0.8154 0.0000 0.0000 51909.05 0.10 -4.53 60574.0 920.9 -1201.1 0.000 75 41.66 -0.075 0.000 0.000 0.8154 0.0000 0.0000 49700.12 -0.91 -4.12 58330.4 666.1 -1206.7 0.000 76 42.22 -0.072 0.000 0.000 0.8154 0.0000 0.0000 47545.50 -1.66 -3.59 56086.8 434.1 -1155.4 0.000 77 42.79 -0.070 0.000 0.000 0.8154 0.0000 0.0000 45442.92 -2.16 -2.98 53843.3 232.2 -1062.1 0.000 78 43.35 -0.068 0.000 0.000 0.8154 0.0000 0.0000 43390.14 -2.44 -2.35 51599.7 64.6 -940.7 0.000 79 43.91 -0.066 0.000 0.000 0.8154 0.0000 0.0000 41384.96 -2.55 -1.73 49356.1 -67.5 -803.2 0.000 80 44.48 -0.064 0.000 0.000 0.8154 0.0000 0.0000 39425.25 -2.50 -1.16 47112.6 -165.0 -659.9 0.000 81 45.04 -0.063 0.000 0.000 0.8154 0.0000 0.0000 37508.88 -2.35 -0.66 44869.1 -230.5 -519.1 0.000 82 45.60 -0.061 0.000 0.000 0.8154 0.0000 0.0000 35633.77 -2.11 -0.24 42625.5 -267.8 -387.0 0.000 83 46.17 -0.059 0.000 0.000 0.8154 0.0000 0.0000 33797.87 -1.82 0.09 40382.0 -281.4 -268.3 0.000 84 46.73 -0.058 0.000 0.000 0.8153 0.0000 0.0000 31999.17 -1.52 0.35 38138.5 -276.1 -165.5 0.000 85 47.29 -0.056 0.000 0.000 0.8153 0.0000 0.0000 30235.67 -1.20 0.52 35895.0 -256.7 -80.2 0.000 86 47.85 -0.055 0.000 0.000 0.8153 0.0000 0.0000 28505.41 -0.90 0.62 33651.6 -227.6 -12.5 0.000 87 48.42 -0.054 0.000 0.000 0.8153 0.0000 0.0000 26806.46 -0.63 0.66 31408.1 -192.8 38.4 0.000 88 48.98 -0.052 0.000 0.000 0.8153 0.0000 0.0000 25136.90 -0.39 0.65 29164.6 -155.8 74.0 0.000 89 49.54 -0.051 0.000 0.000 0.8153 0.0000 0.0000 23494.83 -0.19 0.61 26921.2 -119.1 96.1 0.000 90 50.11 -0.050 0.000 0.000 0.8153 0.0000 0.0000 21878.38 -0.03 0.54 24677.7 -84.8 107.0 0.000 91 50.67 -0.049 0.000 0.000 0.8153 0.0000 0.0000 20285.69 0.09 0.46 22434.3 -54.3 108.7 0.000 92 51.23 -0.048 0.000 0.000 0.8153 0.0000 0.0000 18714.91 0.18 0.38 20190.8 -28.4 103.5 0.000 93 51.80 -0.047 0.000 0.000 0.8153 0.0000 0.0000 17164.21 0.24 0.29 17947.4 -7.2 93.3 0.000 94 52.36 -0.047 0.000 0.000 0.8153 0.0000 0.0000 15631.78 0.28 0.22 15703.9 9.2 79.8 0.000 95 52.92 -0.046 0.000 0.000 0.8153 0.0000 0.0000 14115.79 0.29 0.16 13460.5 21.6 64.2 0.000 96 53.48 -0.045 0.000 0.000 0.8153 0.0000 0.0000 12614.45 0.29 0.11 11217.1 30.5 47.8 0.000 97 54.05 -0.045 0.000 0.000 0.8153 0.0000 0.0000 11233.48 0.25 -0.11 8973.7 36.9 31.2 0.000 98 54.61 -0.044 0.000 0.000 0.8153 0.0000 0.0000 9865.40 0.18 -0.22 6730.3 30.4 17.2 0.000 99 55.17 -0.044 0.000 0.000 0.8153 0.0000 0.0000 8508.64 0.10 -0.21 4486.8 18.1 7.3 0.000 100 55.74 -0.043 0.000 0.000 0.8153 0.0000 0.0000 7161.64 0.03 -0.11 2243.4 6.0 1.7 0.000 101 56.30 -0.043 0.000 0.000 0.8153 0.0000 0.0000 7161.64 -0.03 0.11 2243.4 0.0 0.0 0.000 ** SACS COLLAPSE PILE DETAIL REPORT ** *** FINAL *** PILEHEAD JOINT 722 **** DEFLECTIONS **** ***** ROTATIONS ***** ************** ELASTIC INTERNAL LOADS *************** PLASTIC INCR DISTANCE X Y Z X Y Z FX FY FZ MX MY MZ RATIO M CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 1 0.00 0.245 15.083 0.000 0.0623 -0.0009 -0.0148 -18308.03 41015.05 -792.50 27370.4 71466.88017736.4 0.000 2 0.56 0.231 14.227 -0.004 0.0623 -0.0009 -0.0153 -18123.59 39671.36 -791.70 27066.6 26864.55708986.2 0.000 3 1.13 0.217 13.349 -0.010 0.0623 -0.0009 -0.0156 -18064.09 38054.01 -790.21 26846.7 -17697.43475872.6 0.000 4 1.69 0.202 12.459 -0.017 0.0623 -0.0009 -0.0157 -17990.61 36220.25 -787.60 26668.2 -62179.01333800.2 0.000 5 2.25 0.187 11.564 -0.024 0.0623 -0.0009 -0.0157 -17906.89 34202.80 -783.41 26493.6-106517.3-705049.7 0.000 6 2.82 0.172 10.672 -0.031 0.0623 -0.0008 -0.0156 -17816.50 32015.64 -777.10 26291.0-150623.0********* 0.000 7 3.38 0.157 9.790 -0.038 0.0623 -0.0008 -0.0154 -17722.43 29672.03 -768.11 26034.0-194376.8********* 0.000 8 3.94 0.143 8.926 -0.045 0.0623 -0.0008 -0.0150 -17587.63 26708.53 -753.40 25701.4-237627.1********* 0.000 9 4.50 0.130 8.085 -0.052 0.0623 -0.0008 -0.0146 -17404.25 22977.85 -730.07 25279.8-280052.0********* 0.000 10 5.07 0.118 7.274 -0.057 0.0623 -0.0008 -0.0140 -17195.84 18673.97 -696.88 24766.2-321165.2********* 0.000 11 5.63 0.106 6.498 -0.062 0.0623 -0.0008 -0.0134 -17046.10 14886.10 -661.54 24170.4-360411.1********* 0.000 12 6.19 0.096 5.759 -0.065 0.0623 -0.0007 -0.0127 -16947.36 11589.64 -624.85 23502.8-397668.8********* 0.000 13 6.76 0.086 5.063 -0.068 0.0623 -0.0007 -0.0120 -16906.69 8809.21 -588.31 22775.8-432861.5********* 0.000 14 7.32 0.078 4.409 -0.069 0.0623 -0.0007 -0.0112 -16917.67 6575.44 -553.91 22001.9-465997.6********* 0.000 15 7.88 0.070 3.802 -0.070 0.0623 -0.0006 -0.0104 -16970.60 4832.60 -522.69 21191.9-497197.2********* 0.000 16 8.44 0.064 3.241 -0.069 0.0623 -0.0006 -0.0095 -16988.02 2675.07 -477.60 20351.8-526639.1********* 0.000 17 9.01 0.059 2.728 -0.067 0.0622 -0.0006 -0.0087 -16975.10 148.02 -416.19 19494.0-553542.5********* 0.000 18 9.57 0.054 2.264 -0.065 0.0622 -0.0005 -0.0078 -16972.45 -2496.37 -341.61 18635.0-576988.3********* 0.000 19 10.13 0.050 1.849 -0.061 0.0622 -0.0005 -0.0070 -16979.80 -5192.76 -253.30 17790.8-596235.1********* 0.000 20 10.70 0.047 1.481 -0.057 0.0622 -0.0005 -0.0061 -16998.07 -7728.62 -156.62 16978.1-610510.0********* 0.000 21 11.26 0.044 1.161 -0.053 0.0622 -0.0004 -0.0053 -17025.43-10083.17 -51.63 16210.8-619341.5********* 0.000





3.298

22 11.82 0.042 0.886 -0.047 0.0622 -0.0004 -0.0045 -17060.17-12281.62 64.01 15500.3-622261.6********* 0.000 23 12.39 0.041 0.654 -0.042 0.0622 -0.0003 -0.0038 -17100.66-14231.12 187.03 14855.0-618671.0********* 0.000 24 12.95 0.039 0.463 -0.036 0.0622 -0.0003 -0.0031 -17146.16-15916.15 316.65 14280.1-608154.1********* 0.000 25 13.51 0.038 0.309 -0.031 0.0622 -0.0003 -0.0025 -17196.47-17387.25 459.13 13777.8-590339.1********* 0.000 26 14.07 0.037 0.190 -0.025 0.0622 -0.0002 -0.0019 -17251.10-18396.18 591.67 13345.2-564502.7********* 0.000 27 14.64 0.036 0.100 -0.020 0.0622 -0.0002 -0.0014 -17218.48-19083.07 726.73 12977.5-531204.2********* 0.000 28 15.20 0.035 0.037 -0.015 0.0622 -0.0001 -0.0010 -17191.70-19340.18 829.19 12666.7-490301.8********* 0.000 29 15.76 0.034 -0.004 -0.011 0.0622 -0.0001 -0.0006 -17171.15-19317.44 902.44 12403.4-443630.3********* 0.000 30 16.33 0.034 -0.027 -0.007 0.0622 -0.0001 -0.0004 -17156.99-19136.49 950.36 12177.5-392834.9********* 0.000 31 16.89 0.033 -0.037 -0.004 0.0622 -0.0001 -0.0001 -17149.27-18890.94 977.26 11979.0-339341.0********* 0.000 32 17.45 0.032 -0.036 -0.002 0.0622 0.0000 0.0000 -16846.10-13768.84 1191.87 11806.2-284331.9********* 0.000 33 18.02 0.031 -0.031 0.000 0.0622 0.0000 0.0001 -16537.00 -9198.43 1181.32 11636.8-217241.5-734138.7 0.000 34 18.58 0.030 -0.024 0.001 0.0622 0.0000 0.0001 -16221.84 -5516.38 1035.54 11467.4-150744.9-216356.1 0.000 35 19.14 0.030 -0.017 0.001 0.0622 0.0000 0.0001 -15900.94 -2808.74 829.10 11297.0 -92453.7 94162.6 0.000 36 19.70 0.029 -0.011 0.001 0.0622 0.0000 0.0001 -15574.89 -1003.59 617.04 11126.0 -45783.3 252267.4 0.000 37 20.27 0.028 -0.006 0.001 0.0622 0.0000 0.0001 -15244.37 55.31 434.77 10954.6 -11049.6 308759.7 0.000 38 20.83 0.028 -0.003 0.001 0.0622 0.0000 0.0001 -14739.87 980.11 186.06 10783.2 13424.0 305646.4 0.000 39 21.39 0.027 -0.001 0.000 0.0622 0.0000 0.0000 -14226.32 1253.04 24.16 10611.9 23897.5 250475.8 0.000 40 21.96 0.026 0.000 0.000 0.0622 0.0000 0.0000 -13704.43 1170.14 -65.06 10440.6 25257.6 179942.0 0.000 41 22.52 0.026 0.001 0.000 0.0622 0.0000 0.0000 -13174.82 942.63 -101.88 10269.4 21595.4 114074.2 0.000 42 23.08 0.025 0.001 0.000 0.0622 0.0000 0.0000 -12638.00 702.97 -106.42 10098.2 15860.7 61013.1 0.000 43 23.65 0.024 0.000 0.000 0.0622 0.0000 0.0000 -11903.41 360.97 -85.43 9927.0 9870.2 21442.5 0.000 44 24.21 0.024 0.000 0.000 0.0622 0.0000 0.0000 -11161.08 141.71 -56.54 9755.8 5061.2 1123.2 0.000 45 24.77 0.023 0.000 0.000 0.0622 0.0000 0.0000 -10410.90 23.04 -31.06 9584.6 1878.5 -6853.7 0.000 46 25.33 0.023 0.000 0.000 0.0622 0.0000 0.0000 -9652.64 -27.56 -13.05 9413.4 130.2 -8150.5 0.000 47 25.90 0.022 0.000 0.000 0.0622 0.0000 0.0000 -8885.88 -38.88 -2.47 9242.2 -604.5 -6599.1 0.000 48 26.46 0.022 0.000 0.000 0.0622 0.0000 0.0000 -8110.10 -31.12 2.53 9071.0 -743.3 -4410.5 0.000 49 27.02 0.022 0.000 0.000 0.0622 0.0000 0.0000 -7524.35 -23.08 3.33 8899.8 -601.1 -2658.8 0.000 50 27.59 0.021 0.000 0.000 0.0622 0.0000 0.0000 -6933.37 -14.86 3.07 8728.6 -413.3 -1359.9 0.000 51 28.15 0.021 0.000 0.000 0.0622 0.0000 0.0000 -6336.68 -8.12 2.27 8557.5 -240.8 -523.3 0.000 52 28.71 0.021 0.000 0.000 0.0622 0.0000 0.0000 -5733.67 -3.23 1.27 8386.3 -112.8 -66.0 0.000 53 29.28 0.020 0.000 0.000 0.0622 0.0000 0.0000 -5123.71 0.11 0.19 8215.1 -41.1 115.8 0.000 54 29.84 0.020 0.000 0.000 0.0622 0.0000 0.0000 -4991.77 0.16 0.16 8043.9 -30.3 109.9 0.000 55 30.40 0.020 0.000 0.000 0.0622 0.0000 0.0000 -4872.60 0.19 0.13 7872.7 -21.2 100.8 0.000 56 30.96 0.020 0.000 0.000 0.0622 0.0000 0.0000 -4765.93 0.21 0.11 7701.6 -13.6 89.9 0.000 57 31.53 0.020 0.000 0.000 0.0622 0.0000 0.0000 -4671.46 0.21 0.08 7530.4 -7.5 78.2 0.000 58 32.09 0.019 0.000 0.000 0.0622 0.0000 0.0000 -4588.96 0.20 0.06 7359.2 -2.8 66.5 0.000 59 32.65 0.019 0.000 0.000 0.0622 0.0000 0.0000 -4518.16 0.19 0.05 7188.1 0.8 55.2 0.000 60 33.22 0.019 0.000 0.000 0.0622 0.0000 0.0000 -4458.85 0.17 0.03 7016.9 3.4 44.8 0.000 61 33.78 0.019 0.000 0.000 0.0622 0.0000 0.0000 -4410.80 0.15 0.02 6845.7 5.1 35.4 0.000 62 34.34 0.019 0.000 0.000 0.0622 0.0000 0.0000 -4373.82 0.13 0.01 6674.6 6.2 27.1 0.000 63 34.91 0.018 0.000 0.000 0.0622 0.0000 0.0000 -4347.70 0.11 0.00 6503.4 6.7 20.0 0.000 64 35.47 0.018 0.000 0.000 0.0622 0.0000 0.0000 -4332.26 0.09 0.00 6332.2 6.9 14.1 0.000 65 36.03 0.018 0.000 0.000 0.0622 0.0000 0.0000 -4327.32 0.07 -0.01 6161.1 6.7 9.2 0.000 66 36.59 0.018 0.000 0.000 0.0622 0.0000 0.0000 -4332.73 0.05 -0.01 5989.9 6.3 5.2 0.000 67 37.16 0.018 0.000 0.000 0.0622 0.0000 0.0000 -4348.31 0.04 -0.01 5818.8 5.7 2.1 0.000 68 37.72 0.017 0.000 0.000 0.0622 0.0000 0.0000 -4373.91 0.03 -0.01 5647.6 5.1 -0.2 0.000 69 38.28 0.017 0.000 0.000 0.0622 0.0000 0.0000 -4409.38 0.02 -0.01 5476.4 4.4 -2.0 0.000 70 38.85 0.017 0.000 0.000 0.0622 0.0000 0.0000 -4454.73 0.01 -0.01 5305.3 3.8 -3.2 0.000 71 39.41 0.017 0.000 0.000 0.0622 0.0000 0.0000 -4509.89 0.01 -0.01 5134.1 3.1 -4.0 0.000 72 39.97 0.017 0.000 0.000 0.0622 0.0000 0.0000 -4574.71 0.00 -0.01 4963.0 2.5 -4.5 0.000 73 40.54 0.016 0.000 0.000 0.0622 0.0000 0.0000 -4649.03 0.00 -0.01 4791.8 1.9 -4.8 0.000 74 41.10 0.016 0.000 0.000 0.0622 0.0000 0.0000 -4732.73 0.00 -0.01 4620.7 1.3 -4.9 0.000 75 41.66 0.016 0.000 0.000 0.0622 0.0000 0.0000 -4577.00 -0.01 -0.01 4449.5 0.8 -4.8 0.000 76 42.22 0.016 0.000 0.000 0.0622 0.0000 0.0000 -4425.67 -0.01 -0.01 4278.4 0.4 -4.5 0.000 77 42.79 0.016 0.000 0.000 0.0622 0.0000 0.0000 -4278.59 -0.01 0.00 4107.3 0.1 -4.0 0.000 78 43.35 0.015 0.000 0.000 0.0622 0.0000 0.0000 -4135.60 -0.01 0.00 3936.1 -0.1 -3.5 0.000 79 43.91 0.015 0.000 0.000 0.0622 0.0000 0.0000 -3996.56 -0.01 0.00 3765.0 -0.3 -2.9 0.000 80 44.48 0.015 0.000 0.000 0.0622 0.0000 0.0000 -3861.32 -0.01 0.00 3593.8 -0.4 -2.4 0.000 81 45.04 0.015 0.000 0.000 0.0622 0.0000 0.0000 -3729.75 -0.01 0.00 3422.7 -0.4 -1.8 0.000 82 45.60 0.015 0.000 0.000 0.0622 0.0000 0.0000 -3601.71 -0.01 0.00 3251.6 -0.4 -1.4 0.000 83 46.17 0.014 0.000 0.000 0.0622 0.0000 0.0000 -3477.07 -0.01 0.00 3080.4 -0.4 -1.0 0.000 84 46.73 0.014 0.000 0.000 0.0622 0.0000 0.0000 -3355.70 0.00 0.00 2909.3 -0.4 -0.6 0.000 85 47.29 0.014 0.000 0.000 0.0622 0.0000 0.0000 -3237.47 0.00 0.00 2738.1 -0.3 -0.4 0.000 86 47.85 0.014 0.000 0.000 0.0622 0.0000 0.0000 -3122.26 0.00 0.00 2567.0 -0.3 -0.2 0.000 87 48.42 0.014 0.000 0.000 0.0622 0.0000 0.0000 -3009.95 0.00 0.00 2395.9 -0.2 0.0 0.000 88 48.98 0.014 0.000 0.000 0.0622 0.0000 0.0000 -2900.41 0.00 0.00 2224.7 -0.2 0.1 0.000 89 49.54 0.014 0.000 0.000 0.0622 0.0000 0.0000 -2793.53 0.00 0.00 2053.6 -0.1 0.2 0.000 90 50.11 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2689.19 0.00 0.00 1882.5 -0.1 0.2 0.000 91 50.67 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2587.29 0.00 0.00 1711.3 -0.1 0.2 0.000 92 51.23 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2487.72 0.00 0.00 1540.2 0.0 0.2 0.000 93 51.80 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2390.36 0.00 0.00 1369.1 0.0 0.2 0.000 94 52.36 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2295.10 0.00 0.00 1197.9 0.0 0.2 0.000 95 52.92 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2201.85 0.00 0.00 1026.8 0.0 0.1 0.000 96 53.48 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2110.51 0.00 0.00 855.7 0.0 0.1 0.000 97 54.05 0.013 0.000 0.000 0.0622 0.0000 0.0000 -2051.53 0.00 0.00 684.5 0.0 0.1 0.000 98 54.61 0.013 0.000 0.000 0.0622 0.0000 0.0000 -1994.91 0.00 0.00 513.4 0.0 0.0 0.000 99 55.17 0.012 0.000 0.000 0.0622 0.0000 0.0000 -1940.58 0.00 0.00 342.3 0.0 0.0 0.000 100 55.74 0.012 0.000 0.000 0.0622 0.0000 0.0000 -1888.47 0.00 0.00 171.1 0.0 0.0 0.000 101 56.30 0.012 0.000 0.000 0.0622 0.0000 0.0000 -1888.47 0.00 0.00 171.1 0.0 0.0 0.000 ************ SOLUTION STATISTICS ************** LOAD CASE ..................................... 12 NUMBER OF INCREMENTS .......................... 170 NUMBER OF STRUCTURE INTERATIONS ............... 785 NUMBER OF MEMBER INTERATIONS ..................45898 AVERAGE NUMBER OF INTERATIONS/MEMBER ..........136.2 *************** COLLAPSE SOLUTION SUMMARY *************** LOAD SEQUENCE 1 LOAD LOAD NO. * MAXIMUM DEFLECTION * ** MAXIMUM ROTATION ** ** SOLUTION DATA ** *** REACTION SUMMATION *** INCR CASE FACTOR LOOPS DEFL. JOINT DOF ROT. JOINT DOF MAX. JOINT DOF FX FY FZ CM DIGITS KG KG KG 1 11 0.10 1 1.040 490 DX 0.0015815 903 RY 3 872 DX 0.00 0.00 0.00 2 11 0.20 1 2.032 490 DX 0.0031549 903 RY 3 872 DX 0.00 0.00 0.00 3 11 0.30 1 3.086 490 DX 0.0047433 903 RY 3 872 DX 0.00 0.00 0.00





3.299

4 11 0.40 1 4.146 490 DX 0.0063347 903 RY 3 872 DX 0.00 0.00 0.00 5 11 0.50 1 5.212 490 DX 0.0079290 903 RY 3 872 DX 0.00 0.00 0.00 6 11 0.60 1 6.284 490 DX 0.0095262 903 RY 3 872 DX 0.00 0.00 0.00 7 11 0.70 1 7.362 490 DX 0.0111264 903 RY 3 872 DX 0.00 0.00 0.00 8 11 0.80 1 8.446 490 DX 0.0127295 903 RY 3 872 DX 0.00 0.00 0.00 9 11 0.90 1 9.536 490 DX 0.0143355 903 RY 3 872 DX 0.00 0.00 0.00 10 11 1.00 1 10.630 490 DX 0.0159447 901 RY 3 872 DX 0.00 0.00 0.00 11 9 0.01 1 11.255 490 DX 0.0162400 901 RY 3 872 DX 0.00 0.00 0.00 12 9 0.02 1 11.900 463 DX 0.0165386 901 RY 3 872 DX 0.00 0.00 0.00 13 9 0.03 1 12.547 463 DX 0.0168375 901 RY 3 872 DX 0.00 0.00 0.00 14 9 0.04 1 13.224 525 DX 0.0171366 903 RY 3 872 DX 0.00 0.00 0.00 15 9 0.05 1 13.924 525 DX 0.0174356 903 RY 3 872 DX 0.00 0.00 0.00 16 9 0.06 1 14.625 525 DX 0.0177346 903 RY 3 872 DX 0.00 0.00 0.00 17 9 0.07 1 15.326 525 DX 0.0180337 903 RY 3 872 DX 0.00 0.00 0.00 18 9 0.08 1 16.027 525 DX 0.0183326 903 RY 3 872 DX 0.00 0.00 0.00 19 9 0.09 1 16.728 525 DX 0.0186315 903 RY 3 872 DX 0.00 0.00 0.00 20 9 0.10 1 17.429 525 DX 0.0189303 903 RY 3 872 DX 0.00 0.00 0.00 21 9 0.11 1 18.130 525 DX 0.0192291 903 RY 3 872 DX 0.00 0.00 0.00 22 9 0.12 1 18.833 525 DX 0.0195278 903 RY 4 509 DY 0.00 0.00 0.00 23 9 0.13 1 19.537 525 DX 0.0198263 903 RY 4 509 DY 0.00 0.00 0.00 24 9 0.14 1 20.243 525 DX 0.0201247 903 RY 4 509 DY 0.00 0.00 0.00 25 9 0.15 1 20.951 525 DX 0.0204230 903 RY 4 509 DY 0.00 0.00 0.00 26 9 0.16 1 21.662 525 DX 0.0207210 903 RY 4 509 DY 0.00 0.00 0.00 27 9 0.17 1 22.375 525 DX 0.0210188 903 RY 4 509 DY 0.00 0.00 0.00 28 9 0.18 1 23.091 525 DX 0.0213162 903 RY 4 509 DY 0.00 0.00 0.00 29 9 0.19 1 23.806 525 DX 0.0216134 903 RY 4 509 DY 0.00 0.00 0.00 30 9 0.20 1 24.525 525 DX 0.0219104 903 RY 4 509 DY 0.00 0.00 0.00 31 9 0.21 1 25.241 525 DX 0.0222075 903 RY 4 509 DY 0.00 0.00 0.00 32 9 0.22 1 25.962 525 DX 0.0225047 903 RY 4 509 DY 0.00 0.00 0.00 33 9 0.23 1 26.683 525 DX 0.0228018 903 RY 4 509 DY 0.00 0.00 0.00 34 9 0.24 1 27.407 525 DX 0.0230986 903 RY 4 509 DY 0.00 0.00 0.00 35 9 0.25 1 28.136 525 DX 0.0233949 903 RY 4 509 DY 0.00 0.00 0.00 36 9 0.26 1 28.866 525 DX 0.0236913 903 RY 4 509 DY 0.00 0.00 0.00 37 9 0.27 1 29.600 525 DX 0.0239874 903 RY 4 509 DY 0.00 0.00 0.00 38 9 0.28 1 30.331 525 DX 0.0242836 903 RY 4 509 DY 0.00 0.00 0.00 39 9 0.29 1 31.068 525 DX 0.0245796 903 RY 4 509 DY 0.00 0.00 0.00 40 9 0.30 1 31.808 525 DX 0.0248753 903 RY 4 509 DY 0.00 0.00 0.00 41 9 0.31 1 32.550 525 DX 0.0251708 903 RY 4 509 DY 0.00 0.00 0.00 42 9 0.32 1 33.295 525 DX 0.0254662 903 RY 4 509 DY 0.00 0.00 0.00 43 9 0.33 1 34.042 525 DX 0.0257615 903 RY 4 509 DY 0.00 0.00 0.00 44 9 0.34 1 34.792 525 DX 0.0260565 903 RY 4 509 DY 0.00 0.00 0.00 45 9 0.35 1 35.544 525 DX 0.0263514 903 RY 4 509 DY 0.00 0.00 0.00 46 9 0.36 1 36.299 525 DX 0.0266461 903 RY 4 509 DY 0.00 0.00 0.00 47 9 0.37 1 37.057 525 DX 0.0269406 903 RY 4 509 DY 0.00 0.00 0.00 48 9 0.38 1 37.818 525 DX 0.0272349 903 RY 4 509 DY 0.00 0.00 0.00 49 9 0.39 1 38.581 525 DX 0.0275290 903 RY 4 509 DY 0.00 0.00 0.00 50 9 0.40 1 39.347 525 DX 0.0278229 903 RY 4 509 DY 0.00 0.00 0.00 51 9 0.41 1 40.123 525 DX 0.0281177 903 RY 4 509 DY 0.00 0.00 0.00 52 9 0.42 1 40.887 525 DX 0.0284105 903 RY 4 509 DY 0.00 0.00 0.00 53 9 0.43 1 41.672 525 DX 0.0287023 903 RY 4 509 DY 0.00 0.00 0.00 54 9 0.44 1 42.437 525 DX 0.0289971 903 RY 4 509 DY 0.00 0.00 0.00 55 9 0.45 1 43.217 525 DX 0.0292918 903 RY 4 509 DY 0.00 0.00 0.00 56 9 0.46 1 43.995 525 DX 0.0295853 903 RY 4 509 DY 0.00 0.00 0.00 57 9 0.47 1 44.793 525 DX 0.0298770 903 RY 4 509 DY 0.00 0.00 0.00 58 9 0.48 1 45.581 525 DX 0.0301705 903 RY 4 509 DY 0.00 0.00 0.00 59 9 0.49 1 46.365 525 DX 0.0304627 903 RY 4 509 DY 0.00 0.00 0.00 60 9 0.50 1 47.180 525 DX 0.0307537 903 RY 4 509 DY 0.00 0.00 0.00 61 9 0.51 1 47.971 525 DX 0.0310465 903 RY 4 509 DY 0.00 0.00 0.00 62 9 0.52 1 48.764 525 DX 0.0313391 903 RY 4 509 DY 0.00 0.00 0.00 63 9 0.53 1 49.557 525 DX 0.0316315 903 RY 4 509 DY 0.00 0.00 0.00 64 9 0.54 1 50.370 525 DX 0.0319233 903 RY 4 509 DY 0.00 0.00 0.00 65 9 0.55 1 51.156 525 DX 0.0322161 903 RY 4 509 DY 0.00 0.00 0.00 66 9 0.56 1 51.953 525 DX 0.0325086 903 RY 4 509 DY 0.00 0.00 0.00 67 9 0.57 1 52.752 525 DX 0.0328008 903 RY 4 509 DY 0.00 0.00 0.00 68 9 0.58 1 53.557 525 DX 0.0330927 903 RY 4 509 DY 0.00 0.00 0.00 69 9 0.59 1 54.379 525 DX 0.0333839 903 RY 4 509 DY 0.00 0.00 0.00 70 9 0.60 1 55.186 525 DX 0.0336757 903 RY 4 509 DY 0.00 0.00 0.00 71 9 0.61 1 55.993 525 DX 0.0339675 903 RY 4 509 DY 0.00 0.00 0.00 72 9 0.62 1 56.792 525 DX 0.0342598 903 RY 4 509 DY 0.00 0.00 0.00 73 9 0.63 1 57.602 525 DX 0.0345514 903 RY 4 509 DY 0.00 0.00 0.00 74 9 0.64 1 58.432 525 DX 0.0348422 903 RY 4 509 DY 0.00 0.00 0.00 75 9 0.65 1 59.247 525 DX 0.0351336 903 RY 4 509 DY 0.00 0.00 0.00 76 9 0.66 1 60.064 525 DX 0.0354250 903 RY 4 509 DY 0.00 0.00 0.00 77 9 0.67 1 60.885 525 DX 0.0357162 903 RY 4 509 DY 0.00 0.00 0.00 78 9 0.68 1 61.707 525 DX 0.0360074 903 RY 4 509 DY 0.00 0.00 0.00 79 9 0.69 1 62.532 525 DX 0.0362984 903 RY 4 509 DY 0.00 0.00 0.00 80 9 0.70 1 63.358 525 DX 0.0365896 903 RY 4 509 DY 0.00 0.00 0.00 81 9 0.71 1 64.185 525 DX 0.0368805 903 RY 4 509 DY 0.00 0.00 0.00 82 9 0.72 1 65.016 525 DX 0.0371714 903 RY 4 509 DY 0.00 0.00 0.00 83 9 0.73 1 65.849 525 DX 0.0374621 903 RY 4 509 DY 0.00 0.00 0.00 84 9 0.74 1 66.682 525 DX 0.0377529 903 RY 4 509 DY 0.00 0.00 0.00 85 9 0.75 1 67.519 525 DX 0.0380435 903 RY 4 509 DY 0.00 0.00 0.00 86 9 0.76 1 68.358 525 DX 0.0383341 903 RY 4 509 DY 0.00 0.00 0.00 87 9 0.77 1 69.198 525 DX 0.0386245 903 RY 4 509 DY 0.00 0.00 0.00 88 9 0.78 1 70.039 525 DX 0.0389149 903 RY 4 509 DY 0.00 0.00 0.00 89 9 0.79 1 70.881 525 DX 0.0392054 903 RY 4 509 DY 0.00 0.00 0.00 90 9 0.80 1 71.724 525 DX 0.0394957 903 RY 4 509 DY 0.00 0.00 0.00 91 9 0.81 1 72.571 525 DX 0.0397860 903 RY 4 509 DY 0.00 0.00 0.00 92 9 0.82 1 73.419 525 DX 0.0400762 903 RY 4 509 DY 0.00 0.00 0.00 93 9 0.83 1 74.269 525 DX 0.0403663 903 RY 4 509 DY 0.00 0.00 0.00 94 9 0.84 1 75.119 525 DX 0.0406564 903 RY 4 509 DY 0.00 0.00 0.00 95 9 0.85 1 75.974 525 DX 0.0409465 903 RY 4 509 DY 0.00 0.00 0.00 96 9 0.86 1 76.829 525 DX 0.0412365 903 RY 4 509 DY 0.00 0.00 0.00 97 9 0.87 1 77.684 525 DX 0.0415265 903 RY 4 509 DY 0.00 0.00 0.00 98 9 0.88 1 78.543 525 DX 0.0418163 903 RY 4 509 DY 0.00 0.00 0.00 99 9 0.89 1 79.402 525 DX 0.0421061 903 RY 4 509 DY 0.00 0.00 0.00 100 9 0.90 1 80.266 525 DX 0.0423958 903 RY 4 509 DY 0.00 0.00 0.00





3.300

101 9 0.91 1 81.131 525 DX 0.0426854 903 RY 4 509 DY 0.00 0.00 0.00 102 9 0.92 1 81.996 525 DX 0.0429751 903 RY 4 509 DY 0.00 0.00 0.00 103 9 0.93 3 82.891 525 DX 0.0432719 903 RY 4 509 DY 0.00 0.00 0.00 104 9 0.94 1 83.733 525 DX 0.0435546 903 RY 4 509 DY 0.00 0.00 0.00 105 9 0.95 1 84.602 525 DX 0.0438438 903 RY 4 509 DY 0.00 0.00 0.00 106 9 0.96 1 85.473 525 DX 0.0441332 903 RY 4 509 DY 0.00 0.00 0.00 107 9 0.97 1 86.346 525 DX 0.0444225 903 RY 4 509 DY 0.00 0.00 0.00 108 9 0.98 3 87.249 525 DX 0.0447189 903 RY 4 509 DY 0.00 0.00 0.00 109 9 0.99 1 88.098 525 DX 0.0450015 903 RY 4 509 DY 0.00 0.00 0.00 110 9 1.00 1 88.974 525 DX 0.0452903 903 RY 4 509 DY 0.00 0.00 0.00 111 12 0.01 1 89.610 525 DX 0.0455786 903 RY 4 509 DY 0.00 0.00 0.00 112 12 0.02 3 90.258 525 DX 0.0458719 903 RY 4 509 DY 0.00 0.00 0.00 113 12 0.03 1 90.868 525 DX 0.0461536 903 RY 4 509 DY 0.00 0.00 0.00 114 12 0.04 1 91.495 525 DX 0.0464404 903 RY 4 509 DY 0.00 0.00 0.00 115 12 0.05 1 92.124 525 DX 0.0467274 903 RY 4 509 DY 0.00 0.00 0.00 116 12 0.06 3 92.773 525 DX 0.0470204 903 RY 4 509 DY 0.00 0.00 0.00 117 12 0.07 1 93.383 525 DX 0.0473019 903 RY 4 509 DY 0.00 0.00 0.00 118 12 0.08 3 94.034 525 DX 0.0475961 903 RY 4 509 DY 0.00 0.00 0.00 119 12 0.09 1 94.647 525 DX 0.0478789 903 RY 4 509 DY 0.00 0.00 0.00 120 12 0.10 1 95.282 525 DX 0.0481687 903 RY 4 509 DY 0.00 0.00 0.00 121 12 0.11 1 95.922 525 DX 0.0484612 903 RY 4 509 DY 0.00 0.00 0.00 122 12 0.12 3 96.597 525 DX 0.0487674 903 RY 4 509 DY 0.00 0.00 0.00 123 12 0.13 1 97.212 525 DX 0.0490506 903 RY 4 509 DY 0.00 0.00 0.00 124 12 0.14 3 97.883 525 DX 0.0493540 903 RY 4 509 DY 0.00 0.00 0.00 125 12 0.15 3 98.528 525 DX 0.0496480 903 RY 4 509 DY 0.00 0.00 0.00 126 12 0.16 3 99.172 525 DX 0.0499420 903 RY 4 509 DY 0.00 0.00 0.00 127 12 0.17 1 99.788 525 DX 0.0502251 903 RY 4 509 DY 0.00 0.00 0.00 128 12 0.18 3 100.473 525 DX 0.0505355 903 RY 4 509 DY 0.00 0.00 0.00 129 12 0.19 1 101.090 525 DX 0.0508190 903 RY 4 509 DY 0.00 0.00 0.00 130 12 0.20 3 101.777 525 DX 0.0511307 903 RY 4 509 DY 0.00 0.00 0.00 131 12 0.21 3 102.442 525 DX 0.0514344 903 RY 4 509 DY 0.00 0.00 0.00 132 12 0.22 3 103.168 525 DX 0.0517711 903 RY 4 509 DY 0.00 0.00 0.00 133 12 0.23 3 103.904 525 DX 0.0521129 903 RY 4 509 DY 0.00 0.00 0.00 134 12 0.24 3 104.638 525 DX 0.0524533 903 RY 4 509 DY 0.00 0.00 0.00 135 12 0.25 3 105.374 525 DX 0.0527941 903 RY 4 509 DY 0.00 0.00 0.00 136 12 0.26 3 106.110 525 DX 0.0531352 903 RY 4 509 DY 0.00 0.00 0.00 137 12 0.27 3 106.849 525 DX 0.0534777 903 RY 4 509 DY 0.00 0.00 0.00 138 12 0.28 3 107.594 525 DX 0.0538229 903 RY 4 509 DY 0.00 0.00 0.00 139 12 0.29 3 108.419 525 DX 0.0542125 903 RY 4 509 DY 0.00 0.00 0.00 140 12 0.30 5 109.200 525 DX 0.0545795 903 RY 4 509 DY 0.00 0.00 0.00 141 12 0.31 7 110.014 525 DX 0.0549646 903 RY 4 509 DY 0.00 0.00 0.00 142 12 0.32 7 110.815 525 DX 0.0553429 903 RY 4 509 DY 0.00 0.00 0.00 143 12 0.33 7 111.621 525 DX 0.0557230 903 RY 4 509 DY 0.00 0.00 0.00 144 12 0.34 7 112.440 525 DX 0.0561096 903 RY 4 509 DY 0.00 0.00 0.00 145 12 0.35 11 114.977 525 DX 0.0576053 903 RY 4 509 DY 0.00 0.00 0.00 146 12 0.36 4 116.052 525 DX 0.0581441 903 RY 4 509 DY 0.00 0.00 0.00 147 12 0.37 4 117.133 525 DX 0.0586815 903 RY 4 509 DY 0.00 0.00 0.00 148 12 0.38 5 118.293 525 DX 0.0592623 903 RY 4 509 DY 0.00 0.00 0.00 149 12 0.39 5 119.442 525 DX 0.0598372 903 RY 4 509 DY 0.00 0.00 0.00 150 12 0.40 19 120.953 525 DX 0.0606299 903 RY 4 509 DY 0.00 0.00 0.00 151 12 0.41 19 121.980 525 DX 0.0611300 903 RY 4 509 DY 0.00 0.00 0.00 152 12 0.42 19 123.023 525 DX 0.0616370 903 RY 4 509 DY 0.00 0.00 0.00 153 12 0.43 19 124.139 525 DX 0.0621843 903 RY 4 509 DY 0.00 0.00 0.00 154 12 0.44 19 125.353 525 DX 0.0627837 903 RY 4 509 DY 0.00 0.00 0.00 155 12 0.45 19 126.982 525 DX 0.0636028 903 RY 4 509 DY 0.00 0.00 0.00 156 12 0.46 19 128.999 525 DX 0.0646419 903 RY 4 509 DY 0.00 0.00 0.00 157 12 0.47 19 131.609 525 DX 0.0660121 903 RY 4 509 DY 0.00 0.00 0.00 158 12 0.48 8 133.141 525 DX 0.0667826 903 RY 4 509 DY 0.00 0.00 0.00 159 12 0.49 19 134.459 525 DX 0.0674482 903 RY 4 509 DY 0.00 0.00 0.00 160 12 0.50 19 135.760 525 DX 0.0681009 903 RY 4 509 DY 0.00 0.00 0.00 161 12 0.51 17 137.244 525 DX 0.0688606 903 RY 4 509 DY 0.00 0.00 0.00 162 12 0.52 19 138.795 525 DX 0.0696561 903 RY 4 509 DY 0.00 0.00 0.00 163 12 0.53 19 140.317 525 DX 0.0704401 903 RY 4 509 DY 0.00 0.00 0.00 164 12 0.54 19 141.859 525 DX 0.0712360 903 RY 4 509 DY 0.00 0.00 0.00 165 12 0.55 19 143.501 525 DX 0.0720859 903 RY 4 509 DY 0.00 0.00 0.00 166 12 0.56 19 147.286 525 DX 0.0741163 903 RY 4 509 DY 0.00 0.00 0.00 167 12 0.57 19 150.706 525 DX 0.0759545 903 RY 4 509 DY 0.00 0.00 0.00 168 12 0.58 19 154.336 525 DX 0.0778568 903 RY 4 509 DY 0.00 0.00 0.00 169 12 0.59 19 159.067 525 DX -0.1349915 841 RZ 4 509 DY 0.00 0.00 0.00 170 12 0.60 4 167.343 525 DX -0.3279752 842 RZ 4 509 DY 0.00 0.00 0.00 ************************* PILEHEAD SUMMARY REPORT ************************* LOAD SEQUENCE 1 AXIAL PILE INCR **** DEFLECTIONS **** ***** ROTATIONS ***** ******** FORCES ******** ******* MOMENTS ******* CAPACITY JOINT NO. X Y Z X Y Z X Y Z X Y Z RATIO CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 102 1 0.018 0.007 0.000 0.0000 0.0000 0.0000 14350.7 26.4 -19.6 2.2 14046.3 -42933.8 0.014 2 0.072 0.016 0.000 0.0000 0.0000 0.0000 -29821.5 28.1 -38.8 4.1 27720.4-135346.4 0.033 3 0.090 0.023 0.000 0.0000 0.0000 0.0000 -44879.8 63.6 -57.0 6.4 42017.5-175402.5 0.049 4 0.108 0.030 0.000 0.0000 0.0000 -0.0001 -59875.5 99.9 -74.0 8.6 56322.9-215251.9 0.066 5 0.127 0.037 0.000 0.0000 0.0000 -0.0001 -74874.6 138.5 -89.9 10.8 70628.2-254386.9 0.082 6 0.145 0.044 0.000 0.0000 0.0000 -0.0001 -89877.3 179.4 -104.6 13.1 84916.8-292790.5 0.098 7 0.163 0.051 0.000 0.0001 0.0000 -0.0001-104883.5 222.2 -118.8 15.3 98033.2-330801.6 0.115 8 0.181 0.059 0.000 0.0001 0.0000 -0.0001-119878.1 266.8 -133.0 17.5 109776.0-368493.6 0.131 9 0.200 0.066 0.000 0.0001 0.0000 -0.0001-134865.2 313.5 -146.5 19.7 121015.3-405912.4 0.148 10 0.218 0.074 0.000 0.0001 0.0000 -0.0001-149899.9 362.0 -159.4 22.0 131760.5-443237.6 0.164 11 0.212 0.028 0.000 0.0001 0.0000 -0.0001-145077.1 -557.2 -146.3 19.8 120909.8-743895.4 0.159 12 0.206 0.020 0.000 0.0001 0.0000 0.0001-140086.9 1518.7 161.0 17.8-133045.51056956.0 0.153 13 0.200 0.068 0.000 0.0001 0.0000 0.0000-135091.5 2485.0 151.9 15.7-125517.51373222.2 0.148 14 0.194 0.116 0.000 0.0000 0.0000 0.0000-130097.9 3450.5 148.7 13.7-122820.41688881.2 0.142 15 0.188 0.164 0.000 0.0000 0.0000 0.0000-125103.5 4416.2 146.2 11.6-120716.52004520.8 0.137 16 0.182 0.212 0.000 0.0000 0.0000 -0.0001-120115.9 5381.9 143.9 9.5-118812.72320226.7 0.131 17 0.176 0.260 0.000 0.0000 0.0000 -0.0001-115122.2 6347.7 141.7 7.4-117006.12635955.5 0.126 18 0.170 0.308 0.000 0.0000 0.0000 -0.0001-110129.2 7313.7 139.6 5.3-115256.72951740.4 0.121 19 0.164 0.356 0.000 0.0000 0.0000 -0.0002-105146.8 8279.8 137.6 3.1-113547.13267589.8 0.115





3.301

20 0.158 0.404 0.000 0.0000 0.0000 -0.0002-100154.9 9246.0 135.6 1.0-111869.33583419.5 0.110 21 0.152 0.452 0.000 0.0000 0.0000 -0.0002 -95163.1 10212.3 133.6 -1.1-110217.53899266.8 0.104 22 0.145 0.501 0.000 0.0000 0.0000 -0.0003 -90166.4 11189.5 131.4 -3.3-108354.34219090.0 0.099 23 0.139 0.552 0.000 0.0000 0.0000 -0.0003 -85149.9 12214.7 129.1 -5.2-106383.54556310.1 0.093 24 0.133 0.604 0.000 0.0000 0.0000 -0.0003 -80119.2 13277.4 127.1 -6.8-104718.74907015.1 0.088 25 0.127 0.660 0.000 0.0000 0.0000 -0.0004 -75068.5 14375.4 125.9 -7.6-103687.15276089.7 0.082 26 0.121 0.717 0.000 0.0000 0.0000 -0.0004 -69999.6 15451.8 123.9 -8.3-102118.15660354.8 0.077 27 0.115 0.778 0.000 0.0000 0.0000 -0.0004 -64905.9 16525.9 122.3 -8.4-100929.66065705.4 0.071 28 0.109 0.841 0.000 0.0000 0.0000 -0.0005 -59798.1 17578.6 120.6 -8.8 -99731.36476825.7 0.065 29 0.103 0.904 0.000 0.0000 0.0000 -0.0005 -54703.7 18563.7 118.8 -9.8 -98531.16872348.4 0.060 30 0.097 0.971 0.000 0.0000 0.0000 -0.0005 -49575.1 19608.8 117.1 -10.0 -97412.07303274.0 0.054 31 0.090 1.037 0.000 0.0000 0.0000 -0.0006 -44459.5 20616.9 115.2 -9.6 -96107.57720496.9 0.049 32 0.084 1.102 0.000 0.0000 0.0000 -0.0006 -39348.8 21579.4 114.4 -12.8 -95700.88123275.3 0.043 33 0.078 1.167 0.000 -0.0001 0.0000 -0.0007 -34230.6 22479.2 111.1 -14.5 -93211.68493511.6 0.037 34 0.072 1.239 0.000 -0.0001 0.0000 -0.0007 -29076.7 23465.7 109.1 -15.1 -91922.88921880.8 0.032 35 0.066 1.314 0.000 -0.0001 0.0000 -0.0007 -23904.0 24460.4 107.1 -16.3 -90547.09363480.4 0.026 36 0.060 1.391 0.000 -0.0001 0.0000 -0.0008 -18723.9 25444.6 105.2 -16.5 -89363.59810543.8 0.020 37 0.054 1.471 0.000 -0.0001 0.0000 -0.0008 -13530.1 26450.6 103.1 -17.3 -88007.6********* 0.015 38 0.047 1.552 0.000 -0.0001 0.0000 -0.0009 -8347.9 27437.2 101.8 -14.5 -87305.5********* 0.009 39 0.041 1.636 0.000 -0.0001 0.0000 -0.0009 -3141.5 28426.5 99.9 -14.1 -86117.1********* 0.003 40 0.035 1.723 0.000 -0.0001 0.0000 -0.0010 2079.9 29441.6 98.1 -13.8 -84957.0********* 0.002 41 0.029 1.813 0.000 -0.0001 0.0000 -0.0010 7311.7 30453.6 96.3 -13.4 -83811.6********* 0.007 42 0.023 1.905 0.000 0.0000 0.0000 -0.0011 12552.7 31470.7 94.5 -12.8 -82685.2********* 0.012 43 0.017 2.000 0.000 0.0000 0.0000 -0.0011 17806.9 32496.5 92.8 -11.9 -81625.2********* 0.017 44 0.011 2.097 0.000 0.0000 0.0000 -0.0012 23069.9 33498.0 91.1 -10.7 -80557.9********* 0.022 45 0.004 2.197 0.000 0.0000 0.0000 -0.0012 28341.9 34489.7 89.4 -9.4 -79529.1********* 0.027 102 46 -0.002 2.301 0.000 0.0000 0.0000 -0.0012 33630.5 35498.6 87.8 -8.1 -78498.1********* 0.032 47 -0.008 2.407 0.000 0.0000 0.0000 -0.0013 38929.3 36483.2 86.1 -6.5 -77455.6********* 0.037 48 -0.014 2.515 0.000 0.0000 0.0000 -0.0013 44232.8 37478.8 84.5 -4.8 -76458.8********* 0.043 49 -0.020 2.626 0.000 0.0000 0.0000 -0.0014 49546.5 38454.8 82.9 -3.2 -75414.3********* 0.048 50 -0.026 2.741 0.000 0.0000 0.0000 -0.0014 54874.7 39461.6 81.3 -1.9 -74388.0********* 0.053 51 -0.032 2.864 0.000 0.0000 0.0000 -0.0015 60264.5 40541.9 79.6 1.1 -73344.6********* 0.058 52 -0.038 2.977 0.000 0.0000 0.0000 -0.0015 65548.9 41501.5 78.1 1.2 -72287.0********* 0.063 53 -0.044 3.115 0.000 0.0000 0.0000 -0.0016 70971.3 42799.0 76.1 6.0 -70921.0********* 0.068 54 -0.050 3.222 0.000 0.0000 0.0000 -0.0016 76257.6 43603.5 75.1 4.0 -70214.3********* 0.073 55 -0.057 3.347 0.000 0.0000 0.0000 -0.0017 81663.1 44628.1 73.6 6.0 -69136.5********* 0.079 56 -0.063 3.472 0.000 0.0000 0.0000 -0.0018 87018.5 45608.5 72.0 6.7 -68059.4********* 0.084 57 -0.069 3.623 0.000 0.0000 0.0000 -0.0018 92502.3 46954.5 70.0 12.5 -66577.3********* 0.089 58 -0.075 3.746 0.000 0.0000 0.0000 -0.0019 97862.0 47833.2 68.9 6.9 -65662.4********* 0.094 59 -0.081 3.887 0.000 0.0000 0.0000 -0.0019 103321.8 48884.4 67.3 14.3 -64634.2********* 0.100 60 -0.087 4.054 0.000 0.0001 0.0000 -0.0020 108867.2 50287.3 64.2 20.0 -62047.8********* 0.105 61 -0.092 4.191 0.000 0.0001 0.0000 -0.0020 114226.4 51316.9 67.2 20.4 -65285.5********* 0.110 62 -0.098 4.329 0.000 0.0001 0.0000 -0.0021 119637.0 52332.3 62.1 21.2 -60554.4********* 0.115 63 -0.104 4.469 0.000 0.0001 0.0000 -0.0021 125054.2 53355.6 63.5 22.5 -62170.4********* 0.120 64 -0.110 4.621 0.000 0.0000 0.0000 -0.0022 130562.9 54434.9 61.2 14.7 -60101.0********* 0.126 65 -0.116 4.759 0.000 0.0001 0.0000 -0.0022 135918.8 55428.7 57.9 23.8 -57191.7********* 0.131 66 -0.122 4.903 0.000 0.0001 0.0000 -0.0023 141352.0 56443.9 58.2 26.5 -57809.9********* 0.136 67 -0.127 5.049 0.000 0.0001 0.0000 -0.0024 146791.3 57471.8 57.2 28.4 -57032.5********* 0.141 68 -0.133 5.200 0.000 0.0001 0.0000 -0.0024 152251.2 58517.3 56.2 30.3 -56259.7********* 0.147 69 -0.139 5.361 0.000 0.0001 0.0000 -0.0025 157792.1 59628.4 55.2 22.5 -55304.2********* 0.152 70 -0.145 5.514 0.000 0.0001 0.0000 -0.0025 163231.5 60681.9 52.6 24.1 -52929.9********* 0.157 71 -0.150 5.666 0.000 0.0001 0.0000 -0.0026 168688.3 61710.8 52.0 25.8 -52536.2********* 0.162 72 -0.156 5.817 0.000 0.0001 0.0000 -0.0026 174104.9 62731.4 50.0 36.0 -50883.5********* 0.168 73 -0.161 5.975 0.000 0.0001 0.0000 -0.0027 179588.8 63786.7 49.7 39.9 -50836.7********* 0.173 74 -0.167 6.142 0.000 0.0001 0.0000 -0.0028 185155.3 64894.2 49.5 31.8 -50665.3********* 0.178 75 -0.173 6.304 0.000 0.0001 0.0000 -0.0028 190623.3 65965.5 46.3 34.6 -47584.7********* 0.184 76 -0.178 6.466 0.000 0.0001 0.0000 -0.0029 196115.5 67020.5 46.5 36.6 -48002.4********* 0.189 77 -0.184 6.632 0.000 0.0001 0.0000 -0.0029 201620.6 68084.8 44.8 38.2 -46452.5********* 0.194 78 -0.189 6.799 0.000 0.0001 0.0000 -0.0030 207137.9 69149.1 43.4 40.6 -45223.6********* 0.199 79 -0.195 6.969 0.000 0.0001 0.0000 -0.0031 212657.0 70222.4 42.6 43.3 -44563.9********* 0.205 80 -0.200 7.139 0.000 0.0001 0.0000 -0.0031 218183.6 71294.7 41.1 45.7 -43205.2********* 0.210 81 -0.205 7.311 0.000 0.0001 0.0000 -0.0032 223708.9 72356.8 40.5 48.2 -42753.2********* 0.215 82 -0.211 7.486 0.000 0.0001 0.0000 -0.0033 229245.2 73424.8 39.2 50.3 -41548.6********* 0.221 83 -0.216 7.663 0.000 0.0001 0.0000 -0.0033 234795.4 74497.1 37.6 52.9 -40002.7********* 0.226 84 -0.221 7.841 0.000 0.0001 0.0000 -0.0034 240336.1 75562.3 36.7 55.5 -39299.3********* 0.231 85 -0.227 8.021 0.000 0.0001 0.0000 -0.0034 245897.0 76634.4 36.5 57.1 -39204.6********* 0.237 86 -0.232 8.204 0.000 0.0001 0.0000 -0.0035 251457.3 77717.1 34.3 60.1 -37031.5********* 0.242 87 -0.237 8.388 0.000 0.0001 0.0000 -0.0036 257027.8 78802.5 33.2 63.0 -35996.6********* 0.248 88 -0.242 8.572 0.000 0.0001 0.0000 -0.0036 262589.0 79886.8 32.3 65.2 -35214.0********* 0.253 89 -0.248 8.757 0.000 0.0001 0.0000 -0.0037 268156.1 80975.1 31.3 67.5 -34254.8********* 0.258 90 -0.253 8.943 0.000 0.0001 0.0000 -0.0038 273727.2 82064.1 30.2 69.6 -33191.4********* 0.264 102 91 -0.258 9.132 0.000 0.0001 0.0000 -0.0038 279316.0 83161.2 29.5 71.3 -32649.4********* 0.269 92 -0.263 9.323 0.000 0.0001 0.0000 -0.0039 284906.4 84263.2 27.6 73.9 -30681.7********* 0.274 93 -0.268 9.515 0.000 0.0001 0.0000 -0.0040 290496.3 85370.0 26.8 76.2 -29970.9********* 0.280 94 -0.273 9.707 0.000 0.0001 0.0000 -0.0040 296080.3 86467.5 26.0 78.3 -29188.6********* 0.285 95 -0.278 9.903 0.000 0.0002 0.0000 -0.0041 301695.0 87576.4 25.0 79.9 -28261.5********* 0.291 96 -0.283 10.100 0.000 0.0002 0.0000 -0.0042 307295.4 88683.2 23.6 82.0 -26875.9********* 0.296 97 -0.287 10.296 0.000 0.0002 0.0000 -0.0042 312895.2 89777.2 22.4 84.3 -25684.3********* 0.301 98 -0.292 10.496 0.000 0.0002 0.0000 -0.0043 318519.8 90888.6 22.0 86.5 -25333.8********* 0.307 99 -0.297 10.696 0.000 0.0002 0.0000 -0.0044 324122.4 91989.5 20.3 89.1 -23608.5********* 0.312 100 -0.302 10.901 0.000 0.0002 0.0000 -0.0044 329764.9 93101.3 19.5 91.1 -22831.9********* 0.318 101 -0.306 11.106 0.000 0.0002 0.0000 -0.0045 335391.3 94212.3 18.5 93.2 -21784.4********* 0.323 102 -0.311 11.312 0.000 0.0002 0.0000 -0.0046 341017.6 95323.4 17.3 95.9 -20604.7********* 0.328 103 -0.314 11.523 0.000 0.0002 0.0000 -0.0046 345663.4 96456.9 16.9 96.8 -20257.7********* 0.333 104 -0.320 11.727 0.000 0.0002 0.0000 -0.0047 352264.6 97547.8 15.7 100.0 -19002.7********* 0.339 105 -0.324 11.936 0.000 0.0002 0.0000 -0.0048 357933.5 98666.7 14.1 103.1 -17381.7********* 0.345 106 -0.328 12.147 0.000 0.0002 0.0000 -0.0048 363575.5 99782.3 13.5 105.4 -16817.3********* 0.350 107 -0.333 12.359 0.000 0.0002 0.0000 -0.0049 369224.0 100899.0 12.1 107.6 -15322.0********* 0.356 108 -0.335 12.578 0.000 0.0002 0.0000 -0.0050 373768.9 102043.7 12.0 108.9 -15254.8********* 0.360 109 -0.341 12.788 0.000 0.0002 0.0000 -0.0050 380507.7 103145.3 10.5 112.2 -13666.5********* 0.366 110 -0.345 13.004 0.000 0.0002 0.0000 -0.0051 386175.9 104266.1 8.8 115.3 -11963.0********* 0.372 111 -0.346 13.082 0.000 0.0002 0.0000 -0.0051 388129.0 104680.6 8.7 125.8 -11980.5********* 0.374 112 -0.348 13.157 0.000 0.0002 0.0000 -0.0052 390389.1 105076.8 9.4 137.3 -13009.0********* 0.376 113 -0.351 13.230 0.000 0.0002 0.0000 -0.0052 393472.9 105462.2 7.8 149.8 -11549.6********* 0.379 114 -0.353 13.304 0.000 0.0002 0.0000 -0.0052 396168.6 105853.6 7.9 161.8 -11899.5********* 0.382 115 -0.356 13.379 0.000 0.0002 0.0000 -0.0052 398856.2 106245.0 7.2 173.8 -11336.4********* 0.384 116 -0.358 13.454 0.000 0.0003 0.0000 -0.0053 401129.1 106641.1 7.8 185.9 -12220.3********* 0.386





3.302

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3.305

68 0.430 5.318 -0.514 0.0002 -0.0003 -0.0052-161720.0 29730.7 -3833.6 10.11443708.17216703.2 0.204 69 0.438 5.477 -0.531 0.0002 -0.0003 -0.0053-164431.4 30265.7 -3915.8 11.11485606.87404082.4 0.208 70 0.447 5.631 -0.543 0.0002 -0.0003 -0.0055-167148.5 30775.5 -3969.1 12.01518523.17580836.8 0.211 71 0.455 5.784 -0.556 0.0002 -0.0003 -0.0056-169855.8 31278.6 -4032.9 12.41555569.67755595.4 0.214 72 0.463 5.938 -0.564 0.0002 -0.0003 -0.0057-172541.6 31777.6 -4067.3 12.81584459.67928734.4 0.218 73 0.471 6.096 -0.578 0.0002 -0.0003 -0.0058-175248.2 32276.7 -4132.1 12.91623297.08105924.0 0.221 74 0.480 6.262 -0.596 0.0002 -0.0003 -0.0059-177969.2 32799.4 -4221.1 13.61668538.88294229.5 0.225 75 0.488 6.425 -0.607 0.0002 -0.0003 -0.0061-180693.2 33310.8 -4263.6 15.01699214.68478018.2 0.228 76 0.496 6.587 -0.622 0.0003 -0.0003 -0.0062-183412.1 33815.7 -4337.5 15.01741327.18659518.2 0.232 77 0.505 6.753 -0.635 0.0003 -0.0003 -0.0063-186129.8 34322.6 -4394.1 15.91777432.08842744.5 0.235 78 0.513 6.921 -0.649 0.0003 -0.0004 -0.0064-188850.4 34837.2 -4455.5 16.51816051.49031865.2 0.238 79 0.522 7.091 -0.662 0.0003 -0.0004 -0.0066-191580.7 35346.6 -4514.0 17.11853724.99219517.7 0.242 80 0.531 7.263 -0.675 0.0003 -0.0004 -0.0067-194310.6 35853.4 -4571.8 18.11891396.19407528.2 0.245 81 0.540 7.434 -0.690 0.0003 -0.0004 -0.0068-197044.9 36358.6 -4635.4 18.61931031.79594927.7 0.249 82 0.548 7.610 -0.704 0.0003 -0.0004 -0.0069-199772.1 36870.4 -4699.3 19.31971185.79786454.5 0.252 83 0.557 7.788 -0.717 0.0003 -0.0004 -0.0071-202507.9 37384.7 -4753.3 20.52008632.69981503.7 0.256 84 0.566 7.965 -0.731 0.0003 -0.0004 -0.0072-205247.2 37896.4 -4814.3 21.42048654.5********* 0.259 85 0.576 8.145 -0.748 0.0003 -0.0004 -0.0073-207991.8 38401.3 -4887.4 21.12092307.3********* 0.263 86 0.585 8.328 -0.762 0.0003 -0.0004 -0.0075-210733.6 38913.5 -4942.5 22.42130187.1********* 0.266 87 0.594 8.513 -0.776 0.0004 -0.0004 -0.0076-213472.9 39421.7 -4998.1 23.82169026.0********* 0.269 88 0.603 8.697 -0.790 0.0004 -0.0004 -0.0077-216229.5 39926.8 -5058.5 24.92209291.4********* 0.273 89 0.613 8.882 -0.805 0.0004 -0.0004 -0.0079-218976.7 40434.0 -5120.4 25.92250002.8********* 0.276 90 0.622 9.068 -0.820 0.0004 -0.0004 -0.0080-221727.5 40941.0 -5182.4 26.92290835.6********* 0.280 91 0.631 9.256 -0.837 0.0004 -0.0004 -0.0081-224481.7 41440.0 -5251.0 27.42334005.9********* 0.283 92 0.641 9.448 -0.851 0.0004 -0.0004 -0.0083-227229.7 41945.4 -5303.0 28.32371542.5********* 0.287 93 0.651 9.640 -0.866 0.0004 -0.0004 -0.0084-229993.7 42451.5 -5363.3 29.72412579.3********* 0.290 94 0.660 9.832 -0.882 0.0004 -0.0004 -0.0085-232745.6 42953.6 -5427.3 30.82454575.3********* 0.294 95 0.670 10.028 -0.899 0.0004 -0.0004 -0.0087-235505.6 43461.8 -5490.8 32.32496761.3********* 0.297 96 0.680 10.224 -0.914 0.0004 -0.0004 -0.0088-238273.2 43967.6 -5550.1 33.92537708.5********* 0.301 97 0.690 10.421 -0.929 0.0005 -0.0004 -0.0089-241035.1 44470.9 -5609.0 35.42578563.0********* 0.304 98 0.701 10.619 -0.947 0.0005 -0.0004 -0.0091-243772.9 44976.4 -5677.6 36.02623207.3********* 0.308 99 0.711 10.819 -0.963 0.0005 -0.0004 -0.0092-246573.1 45479.0 -5735.3 37.52663577.3********* 0.311 100 0.721 11.024 -0.979 0.0005 -0.0004 -0.0093-249333.6 45986.4 -5795.4 37.82705778.5********* 0.315 101 0.732 11.228 -0.996 0.0005 -0.0004 -0.0095-252092.2 46488.7 -5857.9 39.52748797.0********* 0.318 102 0.742 11.434 -1.011 0.0005 -0.0004 -0.0096-254888.0 46995.5 -5914.2 41.72789640.2********* 0.322 103 0.755 11.644 -1.031 0.0005 -0.0004 -0.0098-258326.4 47505.3 -5987.9 42.92836576.0********* 0.326 104 0.764 11.847 -1.047 0.0005 -0.0004 -0.0099-260435.7 47995.4 -6045.2 44.92877815.2********* 0.329 105 0.775 12.057 -1.062 0.0005 -0.0004 -0.0100-263220.5 48499.7 -6101.6 47.02919411.6********* 0.332 106 0.786 12.267 -1.079 0.0005 -0.0004 -0.0102-265999.8 49002.7 -6162.7 49.22962763.1********* 0.336 107 0.797 12.479 -1.097 0.0006 -0.0004 -0.0103-268770.8 49502.2 -6224.5 50.83006181.3********* 0.339 108 0.810 12.696 -1.116 0.0006 -0.0004 -0.0105-272281.2 50010.2 -6294.2 51.03052398.6********* 0.344 109 0.820 12.906 -1.132 0.0006 -0.0004 -0.0106-274367.5 50496.2 -6348.3 52.83092885.3********* 0.346 110 0.831 13.122 -1.149 0.0006 -0.0004 -0.0107-277128.9 50997.0 -6404.9 55.63135133.1********* 0.350 199 111 0.837 13.203 -1.150 0.0006 -0.0004 -0.0108-278884.2 51179.1 -6408.1 58.43146078.2********* 0.352 112 0.843 13.280 -1.152 0.0006 -0.0004 -0.0109-280492.8 51351.7 -6419.7 60.53160856.3********* 0.354 113 0.847 13.358 -1.151 0.0006 -0.0004 -0.0109-281531.4 51527.7 -6412.4 64.03167543.1********* 0.355 114 0.852 13.435 -1.153 0.0006 -0.0004 -0.0110-282834.1 51701.1 -6422.4 66.53181840.3********* 0.357 115 0.857 13.513 -1.153 0.0006 -0.0004 -0.0110-284138.8 51876.3 -6422.8 69.23191892.2********* 0.359 116 0.863 13.591 -1.156 0.0006 -0.0004 -0.0111-285720.0 52049.2 -6436.0 71.23207440.9********* 0.361 117 0.868 13.669 -1.155 0.0007 -0.0004 -0.0111-286752.0 52225.5 -6430.3 74.63214754.1********* 0.362 118 0.873 13.747 -1.158 0.0007 -0.0004 -0.0112-288335.0 52397.4 -6444.4 76.53230760.8********* 0.364 119 0.878 13.825 -1.157 0.0007 -0.0004 -0.0112-289368.3 52573.7 -6439.4 79.93238276.1********* 0.365 120 0.883 13.903 -1.160 0.0007 -0.0004 -0.0113-290674.1 52745.9 -6449.6 82.23252480.9********* 0.367 121 0.888 13.982 -1.159 0.0007 -0.0004 -0.0113-291984.5 52919.4 -6448.2 85.63261786.9********* 0.369 122 0.894 14.061 -1.162 0.0007 -0.0004 -0.0114-293581.2 53091.5 -6459.3 87.83276780.5********* 0.371 123 0.898 14.140 -1.160 0.0007 -0.0004 -0.0114-294608.6 53267.4 -6451.8 91.53283397.5********* 0.372 124 0.904 14.219 -1.163 0.0007 -0.0004 -0.0115-296206.6 53438.5 -6465.1 93.63299273.9********* 0.374 125 0.910 14.298 -1.164 0.0007 -0.0004 -0.0115-297522.6 53611.8 -6468.3 96.83310585.5********* 0.376 126 0.915 14.378 -1.164 0.0007 -0.0004 -0.0116-298834.7 53785.7 -6471.7 99.83322032.5********* 0.377 127 0.919 14.457 -1.163 0.0007 -0.0004 -0.0117-299856.1 53962.4 -6464.4 103.73328713.5********* 0.379 128 0.925 14.537 -1.166 0.0007 -0.0004 -0.0117-301459.0 54134.3 -6478.1 105.93344658.2********* 0.381 129 0.930 14.616 -1.164 0.0008 -0.0004 -0.0118-302479.6 54311.1 -6472.7 109.83352041.4********* 0.382 130 0.936 14.696 -1.167 0.0008 -0.0003 -0.0118-304079.8 54484.7 -6486.0 112.03367882.7********* 0.384 131 0.941 14.776 -1.168 0.0008 -0.0003 -0.0119-305399.0 54660.2 -6490.2 115.03379583.1********* 0.386 132 0.947 14.856 -1.169 0.0008 -0.0003 -0.0119-306735.3 54834.0 -6495.1 118.13391327.1********* 0.387 133 0.952 14.936 -1.170 0.0008 -0.0003 -0.0120-308077.5 55007.3 -6498.7 121.13402475.8********* 0.389 134 0.958 15.016 -1.171 0.0008 -0.0003 -0.0120-309415.2 55181.2 -6503.3 124.53414120.8********* 0.391 135 0.963 15.096 -1.172 0.0008 -0.0003 -0.0121-310758.4 55354.8 -6506.7 127.53425230.6********* 0.392 136 0.969 15.176 -1.172 0.0008 -0.0003 -0.0121-312096.7 55528.9 -6511.3 130.73436881.3********* 0.394 137 0.975 15.256 -1.173 0.0008 -0.0003 -0.0122-313440.7 55701.9 -6514.6 133.73447919.8********* 0.396 138 0.980 15.336 -1.174 0.0008 -0.0003 -0.0122-314779.1 55874.8 -6519.1 137.13459457.7********* 0.397 139 0.986 15.415 -1.175 0.0008 -0.0003 -0.0123-316126.6 56045.8 -6522.0 140.43469993.0********* 0.399 140 0.991 15.495 -1.175 0.0009 -0.0003 -0.0124-317451.7 56219.4 -6525.2 143.53481005.4********* 0.401 141 0.997 15.576 -1.176 0.0009 -0.0003 -0.0124-318775.8 56393.0 -6529.6 146.83492502.9********* 0.402 142 1.003 15.656 -1.177 0.0009 -0.0003 -0.0125-320099.2 56566.8 -6533.0 149.93503619.1********* 0.404 143 1.008 15.737 -1.178 0.0009 -0.0003 -0.0125-321419.4 56740.7 -6538.3 153.03515471.7********* 0.406 144 1.014 15.818 -1.179 0.0009 -0.0003 -0.0126-322749.4 56912.6 -6543.8 155.43527136.5********* 0.407 145 1.021 15.887 -1.182 0.0009 -0.0003 -0.0126-324637.5 57049.3 -6549.6 158.03534169.0********* 0.410 146 1.027 15.967 -1.183 0.0009 -0.0003 -0.0127-326047.7 57216.1 -6554.2 161.13544808.2********* 0.412 147 1.033 16.046 -1.185 0.0009 -0.0003 -0.0127-327458.4 57382.3 -6559.6 164.43555720.6********* 0.413 148 1.039 16.124 -1.186 0.0009 -0.0003 -0.0128-328897.8 57546.1 -6565.8 167.73566469.8********* 0.415 149 1.045 16.203 -1.189 0.0009 -0.0003 -0.0128-330320.2 57710.9 -6573.1 171.13577664.3********* 0.417 150 1.051 16.278 -1.191 0.0009 -0.0003 -0.0129-331817.1 57867.3 -6580.3 174.33587445.8********* 0.419 151 1.057 16.359 -1.193 0.0009 -0.0003 -0.0129-333152.2 58037.0 -6586.5 177.73599009.2********* 0.421 152 1.063 16.439 -1.194 0.0010 -0.0003 -0.0130-334513.1 58204.2 -6591.5 180.93609861.0********* 0.422 153 1.069 16.519 -1.196 0.0010 -0.0003 -0.0131-335881.2 58368.5 -6597.5 184.73621122.7********* 0.424 154 1.075 16.598 -1.197 0.0010 -0.0003 -0.0131-337298.1 58529.7 -6601.5 187.53631512.1********* 0.426 155 1.081 16.675 -1.199 0.0010 -0.0003 -0.0132-338839.7 58683.9 -6607.8 186.03641846.7********* 0.428 199 156 1.088 16.748 -1.200 0.0010 -0.0003 -0.0132-340465.6 58827.0 -6608.4 188.93648625.2********* 0.430 157 1.095 16.814 -1.203 0.0010 -0.0003 -0.0133-342147.2 58956.2 -6613.3 191.73654407.8********* 0.432 158 1.101 16.892 -1.204 0.0010 -0.0003 -0.0133-343601.9 59112.2 -6616.2 195.03663926.7********* 0.434 159 1.107 16.972 -1.204 0.0010 -0.0003 -0.0134-344952.4 59274.1 -6619.3 198.73674303.4********* 0.435 160 1.113 17.051 -1.206 0.0010 -0.0003 -0.0134-346282.9 59435.5 -6623.7 201.93684755.6********* 0.437 161 1.120 17.129 -1.207 0.0010 -0.0002 -0.0135-347655.8 59594.4 -6626.9 205.53694638.8********* 0.439 162 1.126 17.207 -1.207 0.0010 -0.0002 -0.0135-349053.2 59750.7 -6628.6 208.73703708.4********* 0.441 163 1.132 17.287 -1.208 0.0010 -0.0002 -0.0136-350400.3 59907.7 -6630.4 212.83713524.6********* 0.442 164 1.138 17.366 -1.208 0.0010 -0.0002 -0.0136-351787.0 60061.6 -6629.7 215.63721474.5********* 0.444





3.306

165 1.144 17.447 -1.210 0.0011 -0.0002 -0.0137-353118.9 60221.1 -6637.0 221.23733819.2********* 0.446 166 1.152 17.504 -1.211 0.0010 -0.0002 -0.0137-355023.0 60326.5 -6628.8 219.33730685.8********* 0.448 167 1.158 17.593 -1.213 0.0011 -0.0002 -0.0138-356363.2 60500.6 -6642.6 232.73748783.1********* 0.450 168 1.169 17.715 -1.207 0.0010 -0.0002 -0.0139-358559.0 60743.9 -6607.5 222.03742957.0********* 0.453 169 1.179 18.194 -1.190 0.0012 -0.0002 -0.0141-358084.4 61721.5 -6617.7 275.43842601.7********* 0.452 170 1.188 19.163 -1.043 0.0011 0.0000 -0.0147-353598.3 63662.4 -6262.4 213.33919694.9********* 0.446 ************************* PILEHEAD SUMMARY REPORT ************************* LOAD SEQUENCE 1 AXIAL PILE INCR **** DEFLECTIONS **** ***** ROTATIONS ***** ******** FORCES ******** ******* MOMENTS ******* CAPACITY JOINT NO. X Y Z X Y Z X Y Z X Y Z RATIO CM CM CM RAD RAD RAD KG KG KG CM-KG CM-KG CM-KG 841 1 0.004 0.007 0.000 0.0000 0.0000 0.0000 7074.4 -115.1 41.3 0.0 -23333.6 -94590.6 0.010 2 0.028 0.017 0.000 0.0000 0.0000 -0.0001 -3494.3 -222.8 71.0 -0.1 -40190.5-196796.5 0.005 3 0.033 0.025 0.000 0.0000 0.0000 -0.0001 -5306.9 -335.6 111.5 0.0 -63120.8-292013.6 0.008 4 0.037 0.033 0.000 0.0000 0.0000 -0.0002 -7079.0 -448.7 152.3 -0.1 -86239.0-387654.8 0.011 5 0.041 0.040 0.000 0.0000 0.0000 -0.0002 -8850.8 -561.7 192.8 -0.2-109238.1-483679.7 0.014 6 0.045 0.048 0.000 0.0000 0.0000 -0.0003 -10622.6 -674.5 233.1 -0.3-132079.7-580102.4 0.016 7 0.049 0.056 0.000 0.0000 0.0000 -0.0003 -12394.5 -787.2 273.1 -0.5-154750.3-676931.0 0.019 8 0.053 0.064 0.000 0.0000 -0.0001 -0.0004 -14166.3 -899.7 312.7 -0.7-177244.6-774170.7 0.022 9 0.057 0.073 0.000 0.0000 -0.0001 -0.0004 -15938.2 -1012.1 351.9 -1.0-199519.3-871870.0 0.024 10 0.061 0.081 0.000 0.0000 -0.0001 -0.0005 -17710.0 -1124.2 390.7 -1.2-221547.3-970059.9 0.027 11 0.061 0.039 0.000 -0.0002 -0.0002 -0.0004 -17721.6 -1402.4 909.3 -64.5-515577.7-953591.8 0.027 12 0.061 -0.006 -0.022 -0.0003 0.0003 0.0002 -17721.5 1251.5 -1779.5 -69.8 919975.1 733632.7 0.027 13 0.061 0.054 -0.032 -0.0003 0.0000 0.0003 -17721.4 2563.0 -785.3 -77.9 314356.21229926.9 0.027 14 0.061 0.105 -0.030 -0.0003 0.0000 0.0002 -17721.3 3142.2 -526.4 -85.6 174745.81351033.0 0.027 15 0.061 0.153 -0.028 -0.0003 0.0000 0.0002 -17721.3 3668.8 -408.7 -93.1 118009.61450330.0 0.027 16 0.061 0.201 -0.025 -0.0004 0.0000 0.0001 -17721.4 4183.6 -336.9 -100.2 87771.61545511.9 0.027 17 0.061 0.249 -0.023 -0.0004 0.0000 0.0001 -17721.5 4694.1 -285.3 -107.1 69206.51639442.8 0.027 18 0.061 0.296 -0.020 -0.0004 0.0000 0.0000 -17721.6 5202.8 -244.4 -113.7 56793.11732895.9 0.027 19 0.061 0.344 -0.017 -0.0004 0.0000 0.0000 -17721.9 5710.5 -209.9 -119.9 48013.61826141.0 0.027 20 0.061 0.391 -0.015 -0.0005 0.0000 -0.0001 -17722.1 6217.7 -179.4 -125.9 41556.81919278.8 0.027 21 0.061 0.439 -0.012 -0.0005 0.0000 -0.0001 -17722.5 6724.6 -151.7 -131.5 36675.32012366.1 0.027 22 0.061 0.486 -0.009 -0.0005 0.0000 -0.0002 -17722.7 7205.4 -123.9 -137.2 32612.32104332.8 0.027 23 0.061 0.536 -0.006 -0.0005 0.0000 -0.0002 -17722.6 7660.9 -94.6 -142.1 28709.82199203.9 0.027 24 0.061 0.588 -0.004 -0.0005 0.0000 -0.0003 -17722.5 8098.5 -70.3 -146.8 26264.72294654.7 0.027 25 0.061 0.643 -0.001 -0.0005 0.0000 -0.0004 -17722.1 8533.9 -49.1 -149.1 24450.92393328.3 0.027 26 0.062 0.699 0.000 -0.0006 0.0000 -0.0004 -17721.6 8972.8 -50.8 -155.2 29416.92495749.8 0.027 27 0.062 0.760 0.000 -0.0006 0.0000 -0.0005 -17720.6 9411.1 -63.7 -157.0 37060.32599816.9 0.027 28 0.062 0.822 0.000 -0.0006 0.0000 -0.0005 -17720.7 9852.5 -76.0 -160.8 44529.02703805.8 0.027 29 0.062 0.883 0.000 -0.0006 0.0000 -0.0006 -17720.8 10250.4 -87.8 -164.4 51664.62788302.9 0.027 30 0.062 0.950 0.000 -0.0006 0.0000 -0.0007 -17719.1 10695.3 -100.0 -166.7 59138.12894040.1 0.027 841 31 0.062 1.015 0.000 -0.0006 0.0000 -0.0008 -17719.8 11129.3 -106.3 -157.1 63168.43000568.2 0.027 32 0.062 1.079 0.000 -0.0007 0.0000 -0.0008 -17720.4 11546.1 -122.4 -184.1 73156.83103707.0 0.027 33 0.062 1.144 0.000 -0.0006 0.0000 -0.0009 -17720.9 11950.1 -134.0 -172.3 80414.53204828.8 0.027 34 0.063 1.215 0.000 -0.0006 0.0000 -0.0010 -17717.8 12392.1 -144.5 -173.2 87145.13315126.5 0.027 35 0.063 1.289 0.000 -0.0006 0.0000 -0.0010 -17716.7 12812.9 -154.7 -175.5 93881.23418490.6 0.027 36 0.063 1.366 0.000 -0.0006 0.0000 -0.0011 -17715.3 13255.7 -164.3 -174.0 100237.13532589.9 0.027 37 0.063 1.445 0.000 -0.0006 0.0000 -0.0012 -17713.3 13702.7 -174.2 -176.7 106881.03648856.9 0.027 38 0.063 1.525 0.000 -0.0006 0.0000 -0.0013 -17713.7 14117.1 -181.7 -169.7 112165.53757959.3 0.027 39 0.064 1.609 0.000 -0.0006 0.0000 -0.0013 -17711.3 14549.9 -190.3 -175.5 118225.03876348.8 0.027 40 0.064 1.695 0.000 -0.0006 0.0000 -0.0014 -17708.6 14983.3 -199.1 -175.3 124401.73995944.3 0.027 41 0.064 1.784 0.000 -0.0006 0.0000 -0.0015 -17706.7 15404.4 -207.3 -173.8 130329.14112682.6 0.027 42 0.064 1.875 0.000 -0.0006 0.0000 -0.0016 -17705.7 15828.1 -215.6 -173.8 136355.84233922.8 0.027 43 0.065 1.969 0.000 -0.0006 0.0000 -0.0016 -17701.5 16266.2 -223.4 -171.2 142174.94361248.2 0.027 44 0.065 2.066 0.000 -0.0006 0.0001 -0.0017 -17699.2 16689.0 -230.8 -169.6 147784.64483432.3 0.027 45 0.065 2.165 0.000 -0.0006 0.0001 -0.0018 -17695.6 17124.1 -238.2 -168.1 153414.54612277.0 0.027 46 0.066 2.268 0.000 -0.0006 0.0001 -0.0019 -17693.9 17553.8 -245.4 -166.9 159029.24740452.4 0.027 47 0.066 2.373 0.000 -0.0005 0.0001 -0.0020 -17688.4 18001.1 -252.3 -163.1 164421.64875497.3 0.027 48 0.067 2.481 0.000 -0.0005 0.0001 -0.0021 -17684.5 18440.9 -259.1 -162.2 169854.25008002.3 0.027 49 0.067 2.592 0.000 -0.0005 0.0001 -0.0022 -17680.0 18894.0 -265.8 -159.3 175254.55146373.8 0.027 50 0.068 2.705 0.000 -0.0005 0.0001 -0.0023 -17677.5 19345.4 -272.7 -156.6 180769.35284363.0 0.027 51 0.068 2.828 0.000 -0.0005 0.0001 -0.0024 -17659.9 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2933.0 34.6 -71.8 -19519.2 347350.5 0.027 23 0.061 0.356 0.000 -0.0003 0.0000 -0.0005 -17728.9 3190.3 33.6 -73.2 -18945.2 348363.8 0.027 24 0.061 0.392 0.000 -0.0003 0.0000 -0.0006 -17730.1 3454.8 32.9 -75.0 -18501.5 349440.9 0.027 25 0.061 0.429 0.000 -0.0003 0.0000 -0.0006 -17731.3 3728.8 32.6 -77.7 -18340.6 350568.8 0.027 26 0.061 0.469 0.000 -0.0003 0.0000 -0.0007 -17732.4 4014.3 31.8 -77.5 -17854.1 351846.3 0.027 27 0.061 0.510 0.000 -0.0003 0.0000 -0.0008 -17733.3 4300.5 31.4 -80.1 -17637.4 353895.0 0.027 28 0.061 0.554 0.000 -0.0003 0.0000 -0.0009 -17734.2 4592.8 31.0 -81.8 -17396.1 360497.2 0.027 29 0.062 0.597 0.000 -0.0003 0.0000 -0.0009 -17735.8 4876.9 30.6 -83.7 -17151.0 370159.8 0.027 30 0.062 0.644 0.000 -0.0003 0.0000 -0.0010 -17736.5 5147.5 30.1 -82.9 -16933.9 374752.9 0.027 31 0.062 0.690 0.000 -0.0003 0.0000 -0.0011 -17738.3 5433.2 29.2 -95.1 -16413.0 390305.6 0.027 32 0.062 0.738 0.000 -0.0003 0.0000 -0.0012 -17739.5 5703.6 30.8 -77.6 -17386.8 403648.1 0.027 33 0.062 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54 0.067 2.288 0.000 -0.0003 0.0000 -0.0034 -17755.4 12397.7 21.4 -89.6 -12572.2 901865.8 0.027 55 0.068 2.382 0.000 -0.0003 0.0000 -0.0035 -17746.4 12720.7 21.1 -88.1 -12458.7 938148.9 0.027 56 0.068 2.477 0.000 -0.0003 0.0000 -0.0036 -17747.7 13031.3 20.8 -86.8 -12323.2 972843.1 0.027 57 0.069 2.588 0.000 -0.0003 0.0000 -0.0037 -17729.2 13385.4 20.8 -87.6 -12314.91009766.1 0.027 58 0.069 2.689 0.000 -0.0001 0.0000 -0.0039 -17746.9 13713.3 20.1 -36.1 -12467.71057678.3 0.027 59 0.070 2.794 0.000 -0.0005 0.0000 -0.0040 -17738.8 14058.5 21.5 -131.2 -12444.71106135.4 0.027 60 0.070 2.917 0.000 -0.0003 0.0000 -0.0041 -17714.5 14426.8 20.3 -96.3 -12053.21144143.2 0.027 61 0.071 3.026 0.000 -0.0002 0.0000 -0.0043 -17736.2 14772.5 19.5 -68.2 -11933.21201192.3 0.027 62 0.072 3.134 0.000 -0.0003 0.0000 -0.0044 -17736.1 15109.5 19.8 -90.5 -11856.01252419.7 0.027 63 0.073 3.243 0.000 -0.0002 0.0000 -0.0045 -17739.5 15432.6 19.2 -71.6 -11775.71299107.5 0.027 64 0.073 3.376 0.000 -0.0003 0.0000 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0.000 -0.0001 0.0000 -0.0075 -17655.1 23053.1 16.9 -36.0 -11519.22661920.7 0.027 722 86 0.099 6.224 0.000 -0.0001 0.0000 -0.0077 -17650.2 23393.5 16.1 -43.8 -10790.22727722.1 0.027 87 0.100 6.373 0.000 -0.0001 0.0000 -0.0078 -17646.1 23728.6 16.2 -43.4 -10905.92793212.4 0.027 88 0.102 6.523 0.000 -0.0001 0.0000 -0.0080 -17643.3 24068.9 16.2 -38.2 -11045.62863205.9 0.027 89 0.104 6.674 0.000 -0.0001 0.0000 -0.0081 -17639.7 24403.9 16.3 -35.4 -11194.12931343.4 0.027 90 0.106 6.826 0.000 -0.0001 0.0000 -0.0083 -17635.1 24738.1 16.2 -33.1 -11222.43000567.3 0.027 91 0.107 6.980 0.000 -0.0001 0.0000 -0.0084 -17627.6 25072.4 16.7 -26.5 -11716.23070360.0 0.027 92 0.109 7.136 0.000 -0.0001 0.0000 -0.0086 -17624.2 25408.7 15.9 -33.2 -11062.53142047.6 0.027 93 0.111 7.294 0.000 -0.0001 0.0000 -0.0087 -17618.5 25742.7 16.3 -29.5 -11463.63213153.0 0.027 94 0.113 7.452 0.000 -0.0001 0.0000 -0.0089 -17615.3 26071.6 16.4 -22.0 -11697.33282522.5 0.027 95 0.115 7.614 0.000 -0.0001 0.0000 -0.0090 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0.027 106 0.141 9.474 0.000 0.0000 0.0000 -0.0107 -17539.5 30068.8 17.4 7.4 -13502.44190968.4 0.027 107 0.144 9.651 0.000 0.0000 0.0000 -0.0109 -17531.8 30404.3 18.1 -3.6 -13878.34270583.1 0.027 108 0.148 9.833 0.000 0.0001 0.0000 -0.0111 -18144.9 30750.4 17.1 39.6 -14044.54352861.0 0.028





3.309

109 0.150 10.009 0.000 0.0000 0.0000 -0.0112 -17541.0 31070.6 19.2 -0.6 -14855.84426905.0 0.027 110 0.153 10.189 0.000 0.0000 0.0000 -0.0114 -17518.5 31402.5 17.3 11.1 -13658.24506827.8 0.027 111 0.155 10.251 0.000 0.0001 0.0000 -0.0114 -17944.5 31529.8 17.3 30.7 -14092.94545450.8 0.028 112 0.156 10.311 0.000 0.0001 0.0000 -0.0115 -18170.9 31649.9 17.2 43.1 -14284.94581714.6 0.028 113 0.157 10.369 0.000 0.0001 0.0000 -0.0115 -17967.9 31763.5 17.1 21.8 -13768.44615608.2 0.028 114 0.157 10.428 0.000 0.0001 0.0000 -0.0116 -17964.8 31878.9 16.2 37.1 -13398.24650004.3 0.028 115 0.158 10.487 0.000 0.0001 0.0000 -0.0116 -17965.2 31996.3 17.1 21.7 -13776.34686071.3 0.028 116 0.160 10.547 0.000 0.0001 0.0000 -0.0117 -18183.1 32115.8 16.4 41.4 -13655.44722500.3 0.028 117 0.160 10.606 0.000 0.0000 0.0000 -0.0117 -17973.6 32229.4 16.6 18.1 -13363.94756660.1 0.028 118 0.162 10.666 0.000 0.0001 0.0000 -0.0118 -18189.0 32349.2 16.2 38.9 -13451.14793161.5 0.028 119 0.162 10.725 0.000 0.0000 0.0000 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-11677.55185814.7 0.028 130 0.174 11.389 0.000 0.0001 0.0000 -0.0123 -18225.4 33755.6 13.7 34.9 -11545.45223325.6 0.028 722 131 0.175 11.450 0.000 0.0001 0.0000 -0.0124 -18228.9 33871.9 14.2 24.4 -11731.75259667.5 0.028 132 0.177 11.511 0.000 0.0001 0.0000 -0.0124 -18234.0 33988.8 12.8 39.0 -10958.45297236.6 0.028 133 0.178 11.572 0.000 0.0000 0.0000 -0.0125 -18237.9 34105.8 13.6 18.1 -11173.25334931.2 0.028 134 0.179 11.633 0.000 0.0001 0.0000 -0.0125 -18241.9 34222.6 12.2 33.6 -10408.05372637.0 0.028 135 0.180 11.695 0.000 0.0000 0.0000 -0.0126 -18245.9 34339.6 12.9 15.4 -10612.45410337.2 0.028 136 0.181 11.756 0.000 0.0001 0.0000 -0.0126 -18250.2 34456.5 11.4 32.7 -9794.45448083.4 0.028 137 0.182 11.817 0.000 0.0000 0.0000 -0.0127 -18253.6 34573.2 12.2 14.4 -10053.15485842.8 0.028 138 0.183 11.878 0.000 0.0001 0.0000 -0.0127 -18258.2 34689.8 10.5 35.1 -9109.25523693.3 0.028 139 0.184 11.939 0.000 0.0001 0.0000 -0.0127 -18263.9 34806.8 10.0 27.9 -8583.65562653.4 0.028 140 0.185 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0.000 0.0000 0.0000 -0.0136 -18457.8 37468.8 -25.3 -5.0 20628.96586994.5 0.028 162 0.210 13.298 0.000 -0.0001 0.0000 -0.0136 -18467.8 37591.7 -25.4 -44.2 21605.86636966.9 0.028 163 0.211 13.358 0.000 0.0001 0.0000 -0.0137 -18480.2 37714.7 -32.6 39.7 25708.76686387.9 0.028 164 0.212 13.418 0.000 -0.0003 0.0000 -0.0137 -18487.0 37838.6 -24.9 -143.3 23315.66735795.6 0.028 165 0.213 13.477 0.000 0.0006 0.0000 -0.0138 -18506.6 37963.3 -49.6 240.4 35283.66787893.8 0.028 166 0.214 13.522 0.000 -0.0014 0.0000 -0.0138 -18518.1 38104.1 -9.9 -593.4 20817.46873421.6 0.028 167 0.215 13.571 0.000 0.0029 0.0000 -0.0138 -18571.1 38250.1 -120.8 1186.8 73171.76959248.6 0.029 168 0.217 13.684 0.000 -0.0061 0.0001 -0.0138 -18440.4 38490.9 85.5 -2551.2 -15274.37064050.6 0.028 169 0.223 14.024 -0.005 0.0141 -0.0001 -0.0141 -18199.7 39147.0 -407.4 5941.3 198051.27317422.3 0.028 170 0.245 15.083 0.000 0.0623 -0.0009 -0.0148 -18308.0 41015.1 -792.5 27370.4 71466.88017736.4 0.028 *** SACSCLP TIME LOG *** * OPERATION * * TIME INCREMENT * SETUP ................. 1.080 SEC. SOLUTION .............. 11.110 SEC. ELEMENT GENERATION..... 119.710 SEC. MATRIX ASSEMBLY........ 17.990 SEC. TRIANGULARIZATION...... 30.280 SEC. SUMMARY REPORT......... 2.130 SEC.





3.310

3.14.2.- Historial de carga y de deformaciones (CLPLOG) **** NON-LINEAR COLLAPSE ANALYSIS (LOAD SEQUENCE 1) **** LOAD LOAD *DEFLECTION* ROTATION ** DEFLECTION ** NSLV INC. LOOP CASE FACTOR DIFF. JNT DOF DIFFERENCE MAXIMUM JNT DOF 2 1 1 11 0.100 0.0543 527 DX 0.0000158 0.986 490 DX 4 2 1 11 0.200 0.0032 463 DX 0.0000156 2.035 490 DX 6 3 1 11 0.300 0.0041 463 DX 0.0000228 3.090 490 DX 8 4 1 11 0.400 0.0048 463 DX 0.0000342 4.150 490 DX 10 5 1 11 0.500 0.0056 484 DZ 0.0000489 5.217 490 DX 12 6 1 11 0.600 0.0067 484 DZ 0.0000651 6.290 490 DX 14 7 1 11 0.700 0.0078 484 DZ 0.0000823 7.368 490 DX 16 8 1 11 0.800 0.0092 892 DZ 0.0001000 8.453 490 DX 18 9 1 11 0.900 0.0108 892 DZ 0.0001176 9.542 490 DX 20 10 1 11 1.000 0.0123 892 DZ 0.0001346 10.637 490 DX 22 11 1 9 0.010 0.0190 463 DX 0.0001994 11.273 490 DX 24 12 1 9 0.020 0.0193 463 DX 0.0001886 11.919 463 DX 26 13 1 9 0.030 0.0193 463 DX 0.0001890 12.566 463 DX 28 14 1 9 0.040 0.0191 463 DX 0.0001892 13.240 525 DX 30 15 1 9 0.050 0.0192 463 DX 0.0001895 13.941 525 DX 32 16 1 9 0.060 0.0192 463 DX 0.0001896 14.642 525 DX 34 17 1 9 0.070 0.0192 463 DX 0.0001898 15.343 525 DX 36 18 1 9 0.080 0.0191 463 DX 0.0001899 16.044 525 DX 38 19 1 9 0.090 0.0192 463 DX 0.0001900 16.745 525 DX 40 20 1 9 0.100 0.0191 463 DX 0.0001901 17.447 525 DX 42 21 1 9 0.110 0.0191 463 DX 0.0001902 18.148 525 DX 44 22 1 9 0.120 0.0195 463 DX 0.0001903 18.851 525 DX 46 23 1 9 0.130 0.0197 463 DX 0.0001876 19.556 525 DX 48 24 1 9 0.140 0.0201 463 DX 0.0001879 20.262 525 DX 50 25 1 9 0.150 0.0193 463 DX 0.0001743 20.970 525 DX 52 26 1 9 0.160 0.0199 463 DX 0.0001862 21.680 525 DX 54 27 1 9 0.170 0.0193 463 DX 0.0001780 22.394 525 DX 56 28 1 9 0.180 0.0194 463 DX 0.0001820 23.109 525 DX 58 29 1 9 0.190 0.0231 463 DX 0.0001894 23.827 525 DX 60 30 1 9 0.200 0.0237 463 DX 0.0001948 24.547 525 DX 62 31 1 9 0.210 0.0272 525 DX 0.0002149 25.268 525 DX 64 32 1 9 0.220 0.0299 463 DX 0.0002448 25.990 525 DX 66 33 1 9 0.230 0.0356 463 DX 0.0001970 26.714 525 DX 68 34 1 9 0.240 0.0375 463 DX 0.0001932 27.442 525 DX 70 35 1 9 0.250 0.0399 463 DX 0.0002041 28.171 525 DX 72 36 1 9 0.260 0.0412 463 DX 0.0001899 28.904 525 DX 74 37 1 9 0.270 0.0429 463 DX 0.0002095 29.637 525 DX 76 38 1 9 0.280 0.0430 463 DX 0.0001621 30.373 525 DX 78 39 1 9 0.290 0.0448 463 DX 0.0001819 31.112 525 DX 80 40 1 9 0.300 0.0463 463 DX 0.0001847 31.853 525 DX 82 41 1 9 0.310 0.0479 463 DX 0.0001786 32.597 525 DX 84 42 1 9 0.320 0.0501 463 DX 0.0001853 33.343 525 DX 86 43 1 9 0.330 0.0512 463 DX 0.0001799 34.092 525 DX 88 44 1 9 0.340 0.0531 463 DX 0.0001780 34.843 525 DX 90 45 1 9 0.350 0.0550 463 DX 0.0001759 35.597 525 DX 92 46 1 9 0.360 0.0568 463 DX 0.0001829 36.354 525 DX 94 47 1 9 0.370 0.0579 463 DX 0.0001706 37.114 525 DX 96 48 1 9 0.380 0.0595 463 DX 0.0001762 37.876 525 DX 98 49 1 9 0.390 0.0614 319 DX 0.0001686 38.641 525 DX 100 50 1 9 0.400 0.0669 319 DX 0.0001854 39.411 525 DX 102 51 1 9 0.410 0.0558 525 DX 0.0001471 40.179 525 DX 104 52 1 9 0.420 0.0732 319 DX 0.0002222 40.954 525 DX 106 53 1 9 0.430 0.0546 525 DX 0.0001349 41.727 525 DX 108 54 1 9 0.440 0.0627 525 DX 0.0001952 42.500 525 DX 110 55 1 9 0.450 0.0599 525 DX 0.0001400 43.277 525 DX 112 56 1 9 0.460 0.0739 319 DX 0.0001956 44.062 525 DX 114 57 1 9 0.470 0.0565 525 DX 0.0001973 44.849 525 DX 116 58 1 9 0.480 0.0668 399 DX 0.0003804 45.629 525 DX 118 59 1 9 0.490 0.0668 319 DX 0.0002763 46.426 525 DX 120 60 1 9 0.500 0.0354 525 DX 0.0002404 47.215 525 DX 122 61 1 9 0.510 0.0346 525 DX 0.0001561 48.006 525 DX 124 62 1 9 0.520 0.0342 525 DX 0.0002088 48.798 525 DX 126 63 1 9 0.530 0.0389 525 DX 0.0001143 49.596 525 DX 128 64 1 9 0.540 0.0225 525 DX 0.0001927 50.392 525 DX 130 65 1 9 0.550 0.0326 525 DX 0.0001750 51.188 525 DX 132 66 1 9 0.560 0.0339 525 DX 0.0001674 51.987 525 DX 134 67 1 9 0.570 0.0362 525 DX 0.0001533 52.788 525 DX 136 68 1 9 0.580 0.0397 525 DX 0.0001453 53.597 525 DX 138 69 1 9 0.590 0.0229 525 DX 0.0002127 54.402 525 DX 140 70 1 9 0.600 0.0227 525 DX 0.0001398 55.209 525 DX 142 71 1 9 0.610 0.0238 525 DX 0.0001370 56.017 525 DX 144 72 1 9 0.620 0.0335 525 DX 0.0001662 56.826 525 DX 146 73 1 9 0.630 0.0393 525 DX 0.0001627 57.642 525 DX 148 74 1 9 0.640 0.0231 525 DX 0.0001884 58.455 525 DX 150 75 1 9 0.650 0.0237 525 DX 0.0001515 59.271 525 DX





3.311

152 76 1 9 0.660 0.0240 525 DX 0.0001189 60.088 525 DX 154 77 1 9 0.670 0.0238 525 DX 0.0001204 60.909 525 DX 156 78 1 9 0.680 0.0241 525 DX 0.0001392 61.731 525 DX 158 79 1 9 0.690 0.0245 525 DX 0.0001237 62.556 525 DX 160 80 1 9 0.700 0.0237 525 DX 0.0001406 63.381 525 DX 162 81 1 9 0.710 0.0248 525 DX 0.0001192 64.210 525 DX 164 82 1 9 0.720 0.0243 525 DX 0.0001158 65.040 525 DX 166 83 1 9 0.730 0.0241 525 DX 0.0001383 65.873 525 DX 168 84 1 9 0.740 0.0251 525 DX 0.0001337 66.707 525 DX 170 85 1 9 0.750 0.0243 525 DX 0.0001375 67.543 525 DX 172 86 1 9 0.760 0.0246 525 DX 0.0001234 68.382 525 DX 174 87 1 9 0.770 0.0247 525 DX 0.0001357 69.222 525 DX 176 88 1 9 0.780 0.0249 525 DX 0.0001230 70.064 525 DX 178 89 1 9 0.790 0.0247 525 DX 0.0001219 70.906 525 DX 180 90 1 9 0.800 0.0256 525 DX 0.0001190 71.750 525 DX 182 91 1 9 0.810 0.0248 525 DX 0.0001537 72.596 525 DX 184 92 1 9 0.820 0.0253 525 DX 0.0001227 73.444 525 DX 186 93 1 9 0.830 0.0252 525 DX 0.0001564 74.294 525 DX 188 94 1 9 0.840 0.0259 525 DX 0.0000967 75.145 525 DX 190 95 1 9 0.850 0.0253 525 DX 0.0002027 75.999 525 DX 192 96 1 9 0.860 0.0252 525 DX 0.0000998 76.854 525 DX 194 97 1 9 0.870 0.0266 525 DX 0.0002670 77.711 525 DX 196 98 1 9 0.880 0.0255 525 DX 0.0001667 78.569 525 DX 198 99 1 9 0.890 0.0272 525 DX 0.0003922 79.429 525 DX 200 100 1 9 0.900 0.0266 525 DX 0.0003646 80.293 525 DX 202 101 1 9 0.910 0.0263 525 DX 0.0006529 81.157 525 DX 204 102 1 9 0.920 0.0273 525 DX 0.0007232 82.024 525 DX 206 103 1 9 0.930 0.0261 525 DX 0.0011324 82.890 525 DX 207 103 2 9 0.930 0.0187 841 DY 0.0014262 82.892 525 DX 208 103 3 9 0.930 0.0033 841 DY 0.0002483 82.892 525 DX 210 104 1 9 0.940 0.0257 525 DX 0.0002415 83.759 525 DX 212 105 1 9 0.950 0.0271 525 DX 0.0004627 84.629 525 DX 214 106 1 9 0.960 0.0270 525 DX 0.0005051 85.500 525 DX 216 107 1 9 0.970 0.0277 525 DX 0.0008521 86.374 525 DX 218 108 1 9 0.980 0.0275 525 DX 0.0010364 87.248 525 DX 219 108 2 9 0.980 0.0203 841 DY 0.0015139 87.250 525 DX 220 108 3 9 0.980 0.0039 841 DY 0.0002872 87.250 525 DX 222 109 1 9 0.990 0.0258 525 DX 0.0004944 88.124 525 DX 224 110 1 9 1.000 0.0284 525 DX 0.0005803 89.002 525 DX 226 111 1 12 0.010 0.0223 527 DZ 0.0007014 89.630 525 DX 228 112 1 12 0.020 0.0234 484 DZ 0.0012018 90.258 525 DX 229 112 2 12 0.020 0.0233 841 DY 0.0017139 90.259 525 DX 230 112 3 12 0.020 0.0051 841 DY 0.0003554 90.259 525 DX 232 113 1 12 0.030 0.0215 527 DZ 0.0003402 90.886 525 DX 234 114 1 12 0.040 0.0231 484 DZ 0.0007334 91.515 525 DX 236 115 1 12 0.050 0.0230 527 DZ 0.0008948 92.144 525 DX 238 116 1 12 0.060 0.0243 484 DZ 0.0015112 92.772 525 DX 239 116 2 12 0.060 0.0310 841 DY 0.0022160 92.773 525 DX 240 116 3 12 0.060 0.0074 841 DY 0.0005080 92.773 525 DX 242 117 1 12 0.070 0.0223 527 DZ 0.0005780 93.401 525 DX 244 118 1 12 0.080 0.0244 484 DZ 0.0010805 94.031 525 DX 245 118 2 12 0.080 0.0224 841 DY 0.0015943 94.037 525 DX 246 118 3 12 0.080 0.0053 841 DY 0.0003643 94.037 525 DX 248 119 1 12 0.090 0.0246 525 DX 0.0003666 94.672 525 DX 250 120 1 12 0.100 0.0298 525 DX 0.0007651 95.311 525 DX 252 121 1 12 0.110 0.0309 525 DX 0.0009704 95.953 525 DX 254 122 1 12 0.120 0.0308 525 DX 0.0017119 96.594 525 DX 255 122 2 12 0.120 0.0396 841 DY 0.0026643 96.601 525 DX 256 122 3 12 0.120 0.0113 841 DY 0.0007407 96.601 525 DX 258 123 1 12 0.130 0.0256 527 DZ 0.0009887 97.237 525 DX 260 124 1 12 0.140 0.0316 525 DX 0.0018021 97.880 525 DX 261 124 2 12 0.140 0.0431 841 DY 0.0028481 97.886 525 DX 262 124 3 12 0.140 0.0128 841 DY 0.0008238 97.887 525 DX 264 125 1 12 0.150 0.0266 525 DX 0.0011357 98.525 525 DX 265 125 2 12 0.150 0.0291 841 DY 0.0018587 98.531 525 DX 266 125 3 12 0.150 0.0086 841 DY 0.0005738 98.531 525 DX 268 126 1 12 0.160 0.0269 484 DZ 0.0010899 99.169 525 DX 269 126 2 12 0.160 0.0252 841 DY 0.0016780 99.175 525 DX 270 126 3 12 0.160 0.0075 841 DY 0.0004739 99.176 525 DX 272 127 1 12 0.170 0.0292 525 DX 0.0005857 99.817 525 DX 274 128 1 12 0.180 0.0398 525 DX 0.0011766 100.469 525 DX 275 128 2 12 0.180 0.0286 841 DY 0.0018732 100.477 525 DX 276 128 3 12 0.180 0.0085 841 DY 0.0005430 100.477 525 DX 278 129 1 12 0.190 0.0348 525 DX 0.0006957 101.124 525 DX 280 130 1 12 0.200 0.0366 525 DX 0.0013741 101.773 525 DX 281 130 2 12 0.200 0.0367 841 DY 0.0022987 101.781 525 DX 282 130 3 12 0.200 0.0130 841 DY 0.0007869 101.782 525 DX 284 131 1 12 0.210 0.0378 525 DX 0.0011692 102.432 525 DX 285 131 2 12 0.210 0.0341 841 DY 0.0020376 102.451 525 DX 286 131 3 12 0.210 0.0126 463 DX 0.0007438 102.454 525 DX 288 132 1 12 0.220 0.0778 525 DX 0.0014312 103.145 525 DX 289 132 2 12 0.220 0.0465 463 DX 0.0023543 103.191 525 DX 290 132 3 12 0.220 0.0324 463 DX 0.0008175 103.200 525 DX





3.312

292 133 1 12 0.230 0.0690 525 DX 0.0012267 103.883 525 DX 293 133 2 12 0.230 0.0438 463 DX 0.0021508 103.926 525 DX 294 133 3 12 0.230 0.0309 463 DX 0.0007855 103.935 525 DX 296 134 1 12 0.240 0.0683 525 DX 0.0015116 104.617 525 DX 297 134 2 12 0.240 0.0445 463 DX 0.0025171 104.660 525 DX 298 134 3 12 0.240 0.0307 463 DX 0.0008663 104.669 525 DX 300 135 1 12 0.250 0.0691 525 DX 0.0013205 105.352 525 DX 301 135 2 12 0.250 0.0439 463 DX 0.0023087 105.395 525 DX 302 135 3 12 0.250 0.0310 463 DX 0.0008388 105.404 525 DX 304 136 1 12 0.260 0.0697 525 DX 0.0015976 106.088 525 DX 305 136 2 12 0.260 0.0450 463 DX 0.0026675 106.132 525 DX 306 136 3 12 0.260 0.0310 463 DX 0.0009214 106.141 525 DX 308 137 1 12 0.270 0.0723 525 DX 0.0014199 106.827 525 DX 309 137 2 12 0.270 0.0449 463 DX 0.0024786 106.872 525 DX 310 137 3 12 0.270 0.0318 463 DX 0.0008946 106.881 525 DX 312 138 1 12 0.280 0.0755 525 DX 0.0016744 107.571 525 DX 313 138 2 12 0.280 0.0482 463 DX 0.0027767 107.618 525 DX 314 138 3 12 0.280 0.0336 463 DX 0.0009634 107.628 525 DX 316 139 1 12 0.290 0.0867 525 DX 0.0015057 108.329 525 DX 317 139 2 12 0.290 0.0545 463 DX 0.0026375 108.383 525 DX 318 139 3 12 0.290 0.0400 463 DX 0.0009450 108.396 525 DX 319 139 1 12 0.290 0.0271 841 DY 0.0016083 108.414 525 DX 320 139 2 12 0.290 0.0463 841 DY 0.0027505 108.424 525 DX 321 139 3 12 0.290 0.0164 841 DY 0.0009757 108.426 525 DX 323 140 1 12 0.300 0.0839 463 DX 0.0015461 109.125 525 DX 324 140 2 12 0.300 0.0539 463 DX 0.0028689 109.178 525 DX 325 140 3 12 0.300 0.0396 463 DX 0.0012257 109.191 525 DX 326 140 4 12 0.300 0.0400 841 DY 0.0022534 109.209 525 DX 327 140 5 12 0.300 0.0170 841 DY 0.0009524 109.214 525 DX 329 141 1 12 0.310 0.0875 525 DX 0.0019399 109.917 525 DX 330 141 2 12 0.310 0.0631 841 DY 0.0035288 109.973 525 DX 331 141 3 12 0.310 0.0411 463 DX 0.0015018 109.986 525 DX 332 141 4 12 0.310 0.0509 841 DY 0.0028191 110.005 525 DX 333 141 5 12 0.310 0.0220 841 DY 0.0012198 110.010 525 DX 334 141 6 12 0.310 0.0410 841 DY 0.0022747 110.018 525 DX 335 141 7 12 0.310 0.0177 841 DY 0.0009826 110.020 525 DX 337 142 1 12 0.320 0.0851 463 DX 0.0016553 110.721 525 DX 338 142 2 12 0.320 0.0574 841 DY 0.0031517 110.775 525 DX 339 142 3 12 0.320 0.0404 463 DX 0.0013830 110.788 525 DX 340 142 4 12 0.320 0.0462 841 DY 0.0025592 110.807 525 DX 341 142 5 12 0.320 0.0200 841 DY 0.0011029 110.812 525 DX 342 142 6 12 0.320 0.0372 841 DY 0.0020548 110.819 525 DX 343 142 7 12 0.320 0.0160 841 DY 0.0008872 110.821 525 DX 345 143 1 12 0.330 0.0860 525 DX 0.0018330 111.523 525 DX 346 143 2 12 0.330 0.0600 841 DY 0.0033393 111.579 525 DX 347 143 3 12 0.330 0.0413 463 DX 0.0014163 111.592 525 DX 348 143 4 12 0.330 0.0482 841 DY 0.0026531 111.612 525 DX 349 143 5 12 0.330 0.0207 841 DY 0.0011447 111.617 525 DX 350 143 6 12 0.330 0.0387 841 DY 0.0021307 111.625 525 DX 351 143 7 12 0.330 0.0166 841 DY 0.0009173 111.627 525 DX 353 144 1 12 0.340 0.0867 463 DX 0.0015413 112.330 525 DX 354 144 2 12 0.340 0.0587 463 DX 0.0029296 112.389 525 DX 355 144 3 12 0.340 0.0440 463 DX 0.0012802 112.403 525 DX 356 144 4 12 0.340 0.0430 841 DY 0.0023610 112.427 525 DX 357 144 5 12 0.340 0.0191 463 DX 0.0010141 112.434 525 DX 358 144 6 12 0.340 0.0344 841 DY 0.0018900 112.445 525 DX 359 144 7 12 0.340 0.0148 841 DY 0.0008115 112.448 525 DX 361 145 1 12 0.350 0.0936 525 DX 0.0016885 113.159 525 DX 362 145 2 12 0.350 0.6280 463 DX 0.0031394 113.786 525 DX 363 145 3 12 0.350 0.5646 463 DX 0.0007248 113.891 525 DX 364 145 4 12 0.350 0.3652 463 DX 0.0013539 114.255 525 DX 365 145 5 12 0.350 0.3428 463 DX 0.0003224 114.330 525 DX 366 145 6 12 0.350 0.2626 463 DX 0.0005767 114.592 525 DX 367 145 7 12 0.350 0.2439 463 DX 0.0001598 114.643 525 DX 368 145 8 12 0.350 0.1792 463 DX 0.0002464 114.822 525 DX 369 145 9 12 0.350 0.1663 463 DX 0.0001072 114.857 525 DX 370 145 10 12 0.350 0.1206 463 DX 0.0001064 114.977 525 DX 371 145 11 12 0.350 0.0872 463 DX 0.0001958 115.063 525 DX 373 146 1 12 0.360 0.1474 463 DX 0.0001911 115.827 525 DX 374 146 2 12 0.360 0.1751 463 DX 0.0004153 116.001 525 DX 375 146 3 12 0.360 0.1391 463 DX 0.0001969 116.052 525 DX 376 146 4 12 0.360 0.0907 463 DX 0.0003458 116.142 525 DX 378 147 1 12 0.370 0.1563 463 DX 0.0004697 116.916 525 DX 379 147 2 12 0.370 0.1662 463 DX 0.0009209 117.081 525 DX 380 147 3 12 0.370 0.1352 463 DX 0.0004100 117.133 525 DX 381 147 4 12 0.370 0.0918 463 DX 0.0007411 117.225 525 DX 383 148 1 12 0.380 0.2095 463 DX 0.0012002 118.052 525 DX 384 148 2 12 0.380 0.1407 463 DX 0.0022752 118.192 525 DX 385 148 3 12 0.380 0.1240 463 DX 0.0009807 118.246 525 DX 386 148 4 12 0.380 0.0943 525 DX 0.0017929 118.340 525 DX 387 148 5 12 0.380 0.0826 525 DX 0.0007547 118.375 525 DX 389 149 1 12 0.390 0.2024 463 DX 0.0015454 119.196 525 DX 390 149 2 12 0.390 0.1739 463 DX 0.0027812 119.369 525 DX





3.313

391 149 3 12 0.390 0.1125 525 DX 0.0011653 119.395 525 DX 392 149 4 12 0.390 0.0937 463 DX 0.0021609 119.489 525 DX 393 149 5 12 0.390 0.0816 525 DX 0.0009058 119.524 525 DX 395 150 1 12 0.400 0.1874 463 DX 0.0015645 120.329 525 DX 396 150 2 12 0.400 0.1850 463 DX 0.0031425 120.514 525 DX 397 150 3 12 0.400 0.1193 525 DX 0.0015442 120.541 525 DX 398 150 4 12 0.400 0.0969 525 DX 0.0030420 120.638 525 DX 399 150 5 12 0.400 0.0855 463 DX 0.0014914 120.674 525 DX 400 150 6 12 0.400 0.0658 525 DX 0.0029477 120.740 525 DX 401 150 7 12 0.400 0.0589 463 DX 0.0014422 120.766 525 DX 402 150 8 12 0.400 0.0567 841 DY 0.0028515 120.812 525 DX 403 150 9 12 0.400 0.0415 463 DX 0.0013943 120.830 525 DX 404 150 10 12 0.400 0.0548 841 DY 0.0027567 120.863 525 DX 405 150 11 12 0.400 0.0295 463 DX 0.0013474 120.876 525 DX 406 150 12 12 0.400 0.0530 841 DY 0.0026639 120.899 525 DX 407 150 13 12 0.400 0.0259 841 DY 0.0013017 120.908 525 DX 408 150 14 12 0.400 0.0512 841 DY 0.0025732 120.925 525 DX 409 150 15 12 0.400 0.0250 841 DY 0.0012572 120.932 525 DX 410 150 16 12 0.400 0.0495 841 DY 0.0024852 120.944 525 DX 411 150 17 12 0.400 0.0242 841 DY 0.0012139 120.949 525 DX 412 150 18 12 0.400 0.0478 841 DY 0.0023996 120.957 525 DX 413 150 19 12 0.400 0.0233 841 DY 0.0011721 120.961 525 DX 415 151 1 12 0.410 0.1614 463 DX 0.0024740 121.741 525 DX 416 151 2 12 0.410 0.1167 463 DX 0.0047937 121.856 525 DX 417 151 3 12 0.410 0.0897 463 DX 0.0023206 121.888 525 DX 418 151 4 12 0.410 0.0919 841 DY 0.0045920 121.914 525 DX 419 151 5 12 0.410 0.0446 841 DY 0.0022340 121.926 525 DX 420 151 6 12 0.410 0.0883 841 DY 0.0044126 121.946 525 DX 421 151 7 12 0.410 0.0429 841 DY 0.0021469 121.953 525 DX 422 151 8 12 0.410 0.0848 841 DY 0.0042380 121.963 525 DX 423 151 9 12 0.410 0.0413 841 DY 0.0020623 121.966 525 DX 424 151 10 12 0.410 0.0815 841 DY 0.0040702 121.972 525 DX 425 151 11 12 0.410 0.0396 841 DY 0.0019806 121.973 525 DX 426 151 12 12 0.410 0.0782 841 DY 0.0039087 121.976 525 DX 427 151 13 12 0.410 0.0381 841 DY 0.0019021 121.977 525 DX 428 151 14 12 0.410 0.0751 841 DY 0.0037534 121.979 525 DX 429 151 15 12 0.410 0.0366 841 DY 0.0018265 121.979 525 DX 430 151 16 12 0.410 0.0721 841 DY 0.0036042 121.980 525 DX 431 151 17 12 0.410 0.0351 841 DY 0.0017539 121.980 525 DX 432 151 18 12 0.410 0.0693 841 DY 0.0034610 121.980 525 DX 433 151 19 12 0.410 0.0337 841 DY 0.0016842 121.981 525 DX 435 152 1 12 0.420 0.1689 463 DX 0.0031664 122.767 525 DX 436 152 2 12 0.420 0.1269 841 DY 0.0063106 122.884 525 DX 437 152 3 12 0.420 0.0922 463 DX 0.0030793 122.917 525 DX 438 152 4 12 0.420 0.1215 841 DY 0.0060525 122.970 525 DX 439 152 5 12 0.420 0.0592 841 DY 0.0029672 122.957 525 DX 440 152 6 12 0.420 0.1173 841 DY 0.0058492 122.980 525 DX 441 152 7 12 0.420 0.0568 841 DY 0.0028198 122.987 525 DX 442 152 8 12 0.420 0.1120 841 DY 0.0055696 123.000 525 DX 443 152 9 12 0.420 0.0543 841 DY 0.0026985 123.004 525 DX 444 152 10 12 0.420 0.1069 841 DY 0.0053166 123.011 525 DX 445 152 11 12 0.420 0.0518 841 DY 0.0025758 123.013 525 DX 446 152 12 12 0.420 0.1021 841 DY 0.0050740 123.017 525 DX 447 152 13 12 0.420 0.0495 841 DY 0.0024586 123.018 525 DX 448 152 14 12 0.420 0.0974 841 DY 0.0048423 123.021 525 DX 449 152 15 12 0.420 0.0472 841 DY 0.0023464 123.021 525 DX 450 152 16 12 0.420 0.0930 841 DY 0.0046211 123.023 525 DX 451 152 17 12 0.420 0.0451 841 DY 0.0022393 123.023 525 DX 452 152 18 12 0.420 0.0887 841 DY 0.0044100 123.024 525 DX 453 152 19 12 0.420 0.0430 841 DY 0.0021371 123.024 525 DX 455 153 1 12 0.430 0.1768 525 DX 0.0043623 123.820 525 DX 456 153 2 12 0.430 0.1725 841 DY 0.0085355 123.946 525 DX 457 153 3 12 0.430 0.0991 525 DX 0.0041621 123.982 525 DX 458 153 4 12 0.430 0.1672 841 DY 0.0082304 124.041 525 DX 459 153 5 12 0.430 0.0817 841 DY 0.0040294 124.059 525 DX 460 153 6 12 0.430 0.1617 841 DY 0.0079617 124.070 525 DX 461 153 7 12 0.430 0.0790 841 DY 0.0038912 124.081 525 DX 462 153 8 12 0.430 0.1562 841 DY 0.0076827 124.098 525 DX 463 153 9 12 0.430 0.0762 841 DY 0.0037533 124.105 525 DX 464 153 10 12 0.430 0.1507 841 DY 0.0074154 124.116 525 DX 465 153 11 12 0.430 0.0736 841 DY 0.0036199 124.120 525 DX 466 153 12 12 0.430 0.1454 841 DY 0.0071537 124.127 525 DX 467 153 13 12 0.430 0.0710 841 DY 0.0034917 124.130 525 DX 468 153 14 12 0.430 0.1403 841 DY 0.0069004 124.134 525 DX 469 153 15 12 0.430 0.0685 841 DY 0.0033679 124.135 525 DX 470 153 16 12 0.430 0.1353 841 DY 0.0066556 124.138 525 DX 471 153 17 12 0.430 0.0660 841 DY 0.0032484 124.139 525 DX 472 153 18 12 0.430 0.1305 841 DY 0.0064192 124.140 525 DX 473 153 19 12 0.430 0.0637 841 DY 0.0031329 124.141 525 DX 475 154 1 12 0.440 0.1977 463 DX 0.0060743 124.955 525 DX 476 154 2 12 0.440 0.2468 841 DY 0.0120684 125.105 525 DX 477 154 3 12 0.440 0.1235 463 DX 0.0059087 125.152 525 DX 478 154 4 12 0.440 0.2394 841 DY 0.0116930 125.234 525 DX





3.314

479 154 5 12 0.440 0.1172 841 DY 0.0057094 125.263 525 DX 480 154 6 12 0.440 0.2316 841 DY 0.0112995 125.313 525 DX 481 154 7 12 0.440 0.1133 841 DY 0.0055206 125.330 525 DX 482 154 8 12 0.440 0.2238 841 DY 0.0109141 125.361 525 DX 483 154 9 12 0.440 0.1092 841 DY 0.0052955 125.326 525 DX 484 154 10 12 0.440 0.2148 841 DY 0.0104518 125.334 525 DX 485 154 11 12 0.440 0.1050 841 DY 0.0051229 125.336 525 DX 486 154 12 12 0.440 0.2075 841 DY 0.0101137 125.342 525 DX 487 154 13 12 0.440 0.1013 841 DY 0.0049385 125.344 525 DX 488 154 14 12 0.440 0.2003 841 DY 0.0097632 125.348 525 DX 489 154 15 12 0.440 0.0979 841 DY 0.0047686 125.349 525 DX 490 154 16 12 0.440 0.1934 841 DY 0.0094263 125.352 525 DX 491 154 17 12 0.440 0.0945 841 DY 0.0046037 125.352 525 DX 492 154 18 12 0.440 0.1867 841 DY 0.0091004 125.354 525 DX 493 154 19 12 0.440 0.0912 841 DY 0.0044445 125.354 525 DX 495 155 1 12 0.450 0.2338 525 DX 0.0089140 126.209 525 DX 496 155 2 12 0.450 0.3598 841 DY 0.0174759 126.388 525 DX 497 155 3 12 0.450 0.1751 841 DY 0.0085062 126.449 525 DX 498 155 4 12 0.450 0.3461 841 DY 0.0167838 126.554 525 DX 499 155 5 12 0.450 0.2891 463 DX 0.0081820 126.788 525 DX 500 155 6 12 0.450 0.3322 841 DY 0.0161268 126.745 525 DX 501 155 7 12 0.450 0.1614 841 DY 0.0077933 126.753 525 DX 502 155 8 12 0.450 0.3183 841 DY 0.0153665 126.963 525 DX 503 155 9 12 0.450 0.1542 841 DY 0.0074452 126.826 525 DX 504 155 10 12 0.450 0.3034 841 DY 0.0146745 126.816 525 DX 505 155 11 12 0.450 0.2756 463 DX 0.0071423 127.093 525 DX 506 155 12 12 0.450 0.2894 841 DY 0.0140416 126.988 525 DX 507 155 13 12 0.450 0.1404 841 DY 0.0067668 126.970 525 DX 508 155 14 12 0.450 0.2759 841 DY 0.0133379 126.930 525 DX 509 155 15 12 0.450 0.1337 841 DY 0.0064680 126.908 525 DX 510 155 16 12 0.450 0.2631 841 DY 0.0127310 126.869 525 DX 511 155 17 12 0.450 0.1275 841 DY 0.0061698 126.854 525 DX 512 155 18 12 0.450 0.2623 463 DX 0.0121499 127.109 525 DX 513 155 19 12 0.450 0.1220 841 DY 0.0058813 126.911 525 DX 515 156 1 12 0.460 0.5204 463 DX 0.0114890 128.045 525 DX 516 156 2 12 0.460 0.4700 841 DY 0.0226445 128.100 525 DX 517 156 3 12 0.460 0.4841 463 DX 0.0109439 128.548 525 DX 518 156 4 12 0.460 0.4159 463 DX 0.0052999 128.722 525 DX 519 156 5 12 0.460 0.2150 841 DY 0.0103230 128.597 525 DX 520 156 6 12 0.460 0.4247 463 DX 0.0049027 129.080 525 DX 521 156 7 12 0.460 0.1520 484 DX 0.0023291 128.724 525 DX 522 156 8 12 0.460 0.4048 463 DX 0.0045105 129.125 525 DX 523 156 9 12 0.460 0.1485 490 DX 0.0021317 128.778 525 DX 524 156 10 12 0.460 0.3787 463 DX 0.0041373 129.152 525 DX 525 156 11 12 0.460 0.1617 463 DX 0.0019495 128.805 525 DX 526 156 12 12 0.460 0.3699 463 DX 0.0037830 129.171 525 DX 527 156 13 12 0.460 0.1670 463 DX 0.0017790 128.823 525 DX 528 156 14 12 0.460 0.3641 463 DX 0.0034489 129.183 525 DX 529 156 15 12 0.460 0.1688 463 DX 0.0015029 128.832 525 DX 530 156 16 12 0.460 0.3607 463 DX 0.0029076 129.189 525 DX 531 156 17 12 0.460 0.1677 463 DX 0.0010830 128.833 525 DX 532 156 18 12 0.460 0.3596 463 DX 0.0020849 129.188 525 DX 533 156 19 12 0.460 0.1684 463 DX 0.0007572 128.833 525 DX 535 157 1 12 0.470 0.6250 463 DX 0.0015893 130.072 525 DX 536 157 2 12 0.470 0.5373 463 DX 0.0032175 130.605 525 DX 537 157 3 12 0.470 0.4122 525 DX 0.0062295 131.017 525 DX 538 157 4 12 0.470 0.4377 463 DX 0.0028484 131.245 525 DX 539 157 5 12 0.470 0.2401 463 DX 0.0014457 131.268 525 DX 540 157 6 12 0.470 0.3289 463 DX 0.0027302 131.592 525 DX 541 157 7 12 0.470 0.2587 463 DX 0.0013025 131.686 525 DX 542 157 8 12 0.470 0.3789 525 DX 0.0023690 131.307 525 DX 543 157 9 12 0.470 0.2601 463 DX 0.0009487 131.756 525 DX 544 157 10 12 0.470 0.4139 525 DX 0.0017281 131.343 525 DX 545 157 11 12 0.470 0.2366 525 DX 0.0006696 131.786 525 DX 546 157 12 12 0.470 0.4199 525 DX 0.0011627 131.366 525 DX 547 157 13 12 0.470 0.2282 525 DX 0.0004047 131.804 525 DX 548 157 14 12 0.470 0.4237 525 DX 0.0006469 131.381 525 DX 549 157 15 12 0.470 0.2228 525 DX 0.0001633 131.815 525 DX 550 157 16 12 0.470 0.4256 525 DX 0.0002439 131.390 525 DX 551 157 17 12 0.470 0.2195 525 DX 0.0001253 131.822 525 DX 552 157 18 12 0.470 0.4267 525 DX 0.0002489 131.395 525 DX 553 157 19 12 0.470 0.2174 525 DX 0.0002570 131.826 525 DX 555 158 1 12 0.480 0.2116 463 DX 0.0006703 132.653 525 DX 556 158 2 12 0.480 0.2036 463 DX 0.0011903 132.854 525 DX 557 158 3 12 0.480 0.1213 463 DX 0.0022834 132.974 525 DX 558 158 4 12 0.480 0.1059 463 DX 0.0010966 133.018 525 DX 559 158 5 12 0.480 0.0752 463 DX 0.0021483 133.093 525 DX 560 158 6 12 0.480 0.0643 463 DX 0.0010330 133.118 525 DX 561 158 7 12 0.480 0.0444 525 DX 0.0020210 133.163 525 DX 562 158 8 12 0.480 0.0383 463 DX 0.0009703 133.178 525 DX 564 159 1 12 0.490 0.1867 463 DX 0.0020431 133.986 525 DX 565 159 2 12 0.490 0.1488 463 DX 0.0039167 134.131 525 DX 566 159 3 12 0.490 0.1227 463 DX 0.0018562 134.180 525 DX





3.315

567 159 4 12 0.490 0.0860 463 DX 0.0036452 134.264 525 DX 568 159 5 12 0.490 0.0723 463 DX 0.0017398 134.294 525 DX 569 159 6 12 0.490 0.0740 841 DY 0.0034034 134.344 525 DX 570 159 7 12 0.490 0.0431 463 DX 0.0016229 134.362 525 DX 571 159 8 12 0.490 0.0690 841 DY 0.0031732 134.392 525 DX 572 159 9 12 0.490 0.0329 841 DY 0.0015132 134.402 525 DX 573 159 10 12 0.490 0.0643 841 DY 0.0029574 134.420 525 DX 574 159 11 12 0.490 0.0306 841 DY 0.0014099 134.427 525 DX 575 159 12 12 0.490 0.0599 841 DY 0.0027554 134.438 525 DX 576 159 13 12 0.490 0.0285 841 DY 0.0013135 134.442 525 DX 577 159 14 12 0.490 0.0558 841 DY 0.0025665 134.449 525 DX 578 159 15 12 0.490 0.0266 841 DY 0.0012234 134.452 525 DX 579 159 16 12 0.490 0.0520 841 DY 0.0023904 134.456 525 DX 580 159 17 12 0.490 0.0248 841 DY 0.0011395 134.458 525 DX 581 159 18 12 0.490 0.0484 841 DY 0.0022261 134.460 525 DX 582 159 19 12 0.490 0.0231 841 DY 0.0010612 134.462 525 DX 584 160 1 12 0.500 0.2132 463 DX 0.0019444 135.294 525 DX 585 160 2 12 0.500 0.1218 463 DX 0.0038716 135.415 525 DX 586 160 3 12 0.500 0.1102 463 DX 0.0018516 135.463 525 DX 587 160 4 12 0.500 0.0838 525 DX 0.0035983 135.546 525 DX 588 160 5 12 0.500 0.0731 463 DX 0.0017088 135.576 525 DX 589 160 6 12 0.500 0.0725 841 DY 0.0033176 135.647 525 DX 590 160 7 12 0.500 0.0445 463 DX 0.0015618 135.654 525 DX 591 160 8 12 0.500 0.0663 841 DY 0.0030323 135.693 525 DX 592 160 9 12 0.500 0.0315 841 DY 0.0014368 135.704 525 DX 593 160 10 12 0.500 0.0614 841 DY 0.0028108 135.730 525 DX 594 160 11 12 0.500 0.0294 841 DY 0.0013420 135.730 525 DX 595 160 12 12 0.500 0.0573 841 DY 0.0026227 135.752 525 DX 596 160 13 12 0.500 0.0274 841 DY 0.0012524 135.745 525 DX 597 160 14 12 0.500 0.0534 841 DY 0.0024397 135.754 525 DX 598 160 15 12 0.500 0.0251 841 DY 0.0011464 135.767 525 DX 599 160 16 12 0.500 0.0487 841 DY 0.0022211 135.757 525 DX 600 160 17 12 0.500 0.0230 841 DY 0.0010529 135.757 525 DX 601 160 18 12 0.500 0.0449 841 DY 0.0020524 135.762 525 DX 602 160 19 12 0.500 0.0213 841 DY 0.0009708 135.763 525 DX 604 161 1 12 0.510 0.3271 463 DX 0.0020090 136.710 525 DX 605 161 2 12 0.510 0.1133 463 DX 0.0038025 136.820 525 DX 606 161 3 12 0.510 0.1063 463 DX 0.0017854 136.870 525 DX 607 161 4 12 0.510 0.1011 463 DX 0.0034835 136.969 525 DX 608 161 5 12 0.510 0.0861 463 DX 0.0016393 137.005 525 DX 609 161 6 12 0.510 0.0702 841 DY 0.0031882 137.068 525 DX 610 161 7 12 0.510 0.0572 463 DX 0.0014997 137.093 525 DX 611 161 8 12 0.510 0.0642 841 DY 0.0029147 137.137 525 DX 612 161 9 12 0.510 0.0387 463 DX 0.0013709 137.154 525 DX 613 161 10 12 0.510 0.0587 841 DY 0.0026628 137.183 525 DX 614 161 11 12 0.510 0.0276 841 DY 0.0012523 137.194 525 DX 615 161 12 12 0.510 0.0536 841 DY 0.0024315 137.214 525 DX 616 161 13 12 0.510 0.0252 841 DY 0.0011433 137.222 525 DX 617 161 14 12 0.510 0.0489 841 DY 0.0022195 137.235 525 DX 618 161 15 12 0.510 0.0230 841 DY 0.0010436 137.240 525 DX 619 161 16 12 0.510 0.0447 841 DY 0.0020255 137.249 525 DX 620 161 17 12 0.510 0.0210 841 DY 0.0009523 137.252 525 DX 622 162 1 12 0.520 0.3556 463 DX 0.0017915 138.226 525 DX 623 162 2 12 0.520 0.1104 463 DX 0.0038051 138.336 525 DX 624 162 3 12 0.520 0.1144 463 DX 0.0020852 138.393 525 DX 625 162 4 12 0.520 0.1105 463 DX 0.0011398 138.446 525 DX 626 162 5 12 0.520 0.0930 463 DX 0.0023962 138.537 525 DX 627 162 6 12 0.520 0.0810 463 DX 0.0011283 138.569 525 DX 628 162 7 12 0.520 0.0614 463 DX 0.0023709 138.629 525 DX 629 162 8 12 0.520 0.0538 463 DX 0.0011189 138.651 525 DX 630 162 9 12 0.520 0.0546 841 DY 0.0023446 138.692 525 DX 631 162 10 12 0.520 0.0361 463 DX 0.0011169 138.706 525 DX 632 162 11 12 0.520 0.0545 841 DY 0.0023389 138.733 525 DX 633 162 12 12 0.520 0.0260 841 DY 0.0011164 138.743 525 DX 634 162 13 12 0.520 0.0544 841 DY 0.0023367 138.761 525 DX 635 162 14 12 0.520 0.0260 841 DY 0.0011166 138.768 525 DX 636 162 15 12 0.520 0.0544 841 DY 0.0023370 138.779 525 DX 637 162 16 12 0.520 0.0260 841 DY 0.0011170 138.784 525 DX 638 162 17 12 0.520 0.0545 841 DY 0.0023377 138.792 525 DX 639 162 18 12 0.520 0.0260 841 DY 0.0011173 138.795 525 DX 640 162 19 12 0.520 0.0545 841 DY 0.0023382 138.800 525 DX 642 163 1 12 0.530 0.3726 463 DX 0.0050322 139.794 525 DX 643 163 2 12 0.530 0.2441 841 DY 0.0104133 139.893 525 DX 644 163 3 12 0.530 0.1212 841 DY 0.0051468 139.947 525 DX 645 163 4 12 0.530 0.2544 841 DY 0.0108027 140.050 525 DX 646 163 5 12 0.530 0.1206 841 DY 0.0051309 140.083 525 DX 647 163 6 12 0.530 0.2531 841 DY 0.0107482 140.146 525 DX 648 163 7 12 0.530 0.1207 841 DY 0.0051278 140.169 525 DX 649 163 8 12 0.530 0.2531 841 DY 0.0107407 140.211 525 DX 650 163 9 12 0.530 0.1207 841 DY 0.0051239 140.226 525 DX 651 163 10 12 0.530 0.2529 841 DY 0.0107290 140.253 525 DX 652 163 11 12 0.530 0.1207 841 DY 0.0051220 140.263 525 DX 653 163 12 12 0.530 0.2528 841 DY 0.0107236 140.281 525 DX





3.316

654 163 13 12 0.530 0.1207 841 DY 0.0051202 140.288 525 DX 655 163 14 12 0.530 0.2528 841 DY 0.0107188 140.299 525 DX 656 163 15 12 0.530 0.1207 841 DY 0.0051189 140.304 525 DX 657 163 16 12 0.530 0.2527 841 DY 0.0107152 140.311 525 DX 658 163 17 12 0.530 0.1207 841 DY 0.0051181 140.314 525 DX 659 163 18 12 0.530 0.2527 841 DY 0.0107129 140.319 525 DX 660 163 19 12 0.530 0.1207 841 DY 0.0051175 140.321 525 DX 662 164 1 12 0.540 0.3847 463 DX 0.0106016 141.323 525 DX 663 164 2 12 0.540 0.5256 841 DY 0.0222213 141.413 525 DX 664 164 3 12 0.540 0.2494 841 DY 0.0105131 141.466 525 DX 665 164 4 12 0.540 0.5200 841 DY 0.0219472 141.571 525 DX 666 164 5 12 0.540 0.2494 841 DY 0.0105131 141.601 525 DX 667 164 6 12 0.540 0.5201 841 DY 0.0219306 141.666 525 DX 668 164 7 12 0.540 0.2497 841 DY 0.0105173 141.686 525 DX 669 164 8 12 0.540 0.5206 841 DY 0.0219289 141.733 525 DX 670 164 9 12 0.540 0.2499 841 DY 0.0105251 141.746 525 DX 671 164 10 12 0.540 0.5212 841 DY 0.0219449 141.780 525 DX 672 164 11 12 0.540 0.2500 841 DY 0.0105255 141.789 525 DX 673 164 12 12 0.540 0.5214 841 DY 0.0219483 141.814 525 DX 674 164 13 12 0.540 0.2499 841 DY 0.0105201 141.819 525 DX 675 164 14 12 0.540 0.5212 841 DY 0.0219349 141.837 525 DX 676 164 15 12 0.540 0.2499 841 DY 0.0105152 141.840 525 DX 677 164 16 12 0.540 0.5209 841 DY 0.0219223 141.854 525 DX 678 164 17 12 0.540 0.2498 841 DY 0.0105116 141.854 525 DX 679 164 18 12 0.540 0.5208 841 DY 0.0219130 141.865 525 DX 680 164 19 12 0.540 0.2498 841 DY 0.0105090 141.865 525 DX 682 165 1 12 0.550 0.5228 841 DY 0.0220734 142.882 525 DX 683 165 2 12 0.550 1.0894 841 DY 0.0457005 142.967 525 DX 684 165 3 12 0.550 0.5309 841 DY 0.0222127 143.027 525 DX 685 165 4 12 0.550 1.1046 841 DY 0.0462517 143.137 525 DX 686 165 5 12 0.550 0.5288 841 DY 0.0221188 143.175 525 DX 687 165 6 12 0.550 1.0985 841 DY 0.0459472 143.246 525 DX 688 165 7 12 0.550 0.5291 841 DY 0.0221216 143.275 525 DX 689 165 8 12 0.550 1.0988 841 DY 0.0459276 143.327 525 DX 690 165 9 12 0.550 0.5296 841 DY 0.0221272 143.348 525 DX 691 165 10 12 0.550 1.0994 841 DY 0.0459214 143.387 525 DX 692 165 11 12 0.550 0.5301 841 DY 0.0221397 143.402 525 DX 693 165 12 12 0.550 1.1004 841 DY 0.0459473 143.432 525 DX 694 165 13 12 0.550 0.5303 841 DY 0.0221404 143.443 525 DX 695 165 14 12 0.550 1.1006 841 DY 0.0459464 143.464 525 DX 696 165 15 12 0.550 0.5303 841 DY 0.0221376 143.473 525 DX 697 165 16 12 0.550 1.1006 841 DY 0.0459359 143.489 525 DX 698 165 17 12 0.550 0.5304 841 DY 0.0221350 143.495 525 DX 699 165 18 12 0.550 1.1005 841 DY 0.0459270 143.507 525 DX 700 165 19 12 0.550 0.5304 841 DY 0.0221331 143.512 525 DX 702 166 1 12 0.560 1.1030 841 DY 0.0459530 144.865 525 DX 703 166 2 12 0.560 2.2808 841 DY 0.0947956 144.798 525 DX 704 166 3 12 0.560 1.1116 841 DY 0.0460120 145.344 525 DX 705 166 4 12 0.560 2.2939 841 DY 0.0950249 145.694 525 DX 706 166 5 12 0.560 1.1091 841 DY 0.0457727 145.837 525 DX 707 166 6 12 0.560 2.2840 841 DY 0.0942820 146.171 525 DX 708 166 7 12 0.560 1.1093 841 DY 0.0456782 146.273 525 DX 709 166 8 12 0.560 2.2808 841 DY 0.0938824 146.521 525 DX 710 166 9 12 0.560 1.1111 841 DY 0.0456410 146.591 525 DX 711 166 10 12 0.560 2.2819 841 DY 0.0937262 146.787 525 DX 712 166 11 12 0.560 1.1118 841 DY 0.0455962 146.831 525 DX 713 166 12 12 0.560 2.2813 841 DY 0.0935486 146.981 525 DX 714 166 13 12 0.560 1.1125 841 DY 0.0455705 147.008 525 DX 715 166 14 12 0.560 2.2832 841 DY 0.0934595 147.125 525 DX 716 166 15 12 0.560 1.1151 841 DY 0.0455948 147.139 525 DX 717 166 16 12 0.560 2.2873 841 DY 0.0935259 147.235 525 DX 718 166 17 12 0.560 1.1152 841 DY 0.0455718 147.243 525 DX 719 166 18 12 0.560 2.2866 841 DY 0.0934332 147.331 525 DX 720 166 19 12 0.560 1.1156 841 DY 0.0455625 147.335 525 DX 722 167 1 12 0.570 2.2924 841 DY 0.0937210 148.860 525 DX 723 167 2 12 0.570 4.6772 841 DY 0.1899945 149.343 525 DX 724 167 3 12 0.570 2.3266 841 DY 0.0940889 149.437 525 DX 725 167 4 12 0.570 4.7314 841 DY 0.1912466 149.677 525 DX 726 167 5 12 0.570 2.3240 841 DY 0.0937445 149.700 525 DX 727 167 6 12 0.570 4.7177 841 DY 0.1902415 149.913 525 DX 728 167 7 12 0.570 2.3230 841 DY 0.0935737 149.930 525 DX 729 167 8 12 0.570 4.7105 841 DY 0.1896546 150.118 525 DX 730 167 9 12 0.570 2.3243 841 DY 0.0935132 150.134 525 DX 731 167 10 12 0.570 4.7096 841 DY 0.1893930 150.303 525 DX 732 167 11 12 0.570 2.3258 841 DY 0.0934669 150.311 525 DX 733 167 12 12 0.570 4.7096 841 DY 0.1891859 150.460 525 DX 734 167 13 12 0.570 2.3271 841 DY 0.0934274 150.457 525 DX 735 167 14 12 0.570 4.7096 841 DY 0.1890175 150.582 525 DX 736 167 15 12 0.570 2.3280 841 DY 0.0933899 150.571 525 DX 737 167 16 12 0.570 4.7093 841 DY 0.1888735 150.678 525 DX 738 167 17 12 0.570 2.3286 841 DY 0.0933576 150.660 525 DX 739 167 18 12 0.570 4.7088 841 DY 0.1887493 150.753 525 DX 740 167 19 12 0.570 2.3291 841 DY 0.0933336 150.729 525 DX





3.317

742 168 1 12 0.580 4.7579 841 DY 0.1897142 152.323 525 DX 743 168 2 12 0.580 10.1484 841 DY 0.3902932 153.054 525 DX 744 168 3 12 0.580 5.2361 841 DY 0.1986539 153.096 525 DX 745 168 4 12 0.580 11.0416 841 DY 0.4193787 153.738 525 DX 746 168 5 12 0.580 5.2080 841 DY 0.1972337 153.512 525 DX 747 168 6 12 0.580 10.9609 841 DY 0.4150468 154.111 525 DX 748 168 7 12 0.580 5.2071 841 DY 0.1968076 153.855 525 DX 749 168 8 12 0.580 10.9426 841 DY 0.4133556 154.262 525 DX 750 168 9 12 0.580 5.2129 841 DY 0.1967043 153.952 525 DX 751 168 10 12 0.580 10.9495 841 DY 0.4132650 154.369 525 DX 752 168 11 12 0.580 5.2084 841 DY 0.1965007 154.038 525 DX 753 168 12 12 0.580 10.9365 841 DY 0.4125465 154.428 525 DX 754 168 13 12 0.580 5.2101 841 DY 0.1964682 154.094 525 DX 755 168 14 12 0.580 10.9374 841 DY 0.4124155 154.473 525 DX 756 168 15 12 0.580 5.2105 841 DY 0.1964280 154.133 525 DX 757 168 16 12 0.580 10.9365 841 DY 0.4122668 154.504 525 DX 758 168 17 12 0.580 5.2110 841 DY 0.1964019 154.162 525 DX 759 168 18 12 0.580 10.9361 841 DY 0.4121688 154.527 525 DX 760 168 19 12 0.580 5.2112 841 DY 0.1963831 154.183 525 DX 762 169 1 12 0.590 11.0145 841 DY 0.4139015 155.606 525 DX 763 169 2 12 0.590 23.2750 841 DY 0.8300309 157.761 525 DX 764 169 3 12 0.590 12.5570 841 DY 0.4408253 156.879 525 DX 765 169 4 12 0.590 25.5544 841 DY 0.8953376 158.965 525 DX 766 169 5 12 0.590 12.6497 841 DY 0.4391859 157.476 525 DX 767 169 6 12 0.590 25.6979 841 DY 0.8932171 159.289 525 DX 768 169 7 12 0.590 12.5879 841 DY 0.4368756 157.832 525 DX 769 169 8 12 0.590 25.5723 841 DY 0.8871741 159.579 525 DX 770 169 9 12 0.590 12.5918 841 DY 0.4361878 157.946 525 DX 771 169 10 12 0.590 25.5695 841 DY 0.8861517 159.722 525 DX 772 169 11 12 0.590 12.5722 841 DY 0.4355268 158.059 525 DX 773 169 12 12 0.590 25.5316 841 DY 0.8842822 159.795 525 DX 774 169 13 12 0.590 12.5772 841 DY 0.4354289 158.133 525 DX 775 169 14 12 0.590 25.5342 841 DY 0.8839218 159.856 525 DX 776 169 15 12 0.590 12.5784 841 DY 0.4353007 158.187 525 DX 777 169 16 12 0.590 25.5321 841 DY 0.8835258 159.900 525 DX 778 169 17 12 0.590 12.5793 841 DY 0.4352086 158.226 525 DX 779 169 18 12 0.590 25.5307 841 DY 0.8832400 159.933 525 DX 780 169 19 12 0.590 12.5801 841 DY 0.4351410 158.256 525 DX 782 170 1 12 0.600 26.0361 841 DY 0.8935081 161.144 525 DX 783 170 2 12 0.600 62.2350 841 DY 1.6542482 165.886 525 DX 784 170 3 12 0.600 44.7170 841 DY 1.1433419 164.429 525 DX 785 170 4 12 0.600 100.8184 841 DY 2.5230856 170.859 525 DX





3.318

3.14.3.-Reportes obtenidos directamente del Collvue 3.14.3.1.-Joint Displacement Report (Desplazamientos en nodos) Load Load Load ** Displacements (CM) ** **** Rotations (DEG) **** Step Cond Factor Joint X Y Z Theta X Theta Y Theta Z 169 12 0.59 319 27.942 1.591 -1.339 -0.10153 0.87188 0.13444 169 12 0.59 399 26.651 0.409 -1.298 0.01703 0.81305 -0.06642 169 12 0.59 119 18.907 0.517 -1.199 -0.10152 0.86894 0.13444 169 12 0.59 199 18.224 0.595 -1.179 0.01703 0.81011 -0.06642 169 12 0.59 102 17.858 -0.039 0.505 -0.00116 0.37770 -0.08529 169 12 0.59 201 18.965 -0.034 0.533 -0.00186 0.23949 -0.08530 169 12 0.59 101 17.872 -0.039 0.539 -0.00261 0.24995 -0.07913 169 12 0.59 3 20.045 0.018 0.760 -0.00509 -0.08216 0.10137 169 12 0.59 5 21.407 1.705 -1.167 -0.27577 -0.12823 0.37224 169 12 0.59 4 19.461 1.612 -1.135 0.07240 -0.24460 -0.13655 169 12 0.59 402 16.960 -0.016 0.538 0.00263 0.23948 -0.82905 169 12 0.59 861 19.640 0.059 0.969 -0.00081 0.15116 0.26414 169 12 0.59 614 20.790 0.060 1.044 0.00209 0.42822 0.30314 169 12 0.59 722 14.024 0.003 -0.223 -0.00635 0.80577 -0.80605 169 12 0.59 401 16.956 -0.016 -0.264 -0.00466 0.62250 -0.80620 169 12 0.59 532 22.647 0.060 1.077 0.00317 0.68974 0.32283 169 12 0.59 871 24.127 0.183 0.924 0.01231 0.15131 1.49322 169 12 0.59 842 17.767 -4.402 1.512 0.04904 0.23493 6.93198 169 12 0.59 6 25.339 0.064 1.070 0.00308 0.90353 0.33591 169 12 0.59 872 24.128 0.183 -0.316 -0.03135 0.47542 -0.80732 169 12 0.59 841 17.761 -4.402 -0.216 0.04706 0.50098 -7.73444 169 12 0.59 845 25.503 -1.217 4.682 0.00236 0.90657 0.30808 169 12 0.59 613 28.853 0.068 0.988 0.00832 1.33381 0.37005 169 12 0.59 723 40.991 0.473 -0.634 -0.01486 1.75680 -0.80919 169 12 0.59 695 25.510 -1.217 -0.229 -0.27775 1.66370 -7.72367 169 12 0.59 846 40.987 0.474 0.599 0.01497 1.52393 2.52750 169 12 0.59 727 95.630 -0.530 -2.920 0.01657 2.59559 -0.81043 169 12 0.59 725 72.256 -0.053 -1.867 0.01657 2.54533 -0.81043 169 12 0.59 538 31.173 0.067 0.922 0.01110 1.52568 0.38646 169 12 0.59 848 72.256 -0.053 -1.699 0.06506 3.86672 -0.18773 169 12 0.59 696 105.222 -2.024 -4.261 -0.38175 3.25039 -7.71976 169 12 0.59 669 84.089 -1.643 -3.044 -0.38175 3.23645 -7.71975 169 12 0.59 747 72.381 -0.065 -1.467 0.04536 3.86663 0.34357 169 12 0.59 850 84.091 -1.643 13.784 0.05681 4.02671 0.39579 169 12 0.59 881 110.145 -2.090 16.920 -0.02244 4.04103 0.29980 169 12 0.59 883 109.452 -1.251 7.196 0.11345 4.05479 0.39290 169 12 0.59 885 109.800 -1.718 12.064 0.07826 4.04806 0.32932 169 12 0.59 880 109.354 -2.093 16.933 -0.01277 3.90586 0.37348 169 12 0.59 882 108.706 -1.255 7.532 0.12194 3.91965 0.27092 169 12 0.59 886 109.755 -2.092 16.922 -0.01868 4.15253 0.33292 169 12 0.59 887 109.015 -1.254 7.365 0.11645 4.22173 0.31698 169 12 0.59 884 109.030 -1.629 12.239 0.06722 3.91281 0.33993 169 12 0.59 423 110.275 -1.716 11.917 0.08416 4.11067 0.34542 169 12 0.59 445 109.913 -1.280 6.936 0.09832 4.11258 0.36507 169 12 0.59 416 110.115 -2.487 21.852 0.05319 4.15296 0.32723 169 12 0.59 418 108.810 -1.040 4.595 0.06751 4.22140 0.31929 169 12 0.59 424 109.720 -1.038 4.280 0.12348 4.11318 0.37566 169 12 0.59 444 109.487 -1.039 4.371 0.10897 4.11885 0.36923 169 12 0.59 891 109.535 -0.746 1.095 0.39823 4.19920 0.35048 169 12 0.59 890 110.392 -0.735 -0.009 0.39534 4.10491 0.32165 169 12 0.59 422 110.984 -2.507 21.731 0.00163 4.10881 0.33627 169 12 0.59 446 110.699 -1.713 11.784 0.10238 4.17122 0.36945 169 12 0.59 895 109.377 -0.557 -1.045 0.03211 4.19721 0.35116 169 12 0.59 428 110.950 -1.029 3.655 0.18423 4.14250 0.35087 169 12 0.59 892 108.725 0.152 -9.866 0.30338 4.20138 0.34095 169 12 0.59 893 110.241 -0.562 -2.101 -0.40359 4.10034 0.36324 169 12 0.59 414 108.545 -1.632 12.371 0.05995 4.09133 0.32453 169 12 0.59 896 108.883 -0.029 -7.724 0.11711 4.19988 0.33725 169 12 0.59 889 109.619 0.161 -10.724 0.30045 4.10637 0.35198 169 12 0.59 421 111.693 -3.291 31.545 -0.04352 4.10910 0.34694 169 12 0.59 437 110.565 -0.558 -1.793 -0.40360 4.08507 0.37002 169 12 0.59 427 111.509 -1.707 11.433 0.15250 4.22767 0.36288 169 12 0.59 439 109.125 -0.558 -1.003 0.03108 4.18078 0.38125 169 12 0.59 813 112.729 -1.698 10.718 0.18149 4.26883 0.32076 169 12 0.59 413 109.249 -2.466 22.146 0.11312 4.09570 0.33264 169 12 0.59 412 109.955 -3.299 31.932 0.14137 4.09901 0.31972 169 12 0.59 814 112.152 -1.020 2.861 0.20042 4.17956 0.35249 169 12 0.59 894 109.771 -0.026 -8.630 -0.48402 4.10108 0.39033 169 12 0.59 457 108.617 -0.560 -0.929 0.02359 4.11768 0.41371





3.319

169 12 0.59 425 113.007 -3.282 31.744 -0.10342 4.23221 0.34724 169 12 0.59 453 108.188 -1.241 7.416 0.04371 4.09288 0.30875 169 12 0.59 812 113.501 -2.512 20.982 0.19091 4.31100 0.35536 169 12 0.59 451 108.179 -1.040 4.744 0.03019 4.10383 0.30453 169 12 0.59 459 82.983 -0.131 -2.233 0.05038 4.04278 0.34224 169 12 0.59 440 108.650 -0.030 -7.622 0.11627 4.14109 0.30497 169 12 0.59 823 110.339 -0.288 -5.032 0.21788 4.06955 0.32808 169 12 0.59 452 108.195 -1.634 12.462 0.04366 4.13925 0.30293 169 12 0.59 415 107.997 -1.041 4.771 0.01732 4.09382 0.29789 169 12 0.59 409 108.946 -3.306 32.630 0.19079 4.16941 0.33197 169 12 0.59 410 108.183 -3.311 33.116 0.18545 4.27349 0.34942 169 12 0.59 426 112.253 -2.533 21.619 0.05384 4.26864 0.31131 169 12 0.59 820 111.533 -0.279 -5.860 0.20210 4.03960 0.33244 169 12 0.59 411 107.416 -2.445 22.914 0.08762 4.27261 0.35287 169 12 0.59 436 110.115 -0.020 -8.258 -0.48399 4.05971 0.36813 169 12 0.59 407 107.484 -1.637 12.565 -0.00448 4.19262 0.30411 169 12 0.59 874 105.168 -0.282 -3.837 0.05318 4.16406 0.33685 169 12 0.59 408 108.212 -2.440 22.649 0.09704 4.22426 0.35119 169 12 0.59 14 108.224 -0.297 -4.145 0.05318 4.16580 0.33647 169 12 0.59 406 106.933 -1.045 4.832 -0.01563 4.13364 0.32984 169 12 0.59 697 106.450 -1.643 12.522 -0.04264 4.14055 0.32975 169 12 0.59 458 108.341 -0.032 -7.460 0.10958 4.12733 0.25022 169 12 0.59 873 105.297 1.499 -28.023 -0.05940 4.16168 0.30138 169 12 0.59 698 105.893 -1.049 4.838 -0.01195 4.12045 0.32285 169 12 0.59 875 101.724 1.661 -27.114 0.19254 4.18127 0.36493 169 12 0.59 815 110.949 0.405 -14.310 0.17472 3.95707 0.33342 169 12 0.59 15 106.319 -0.308 -3.878 -0.00769 4.08923 0.32081 169 12 0.59 700 105.271 -0.314 -3.853 -0.01242 4.06982 0.32064 169 12 0.59 448 108.356 0.387 -13.204 0.05945 4.27131 0.35677 169 12 0.59 432 109.740 0.396 -13.646 0.12288 4.09245 0.30904 169 12 0.59 450 106.970 0.380 -12.880 0.05887 4.24314 0.29224 169 12 0.59 816 110.363 1.097 -22.705 0.06661 3.97480 0.33433 169 12 0.59 865 102.528 1.075 -21.927 -0.00095 4.11442 0.28292 169 12 0.59 434 108.509 1.781 -31.205 -0.07051 4.15666 0.30430 169 12 0.59 447 108.409 1.086 -22.392 -0.04546 4.26887 0.34057 169 12 0.59 817 109.762 1.789 -31.188 -0.02046 4.03266 0.35411 169 12 0.59 703 104.661 0.368 -12.449 0.00102 4.04510 0.30880 169 12 0.59 16 105.712 0.373 -12.551 0.03567 4.11864 0.31999 169 12 0.59 867 101.090 2.337 -40.766 -0.13067 4.24843 0.32703 169 12 0.59 433 109.128 1.089 -22.411 0.02534 4.17794 0.33417 169 12 0.59 818 109.053 2.618 -40.937 -0.10830 4.13369 0.35224 169 12 0.59 855 107.465 1.079 -22.469 0.01215 4.23223 0.29464 169 12 0.59 435 107.783 2.609 -41.259 -0.15315 4.21976 0.35286 169 12 0.59 859 107.169 1.788 -31.455 -0.03726 4.32020 0.33211 169 12 0.59 856 106.798 1.790 -31.446 0.01209 4.23032 0.32080 169 12 0.59 857 106.892 1.074 -22.318 0.10682 4.22811 0.35479 169 12 0.59 449 105.725 1.063 -21.701 0.16904 4.28165 0.32465 169 12 0.59 821 108.514 3.211 -48.200 -0.12854 4.20315 0.34303 169 12 0.59 858 106.220 1.794 -31.301 0.09955 4.24116 0.33451 169 12 0.59 708 107.245 3.195 -48.627 -0.20716 4.26978 0.33628 169 12 0.59 734 106.384 2.601 -41.775 -0.07519 4.32782 0.33940 169 12 0.59 18 104.464 1.800 -30.207 0.20230 4.17849 0.36243 169 12 0.59 860 105.839 1.795 -31.128 0.14667 4.32287 0.34030 169 12 0.59 704 104.047 1.055 -21.045 0.06345 4.06492 0.31592 169 12 0.59 862 98.455 1.207 -20.876 0.13286 4.13966 0.37079 169 12 0.59 822 107.964 3.772 -55.562 -0.19191 4.24389 0.34599 169 12 0.59 715 105.810 3.184 -49.318 -0.10654 4.34009 0.33661 169 12 0.59 710 106.674 3.759 -56.152 -0.21663 4.34105 0.34912 169 12 0.59 705 103.428 1.785 -29.680 0.10954 4.07894 0.32074 169 12 0.59 732 105.054 2.595 -41.458 0.18028 4.34420 0.32407 169 12 0.59 897 107.410 4.366 -62.966 -0.25279 4.25507 0.36035 169 12 0.59 864 97.002 2.956 -39.808 0.24613 4.27090 0.33620 169 12 0.59 898 106.094 4.354 -63.734 -0.24101 4.35603 0.35712 169 12 0.59 19 103.730 2.584 -40.307 0.25858 4.23952 0.31022 169 12 0.59 716 105.233 3.753 -56.880 -0.13515 4.34047 0.34188 169 12 0.59 711 104.473 3.178 -49.044 0.19919 4.38401 0.32852 169 12 0.59 706 102.721 2.577 -39.458 0.21189 4.11576 0.30650 169 12 0.59 899 104.657 4.344 -64.428 -0.11021 4.33631 0.34493 169 12 0.59 17 105.091 1.060 -21.365 0.09870 4.19646 0.32941 169 12 0.59 707 103.188 3.165 -47.700 0.32507 4.26995 0.32663 169 12 0.59 712 103.879 3.775 -56.709 0.21031 4.41896 0.31335 169 12 0.59 717 102.197 3.151 -46.646 0.27194 4.13773 0.31445 169 12 0.59 900 103.279 4.337 -64.418 0.01990 4.43134 0.32920 169 12 0.59 709 102.623 3.775 -55.179 0.38582 4.30178 0.32577 169 12 0.59 903 103.534 3.781 -56.372 0.31293 4.59601 0.30952 169 12 0.59 901 102.889 4.335 -64.365 0.01834 4.59448 0.33011 169 12 0.59 718 101.672 3.760 -53.852 0.35525 4.14267 0.31264 169 12 0.59 460 158.341 -3.034 18.104 0.02943 4.25182 0.32024 169 12 0.59 463 154.186 -3.062 19.153 0.11443 4.26042 0.38288 169 12 0.59 512 158.008 -2.691 13.618 -0.02118 4.20560 0.32863 169 12 0.59 522 158.694 -3.032 18.042 0.03331 4.22253 0.34474 169 12 0.59 482 155.131 0.762 -25.929 0.02088 4.23164 0.32705 169 12 0.59 521 155.460 0.411 -21.469 -0.08635 4.18187 0.33949





3.320

169 12 0.59 525 159.067 -3.030 17.977 0.03462 4.15150 0.35471 169 12 0.59 513 157.577 -2.694 13.620 -0.02284 4.26478 0.32823 169 12 0.59 464 157.916 -3.037 18.154 0.01040 4.27025 0.31003 169 12 0.59 528 157.609 -1.776 3.264 -0.14922 4.17068 0.36087 169 12 0.59 529 158.003 -1.774 3.394 -0.14895 4.14564 0.36471 169 12 0.59 518 155.041 0.409 -21.552 -0.08515 4.08634 0.32686 169 12 0.59 515 153.851 -2.651 14.658 0.09573 4.21392 0.37587 169 12 0.59 530 156.526 -0.465 -11.809 -0.09932 4.10069 0.35172 169 12 0.59 523 155.489 0.764 -25.996 0.04084 4.16335 0.34116 169 12 0.59 531 156.900 -0.463 -11.730 -0.09952 4.14788 0.36348 169 12 0.59 526 155.850 0.766 -26.075 0.04629 4.18137 0.34392 169 12 0.59 488 153.971 2.057 -41.585 0.02622 4.20824 0.32921 169 12 0.59 524 154.324 2.059 -41.634 0.02059 4.22192 0.34124 169 12 0.59 527 154.697 2.061 -41.682 0.01892 4.20886 0.35236 169 12 0.59 467 154.708 -3.058 18.951 0.12050 4.20028 0.41916 169 12 0.59 481 154.718 0.759 -25.912 -0.01527 4.13596 0.30305 169 12 0.59 514 154.377 -2.647 14.490 0.09702 4.20077 0.37705 169 12 0.59 487 153.552 2.055 -41.513 0.03480 4.22176 0.30219 169 12 0.59 476 153.211 -1.886 5.921 0.12277 4.14319 0.35487 169 12 0.59 479 150.975 0.731 -24.864 0.10527 4.23567 0.37426 169 12 0.59 477 153.734 -1.882 5.718 0.12257 4.17201 0.37663 169 12 0.59 491 157.561 -3.039 18.187 0.00855 4.26264 0.28795 169 12 0.59 489 152.336 -0.865 -6.191 0.18775 4.10336 0.34423 169 12 0.59 517 151.305 0.327 -20.405 0.17875 4.17989 0.36387 169 12 0.59 483 150.166 0.719 -24.706 0.01966 4.22037 0.34851 169 12 0.59 478 152.854 -0.860 -6.485 0.19373 4.12220 0.37614 169 12 0.59 498 154.360 0.757 -25.916 -0.01859 4.12967 0.29262 169 12 0.59 490 151.573 -0.871 -5.713 0.18641 4.21064 0.34824 169 12 0.59 505 153.208 2.053 -41.441 0.04153 4.19895 0.28367 169 12 0.59 484 148.998 2.029 -40.412 0.06619 4.23085 0.35182 169 12 0.59 485 149.801 2.034 -40.621 0.06533 4.24437 0.36940 169 12 0.59 516 151.828 0.330 -20.680 0.17695 4.13240 0.37078 169 12 0.59 480 151.501 0.736 -25.081 0.13932 4.16724 0.42232 169 12 0.59 497 155.226 -3.054 18.768 0.11307 4.25526 0.44290 169 12 0.59 486 150.331 2.038 -40.747 0.06505 4.23064 0.43018 169 12 0.59 492 157.220 -3.040 18.224 0.01735 4.26935 0.28275 169 12 0.59 499 154.017 0.755 -25.910 -0.00221 4.11837 0.28501 169 12 0.59 506 152.877 2.052 -41.363 0.04757 4.17519 0.27886 169 12 0.59 504 152.028 0.740 -25.298 0.14259 4.13763 0.45029 169 12 0.59 511 150.869 2.042 -40.865 0.06458 4.21236 0.45121 169 12 0.59 496 155.731 -3.050 18.601 0.09740 4.29246 0.39883 169 12 0.59 493 156.882 -3.042 18.278 0.03377 4.27562 0.28557 169 12 0.59 500 153.678 0.753 -25.875 0.02705 4.10948 0.28783 169 12 0.59 507 152.547 2.051 -41.278 0.05289 4.16001 0.28408 169 12 0.59 503 152.545 0.745 -25.504 0.12677 4.10095 0.39698 169 12 0.59 510 151.391 2.045 -40.981 0.06315 4.20314 0.40427 169 12 0.59 495 156.163 -3.047 18.463 0.07698 4.27841 0.33670 169 12 0.59 494 156.536 -3.044 18.356 0.05471 4.27606 0.30015 169 12 0.59 501 153.332 0.751 -25.798 0.06260 4.10781 0.30202 169 12 0.59 508 152.203 2.049 -41.187 0.05738 4.15503 0.30126 169 12 0.59 502 152.963 0.748 -25.673 0.09793 4.10844 0.32921 169 12 0.59 509 151.829 2.048 -41.088 0.06085 4.16642 0.33846

3.14.3.2.-Pile Displacement Report (Desplazamientos en pilotes) Load Load Load Pilehead Pilehead ** Displacements (CM) ** **** Rotations (DEG) **** Step Cond Factor Joint Seg Subseg Distance X Y Z Theta X Theta Y Theta Z 169 12 0.59 102 1 1 0.000 17.858 -0.039 0.505 -0.00116 0.37770 -0.08529 169 12 0.59 102 1 2 0.508 17.494 -0.040 0.500 -0.00097 0.42268 -0.08529 169 12 0.59 102 1 3 1.017 17.091 -0.040 0.496 -0.00079 0.46374 -0.08529 169 12 0.59 102 1 4 1.525 16.654 -0.040 0.492 -0.00062 0.50094 -0.08529 169 12 0.59 102 1 5 2.033 16.185 -0.040 0.489 -0.00047 0.53435 -0.08529 169 12 0.59 102 1 6 2.542 15.689 -0.039 0.486 -0.00033 0.56404 -0.08529 169 12 0.59 102 2 1 3.050 15.168 -0.039 0.484 -0.00020 0.59010 -0.08529 169 12 0.59 102 2 2 3.598 14.578 -0.038 0.481 -0.00004 0.62000 -0.08529 169 12 0.59 102 2 3 4.145 13.962 -0.037 0.478 0.00011 0.64493 -0.08529 169 12 0.59 102 2 4 4.693 13.325 -0.036 0.475 0.00024 0.66507 -0.08529 169 12 0.59 102 2 5 5.241 12.672 -0.034 0.473 0.00035 0.68062 -0.08529 169 12 0.59 102 2 6 5.788 12.006 -0.033 0.471 0.00045 0.69182 -0.08529 169 12 0.59 102 2 7 6.336 11.332 -0.032 0.469 0.00054 0.69890 -0.08529 169 12 0.59 102 2 8 6.884 10.654 -0.030 0.468 0.00062 0.70208 -0.08529 169 12 0.59 102 2 9 7.431 9.974 -0.028 0.467 0.00068 0.70153 -0.08529 169 12 0.59 102 2 10 7.979 9.298 -0.027 0.465 0.00073 0.69741 -0.08529 169 12 0.59 102 2 11 8.527 8.627 -0.025 0.464 0.00077 0.68986 -0.08529 169 12 0.59 102 2 12 9.074 7.965 -0.023 0.462 0.00080 0.67901 -0.08529 169 12 0.59 102 2 13 9.622 7.316 -0.021 0.460 0.00083 0.66505 -0.08529 169 12 0.59 102 2 14 10.170 6.682 -0.020 0.458 0.00084 0.64816 -0.08529 169 12 0.59 102 2 15 10.717 6.065 -0.018 0.455 0.00084 0.62856 -0.08529 169 12 0.59 102 2 16 11.265 5.470 -0.016 0.452 0.00083 0.60644 -0.08529 169 12 0.59 102 2 17 11.813 4.896 -0.014 0.449 0.00082 0.58200 -0.08529 169 12 0.59 102 2 18 12.360 4.348 -0.013 0.445 0.00080 0.55543 -0.08529 169 12 0.59 102 2 19 12.908 3.826 -0.011 0.441 0.00077 0.52693 -0.08529





3.321

169 12 0.59 102 2 20 13.455 3.333 -0.010 0.436 0.00073 0.49665 -0.08529 169 12 0.59 102 2 21 14.003 2.870 -0.008 0.430 0.00070 0.46479 -0.08529 169 12 0.59 102 2 22 14.551 2.439 -0.007 0.425 0.00065 0.43149 -0.08529 169 12 0.59 102 2 23 15.098 2.040 -0.006 0.418 0.00060 0.39693 -0.08529 169 12 0.59 102 2 24 15.646 1.675 -0.005 0.412 0.00055 0.36134 -0.08529 169 12 0.59 102 2 25 16.194 1.346 -0.004 0.405 0.00049 0.32490 -0.08529 169 12 0.59 102 2 26 16.741 1.052 -0.003 0.397 0.00043 0.28780 -0.08529 169 12 0.59 102 2 27 17.289 0.793 -0.002 0.389 0.00037 0.25021 -0.08529 169 12 0.59 102 2 28 17.837 0.572 -0.002 0.382 0.00031 0.21226 -0.08529 169 12 0.59 102 2 29 18.384 0.389 -0.001 0.373 0.00024 0.17478 -0.08528 169 12 0.59 102 2 30 18.932 0.245 -0.001 0.365 0.00018 0.13914 -0.08528 169 12 0.59 102 2 31 19.480 0.136 0.000 0.357 0.00013 0.10648 -0.08528 169 12 0.59 102 2 32 20.027 0.058 0.000 0.349 0.00009 0.07774 -0.08528 169 12 0.59 102 2 33 20.575 0.006 0.000 0.341 0.00005 0.05352 -0.08528 169 12 0.59 102 2 34 21.123 -0.025 0.000 0.333 0.00002 0.03405 -0.08528 169 12 0.59 102 2 35 21.670 -0.040 0.000 0.325 0.00001 0.01918 -0.08528 169 12 0.59 102 2 36 22.218 -0.044 0.000 0.317 0.00000 0.00846 -0.08528 169 12 0.59 102 2 37 22.766 -0.042 0.000 0.310 -0.00001 0.00127 -0.08528 169 12 0.59 102 2 38 23.313 -0.035 0.000 0.302 -0.00001 -0.00306 -0.08528 169 12 0.59 102 2 39 23.861 -0.027 0.000 0.295 -0.00001 -0.00510 -0.08528 169 12 0.59 102 2 40 24.409 -0.019 0.000 0.289 -0.00001 -0.00555 -0.08528 169 12 0.59 102 2 41 24.956 -0.012 0.000 0.282 0.00000 -0.00510 -0.08528 169 12 0.59 102 2 42 25.504 -0.007 0.000 0.276 0.00000 -0.00423 -0.08528 169 12 0.59 102 2 43 26.052 -0.004 0.000 0.270 0.00000 -0.00327 -0.08528 169 12 0.59 102 2 44 26.599 -0.001 0.000 0.265 0.00000 -0.00240 -0.08528 169 12 0.59 102 2 45 27.147 0.000 0.000 0.259 0.00000 -0.00169 -0.08528 169 12 0.59 102 2 46 27.695 0.001 0.000 0.254 0.00000 -0.00116 -0.08528 169 12 0.59 102 2 47 28.242 0.002 0.000 0.250 0.00000 -0.00078 -0.08528 169 12 0.59 102 2 48 28.790 0.002 0.000 0.245 0.00000 -0.00053 -0.08528 169 12 0.59 102 2 49 29.337 0.002 0.000 0.241 0.00000 -0.00037 -0.08528 169 12 0.59 102 2 50 29.885 0.003 0.000 0.237 0.00000 -0.00026 -0.08528 169 12 0.59 102 2 51 30.433 0.003 0.000 0.233 0.00000 -0.00016 -0.08528 169 12 0.59 102 2 52 30.980 0.003 0.000 0.229 0.00000 -0.00008 -0.08528 169 12 0.59 102 2 53 31.528 0.003 0.000 0.226 0.00000 -0.00001 -0.08528 169 12 0.59 102 2 54 32.076 0.003 0.000 0.222 0.00000 0.00004 -0.08528 169 12 0.59 102 2 55 32.623 0.003 0.000 0.218 0.00000 0.00009 -0.08528 169 12 0.59 102 2 56 33.171 0.003 0.000 0.215 0.00000 0.00012 -0.08528 169 12 0.59 102 2 57 33.719 0.003 0.000 0.211 0.00000 0.00015 -0.08528 169 12 0.59 102 2 58 34.266 0.002 0.000 0.208 0.00000 0.00016 -0.08528 169 12 0.59 102 2 59 34.814 0.002 0.000 0.205 0.00000 0.00018 -0.08528 169 12 0.59 102 2 60 35.362 0.002 0.000 0.202 0.00000 0.00018 -0.08528 169 12 0.59 102 2 61 35.909 0.002 0.000 0.198 0.00000 0.00018 -0.08528 169 12 0.59 102 2 62 36.457 0.002 0.000 0.195 0.00000 0.00018 -0.08528 169 12 0.59 102 2 63 37.005 0.001 0.000 0.192 0.00000 0.00018 -0.08528 169 12 0.59 102 2 64 37.552 0.001 0.000 0.189 0.00000 0.00017 -0.08528 169 12 0.59 102 3 1 38.100 0.001 0.000 0.187 0.00000 0.00016 -0.08528 169 12 0.59 102 3 2 38.607 0.001 0.000 0.184 0.00000 0.00015 -0.08528 169 12 0.59 102 3 3 39.113 0.001 0.000 0.182 0.00000 0.00015 -0.08528 169 12 0.59 102 4 1 39.620 0.001 0.000 0.180 0.00000 0.00014 -0.08528 169 12 0.59 102 4 2 40.169 0.001 0.000 0.178 0.00000 0.00013 -0.08528 169 12 0.59 102 4 3 40.718 0.001 0.000 0.175 0.00000 0.00011 -0.08528 169 12 0.59 102 4 4 41.266 0.000 0.000 0.172 0.00000 0.00010 -0.08528 169 12 0.59 102 4 5 41.815 0.000 0.000 0.170 0.00000 0.00009 -0.08528 169 12 0.59 102 4 6 42.364 0.000 0.000 0.167 0.00000 0.00008 -0.08528 169 12 0.59 102 4 7 42.913 0.000 0.000 0.165 0.00000 0.00007 -0.08528 169 12 0.59 102 4 8 43.462 0.000 0.000 0.163 0.00000 0.00006 -0.08528 169 12 0.59 102 4 9 44.010 0.000 0.000 0.160 0.00000 0.00005 -0.08528 169 12 0.59 102 4 10 44.559 0.000 0.000 0.158 0.00000 0.00004 -0.08528 169 12 0.59 102 4 11 45.108 0.000 0.000 0.156 0.00000 0.00003 -0.08528 169 12 0.59 102 4 12 45.657 0.000 0.000 0.154 0.00000 0.00002 -0.08528 169 12 0.59 102 4 13 46.206 0.000 0.000 0.152 0.00000 0.00002 -0.08527 169 12 0.59 102 4 14 46.754 0.000 0.000 0.151 0.00000 0.00001 -0.08527 169 12 0.59 102 4 15 47.303 0.000 0.000 0.149 0.00000 0.00001 -0.08527 169 12 0.59 102 4 16 47.852 0.000 0.000 0.147 0.00000 0.00000 -0.08527 169 12 0.59 102 4 17 48.401 0.000 0.000 0.146 0.00000 0.00000 -0.08527 169 12 0.59 102 4 18 48.950 0.000 0.000 0.144 0.00000 0.00000 -0.08527 169 12 0.59 102 4 19 49.498 0.000 0.000 0.143 0.00000 0.00000 -0.08527 169 12 0.59 102 4 20 50.047 0.000 0.000 0.142 0.00000 -0.00001 -0.08527 169 12 0.59 102 4 21 50.596 0.000 0.000 0.140 0.00000 -0.00001 -0.08527 169 12 0.59 102 4 22 51.145 0.000 0.000 0.139 0.00000 -0.00001 -0.08527 169 12 0.59 102 4 23 51.694 0.000 0.000 0.138 0.00000 -0.00001 -0.08527 169 12 0.59 102 4 24 52.242 0.000 0.000 0.137 0.00000 -0.00001 -0.08527 169 12 0.59 102 4 25 52.791 0.000 0.000 0.136 0.00000 -0.00001 -0.08527 169 12 0.59 102 5 1 53.340 0.000 0.000 0.136 0.00000 -0.00001 -0.08527 169 12 0.59 102 5 2 54.100 0.000 0.000 0.135 0.00000 -0.00001 -0.08527 169 12 0.59 102 5 3 54.860 0.000 0.000 0.134 0.00000 -0.00001 -0.08527 169 12 0.59 119 1 1 0.000 18.907 0.517 -1.199 -0.10152 0.86894 0.13444 169 12 0.59 119 1 2 0.508 18.110 0.429 -1.175 -0.09368 0.90325 0.13426 169 12 0.59 119 1 3 1.017 17.285 0.348 -1.149 -0.08613 0.93140 0.13409 169 12 0.59 119 1 4 1.525 16.438 0.273 -1.122 -0.07890 0.95352 0.13393 169 12 0.59 119 1 5 2.033 15.574 0.205 -1.096 -0.07197 0.96979 0.13379 169 12 0.59 119 1 6 2.542 14.699 0.143 -1.068 -0.06537 0.98038 0.13366 169 12 0.59 119 2 1 3.050 13.817 0.086 -1.041 -0.05909 0.98553 0.13355





3.322

169 12 0.59 119 2 2 3.592 12.872 0.033 -1.007 -0.05081 0.98519 0.13340 169 12 0.59 119 2 3 4.135 11.930 -0.013 -0.974 -0.04304 0.97750 0.13327 169 12 0.59 119 2 4 4.677 11.001 -0.051 -0.941 -0.03578 0.96293 0.13315 169 12 0.59 119 2 5 5.219 10.089 -0.083 -0.908 -0.02904 0.94213 0.13305 169 12 0.59 119 2 6 5.762 9.201 -0.109 -0.877 -0.02283 0.91581 0.13296 169 12 0.59 119 2 7 6.304 8.341 -0.129 -0.847 -0.01713 0.88467 0.13288 169 12 0.59 119 2 8 6.847 7.514 -0.144 -0.817 -0.01195 0.84936 0.13280 169 12 0.59 119 2 9 7.389 6.722 -0.154 -0.789 -0.00729 0.81046 0.13274 169 12 0.59 119 2 10 7.931 5.970 -0.159 -0.762 -0.00314 0.76846 0.13269 169 12 0.59 119 2 11 8.474 5.260 -0.161 -0.736 0.00052 0.72375 0.13264 169 12 0.59 119 2 12 9.016 4.593 -0.160 -0.712 0.00367 0.67676 0.13259 169 12 0.59 119 2 13 9.558 3.973 -0.156 -0.688 0.00634 0.62800 0.13256 169 12 0.59 119 2 14 10.101 3.401 -0.149 -0.666 0.00855 0.57801 0.13253 169 12 0.59 119 2 15 10.643 2.877 -0.141 -0.645 0.01031 0.52737 0.13250 169 12 0.59 119 2 16 11.186 2.403 -0.131 -0.625 0.01164 0.47664 0.13247 169 12 0.59 119 2 17 11.728 1.977 -0.120 -0.605 0.01257 0.42638 0.13246 169 12 0.59 119 2 18 12.270 1.599 -0.108 -0.587 0.01313 0.37710 0.13244 169 12 0.59 119 2 19 12.813 1.267 -0.095 -0.569 0.01334 0.32930 0.13242 169 12 0.59 119 2 20 13.355 0.981 -0.083 -0.552 0.01323 0.28342 0.13241 169 12 0.59 119 2 21 13.897 0.738 -0.071 -0.535 0.01284 0.23988 0.13240 169 12 0.59 119 2 22 14.440 0.536 -0.059 -0.519 0.01219 0.19908 0.13239 169 12 0.59 119 2 23 14.982 0.371 -0.048 -0.503 0.01133 0.16140 0.13239 169 12 0.59 119 2 24 15.525 0.241 -0.038 -0.487 0.01029 0.12728 0.13238 169 12 0.59 119 2 25 16.067 0.142 -0.028 -0.472 0.00913 0.09702 0.13238 169 12 0.59 119 2 26 16.609 0.070 -0.020 -0.457 0.00787 0.07084 0.13237 169 12 0.59 119 2 27 17.152 0.021 -0.014 -0.442 0.00653 0.04887 0.13237 169 12 0.59 119 2 28 17.694 -0.009 -0.008 -0.427 0.00515 0.03116 0.13237 169 12 0.59 119 2 29 18.236 -0.025 -0.004 -0.412 0.00379 0.01766 0.13237 169 12 0.59 119 2 30 18.779 -0.030 -0.001 -0.398 0.00260 0.00801 0.13236 169 12 0.59 119 2 31 19.321 -0.030 0.000 -0.384 0.00163 0.00162 0.13236 169 12 0.59 119 2 32 19.864 -0.025 0.001 -0.370 0.00090 -0.00217 0.13236 169 12 0.59 119 2 33 20.406 -0.019 0.001 -0.356 0.00039 -0.00401 0.13236 169 12 0.59 119 2 34 20.948 -0.013 0.001 -0.343 0.00007 -0.00443 0.13236 169 12 0.59 119 2 35 21.491 -0.008 0.001 -0.330 -0.00010 -0.00397 0.13236 169 12 0.59 119 2 36 22.033 -0.005 0.001 -0.318 -0.00017 -0.00314 0.13235 169 12 0.59 119 2 37 22.575 -0.002 0.000 -0.306 -0.00018 -0.00224 0.13235 169 12 0.59 119 2 38 23.118 -0.001 0.000 -0.294 -0.00015 -0.00146 0.13235 169 12 0.59 119 2 39 23.660 0.000 0.000 -0.283 -0.00012 -0.00085 0.13235 169 12 0.59 119 2 40 24.203 0.000 0.000 -0.272 -0.00008 -0.00043 0.13235 169 12 0.59 119 2 41 24.745 0.000 0.000 -0.262 -0.00005 -0.00017 0.13235 169 12 0.59 119 2 42 25.287 0.000 0.000 -0.253 -0.00002 -0.00003 0.13235 169 12 0.59 119 2 43 25.830 0.000 0.000 -0.244 -0.00001 0.00003 0.13235 169 12 0.59 119 2 44 26.372 0.000 0.000 -0.236 0.00000 0.00005 0.13234 169 12 0.59 119 2 45 26.914 0.000 0.000 -0.228 0.00000 0.00005 0.13234 169 12 0.59 119 2 46 27.457 0.000 0.000 -0.221 0.00000 0.00004 0.13234 169 12 0.59 119 2 47 27.999 0.000 0.000 -0.214 0.00000 0.00003 0.13234 169 12 0.59 119 2 48 28.542 0.000 0.000 -0.208 0.00000 0.00002 0.13234 169 12 0.59 119 2 49 29.084 0.000 0.000 -0.203 0.00000 0.00002 0.13234 169 12 0.59 119 2 50 29.626 0.000 0.000 -0.197 0.00000 0.00001 0.13234 169 12 0.59 119 2 51 30.169 0.000 0.000 -0.192 0.00000 0.00001 0.13234 169 12 0.59 119 2 52 30.711 0.000 0.000 -0.187 0.00000 0.00000 0.13233 169 12 0.59 119 2 53 31.253 0.000 0.000 -0.183 0.00000 0.00000 0.13233 169 12 0.59 119 2 54 31.796 0.000 0.000 -0.178 0.00000 0.00000 0.13233 169 12 0.59 119 2 55 32.338 0.000 0.000 -0.174 0.00000 0.00000 0.13233 169 12 0.59 119 2 56 32.881 0.000 0.000 -0.169 0.00000 0.00000 0.13233 169 12 0.59 119 2 57 33.423 0.000 0.000 -0.165 0.00000 0.00000 0.13233 169 12 0.59 119 2 58 33.965 0.000 0.000 -0.161 0.00000 0.00000 0.13233 169 12 0.59 119 2 59 34.508 0.000 0.000 -0.157 0.00000 0.00000 0.13233 169 12 0.59 119 3 1 35.050 0.000 0.000 -0.153 0.00000 0.00000 0.13233 169 12 0.59 119 3 2 35.557 0.000 0.000 -0.150 0.00000 0.00000 0.13233 169 12 0.59 119 3 3 36.063 0.000 0.000 -0.148 0.00000 0.00000 0.13233 169 12 0.59 119 4 1 36.570 0.000 0.000 -0.145 0.00000 0.00000 0.13232 169 12 0.59 119 4 2 37.129 0.000 0.000 -0.141 0.00000 0.00000 0.13232 169 12 0.59 119 4 3 37.687 0.000 0.000 -0.138 0.00000 0.00000 0.13232 169 12 0.59 119 4 4 38.246 0.000 0.000 -0.134 0.00000 0.00000 0.13232 169 12 0.59 119 4 5 38.805 0.000 0.000 -0.131 0.00000 0.00000 0.13232 169 12 0.59 119 4 6 39.363 0.000 0.000 -0.127 0.00000 0.00000 0.13232 169 12 0.59 119 4 7 39.922 0.000 0.000 -0.124 0.00000 0.00000 0.13232 169 12 0.59 119 4 8 40.481 0.000 0.000 -0.121 0.00000 0.00000 0.13232 169 12 0.59 119 4 9 41.039 0.000 0.000 -0.118 0.00000 0.00000 0.13232 169 12 0.59 119 4 10 41.598 0.000 0.000 -0.114 0.00000 0.00000 0.13232 169 12 0.59 119 4 11 42.157 0.000 0.000 -0.111 0.00000 0.00000 0.13232 169 12 0.59 119 4 12 42.715 0.000 0.000 -0.108 0.00000 0.00000 0.13232 169 12 0.59 119 4 13 43.274 0.000 0.000 -0.106 0.00000 0.00000 0.13232 169 12 0.59 119 4 14 43.833 0.000 0.000 -0.103 0.00000 0.00000 0.13232 169 12 0.59 119 4 15 44.391 0.000 0.000 -0.100 0.00000 0.00000 0.13232 169 12 0.59 119 4 16 44.950 0.000 0.000 -0.098 0.00000 0.00000 0.13232 169 12 0.59 119 4 17 45.509 0.000 0.000 -0.096 0.00000 0.00000 0.13231 169 12 0.59 119 4 18 46.067 0.000 0.000 -0.093 0.00000 0.00000 0.13231 169 12 0.59 119 4 19 46.626 0.000 0.000 -0.091 0.00000 0.00000 0.13231 169 12 0.59 119 4 20 47.185 0.000 0.000 -0.089 0.00000 0.00000 0.13231 169 12 0.59 119 4 21 47.743 0.000 0.000 -0.087 0.00000 0.00000 0.13231 169 12 0.59 119 4 22 48.302 0.000 0.000 -0.085 0.00000 0.00000 0.13231





3.323

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3.324

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3.325

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0.00000 -7.72251 169 12 0.59 841 1 83 46.166 0.000 0.000 -0.007 0.00000 0.00000 -7.72248 169 12 0.59 841 1 84 46.729 0.000 0.000 -0.007 0.00000 0.00000 -7.72244 169 12 0.59 841 1 85 47.292 0.000 0.000 -0.007 0.00000 0.00000 -7.72241 169 12 0.59 841 1 86 47.855 0.000 0.000 -0.007 0.00000 0.00000 -7.72238 169 12 0.59 841 1 87 48.418 0.000 0.000 -0.007 0.00000 0.00000 -7.72235 169 12 0.59 841 1 88 48.981 0.000 0.000 -0.007 0.00000 0.00000 -7.72232 169 12 0.59 841 1 89 49.544 0.000 0.000 -0.007 0.00000 0.00000 -7.72230 169 12 0.59 841 1 90 50.107 0.000 0.000 -0.007 0.00000 0.00000 -7.72228 169 12 0.59 841 1 91 50.670 0.000 0.000 -0.007 0.00000 0.00000 -7.72226 169 12 0.59 841 1 92 51.233 0.000 0.000 -0.007 0.00000 0.00000 -7.72224 169 12 0.59 841 1 93 51.796 0.000 0.000 -0.007 0.00000 0.00000 -7.72222 169 12 0.59 841 1 94 52.359 0.000 0.000 -0.007 0.00000 0.00000 -7.72220 169 12 0.59 841 1 95 52.922 0.000 0.000 -0.007 0.00000 0.00000 -7.72219 169 12 0.59 841 1 96 53.485 0.000 0.000 -0.007 0.00000 0.00000 -7.72218 169 12 0.59 841 1 97 54.048 0.000 0.000 -0.007 0.00000 0.00000 -7.72217 169 12 0.59 841 1 98 54.611 0.000 0.000 -0.007 0.00000 0.00000 -7.72216 169 12 0.59 841 1 99 55.174 0.000 0.000 -0.007 0.00000 0.00000 -7.72216 169 12 0.59 841 1 100 55.737 0.000 0.000 -0.007 0.00000 0.00000 -7.72215 169 12 0.59 841 1 101 56.300 0.000 0.000 -0.007 0.00000 0.00000 -7.72215 169 12 0.59 722 1 1 0.000 14.024 0.003 -0.223 -0.00635 0.80577 -0.80605 169 12 0.59 722 1 2 0.563 13.210 0.007 -0.210 -0.00707 0.82969 -0.80601 169 12 0.59 722 1 3 1.126 12.378 0.012 -0.197 -0.00769 0.84528 -0.80597 169 12 0.59 722 1 4 1.689 11.534 0.016 -0.184 -0.00823 0.85286 -0.80593 169 12 0.59 722 1 5 2.252 10.687 0.019 -0.170 -0.00869 0.85279 -0.80589 169 12 0.59 722 1 6 2.815 9.845 0.022 -0.157 -0.00906 0.84547 -0.80586 169 12 0.59 722 1 7 3.378 9.013 0.025 -0.144 -0.00934 0.83135 -0.80583 169 12 0.59 722 1 8 3.941 8.199 0.027 -0.131 -0.00954 0.81089 -0.80579 169 12 0.59 722 1 9 4.504 7.409 0.028 -0.119 -0.00966 0.78467 -0.80576 169 12 0.59 722 1 10 5.067 6.647 0.029 -0.108 -0.00970 0.75338 -0.80574 169 12 0.59 722 1 11 5.630 5.920 0.030 -0.098 -0.00966 0.71788 -0.80571 169 12 0.59 722 1 12 6.193 5.230 0.030 -0.089 -0.00956 0.67901 -0.80568 169 12 0.59 722 1 13 6.756 4.581 0.030 -0.080 -0.00938 0.63753 -0.80566 169 12 0.59 722 1 14 7.319 3.974 0.029 -0.073 -0.00914 0.59408 -0.80564 169 12 0.59 722 1 15 7.882 3.410 0.028 -0.067 -0.00884 0.54918 -0.80561 169 12 0.59 722 1 16 8.445 2.892 0.027 -0.061 -0.00849 0.50325 -0.80559 169 12 0.59 722 1 17 9.008 2.420 0.026 -0.056 -0.00808 0.45669 -0.80557 169 12 0.59 722 1 18 9.571 1.995 0.024 -0.052 -0.00762 0.40998 -0.80555 169 12 0.59 722 1 19 10.134 1.615 0.022 -0.049 -0.00712 0.36368 -0.80553 169 12 0.59 722 1 20 10.697 1.282 0.020 -0.046 -0.00658 0.31833 -0.80552 169 12 0.59 722 1 21 11.260 0.993 0.018 -0.044 -0.00601 0.27447 -0.80550 169 12 0.59 722 1 22 11.823 0.746 0.015 -0.042 -0.00543 0.23263 -0.80548 169 12 0.59 722 1 23 12.386 0.540 0.013 -0.041 -0.00484 0.19325 -0.80546 169 12 0.59 722 1 24 12.949 0.372 0.011 -0.039 -0.00424 0.15677 -0.80545 169 12 0.59 722 1 25 13.512 0.238 0.009 -0.038 -0.00365 0.12355 -0.80543 169 12 0.59 722 1 26 14.075 0.136 0.007 -0.037 -0.00308 0.09389 -0.80541 169 12 0.59 722 1 27 14.638 0.061 0.006 -0.036 -0.00254 0.06802 -0.80540 169 12 0.59 722 1 28 15.201 0.010 0.004 -0.035 -0.00204 0.04604 -0.80538 169 12 0.59 722 1 29 15.764 -0.022 0.003 -0.035 -0.00158 0.02802 -0.80537 169 12 0.59 722 1 30 16.327 -0.038 0.002 -0.034 -0.00117 0.01395 -0.80535 169 12 0.59 722 1 31 16.890 -0.042 0.001 -0.033 -0.00082 0.00379 -0.80534 169 12 0.59 722 1 32 17.453 -0.038 0.000 -0.032 -0.00052 -0.00253 -0.80533 169 12 0.59 722 1 33 18.016 -0.031 0.000 -0.032 -0.00028 -0.00561 -0.80531 169 12 0.59 722 1 34 18.579 -0.023 0.000 -0.031 -0.00010 -0.00653 -0.80530 169 12 0.59 722 1 35 19.142 -0.016 0.000 -0.030 0.00001 -0.00615 -0.80529 169 12 0.59 722 1 36 19.705 -0.010 0.000 -0.029 0.00008 -0.00511 -0.80527





3.326

169 12 0.59 722 1 37 20.268 -0.005 0.000 -0.029 0.00010 -0.00384 -0.80526 169 12 0.59 722 1 38 20.831 -0.002 0.000 -0.028 0.00010 -0.00261 -0.80525 169 12 0.59 722 1 39 21.394 0.000 0.000 -0.027 0.00008 -0.00157 -0.80523 169 12 0.59 722 1 40 21.957 0.001 0.000 -0.026 0.00006 -0.00080 -0.80522 169 12 0.59 722 1 41 22.520 0.001 0.000 -0.026 0.00004 -0.00030 -0.80521 169 12 0.59 722 1 42 23.083 0.001 0.000 -0.025 0.00002 -0.00001 -0.80520 169 12 0.59 722 1 43 23.646 0.000 0.000 -0.025 0.00001 0.00011 -0.80519 169 12 0.59 722 1 44 24.209 0.000 0.000 -0.024 0.00000 0.00013 -0.80518 169 12 0.59 722 1 45 24.772 0.000 0.000 -0.024 0.00000 0.00010 -0.80516 169 12 0.59 722 1 46 25.335 0.000 0.000 -0.023 0.00000 0.00007 -0.80515 169 12 0.59 722 1 47 25.898 0.000 0.000 -0.023 0.00000 0.00004 -0.80514 169 12 0.59 722 1 48 26.461 0.000 0.000 -0.022 0.00000 0.00002 -0.80513 169 12 0.59 722 1 49 27.024 0.000 0.000 -0.022 0.00000 0.00001 -0.80512 169 12 0.59 722 1 50 27.587 0.000 0.000 -0.022 0.00000 0.00000 -0.80511 169 12 0.59 722 1 51 28.150 0.000 0.000 -0.021 0.00000 0.00000 -0.80510 169 12 0.59 722 1 52 28.713 0.000 0.000 -0.021 0.00000 0.00000 -0.80509 169 12 0.59 722 1 53 29.276 0.000 0.000 -0.021 0.00000 0.00000 -0.80508 169 12 0.59 722 1 54 29.839 0.000 0.000 -0.020 0.00000 0.00000 -0.80507 169 12 0.59 722 1 55 30.402 0.000 0.000 -0.020 0.00000 0.00000 -0.80506 169 12 0.59 722 1 56 30.965 0.000 0.000 -0.020 0.00000 0.00000 -0.80505 169 12 0.59 722 1 57 31.528 0.000 0.000 -0.020 0.00000 0.00000 -0.80504 169 12 0.59 722 1 58 32.091 0.000 0.000 -0.020 0.00000 0.00000 -0.80504 169 12 0.59 722 1 59 32.654 0.000 0.000 -0.019 0.00000 0.00000 -0.80503 169 12 0.59 722 1 60 33.217 0.000 0.000 -0.019 0.00000 0.00000 -0.80502 169 12 0.59 722 1 61 33.780 0.000 0.000 -0.019 0.00000 0.00000 -0.80501 169 12 0.59 722 1 62 34.343 0.000 0.000 -0.019 0.00000 0.00000 -0.80500 169 12 0.59 722 1 63 34.906 0.000 0.000 -0.018 0.00000 0.00000 -0.80499 169 12 0.59 722 1 64 35.469 0.000 0.000 -0.018 0.00000 0.00000 -0.80499 169 12 0.59 722 1 65 36.032 0.000 0.000 -0.018 0.00000 0.00000 -0.80498 169 12 0.59 722 1 66 36.595 0.000 0.000 -0.018 0.00000 0.00000 -0.80497 169 12 0.59 722 1 67 37.158 0.000 0.000 -0.018 0.00000 0.00000 -0.80497 169 12 0.59 722 1 68 37.721 0.000 0.000 -0.017 0.00000 0.00000 -0.80496 169 12 0.59 722 1 69 38.284 0.000 0.000 -0.017 0.00000 0.00000 -0.80495 169 12 0.59 722 1 70 38.847 0.000 0.000 -0.017 0.00000 0.00000 -0.80495 169 12 0.59 722 1 71 39.410 0.000 0.000 -0.017 0.00000 0.00000 -0.80494 169 12 0.59 722 1 72 39.973 0.000 0.000 -0.017 0.00000 0.00000 -0.80493 169 12 0.59 722 1 73 40.536 0.000 0.000 -0.016 0.00000 0.00000 -0.80493 169 12 0.59 722 1 74 41.099 0.000 0.000 -0.016 0.00000 0.00000 -0.80492 169 12 0.59 722 1 75 41.662 0.000 0.000 -0.016 0.00000 0.00000 -0.80492 169 12 0.59 722 1 76 42.225 0.000 0.000 -0.016 0.00000 0.00000 -0.80491 169 12 0.59 722 1 77 42.788 0.000 0.000 -0.016 0.00000 0.00000 -0.80491 169 12 0.59 722 1 78 43.351 0.000 0.000 -0.015 0.00000 0.00000 -0.80490 169 12 0.59 722 1 79 43.914 0.000 0.000 -0.015 0.00000 0.00000 -0.80490 169 12 0.59 722 1 80 44.477 0.000 0.000 -0.015 0.00000 0.00000 -0.80489 169 12 0.59 722 1 81 45.040 0.000 0.000 -0.015 0.00000 0.00000 -0.80489 169 12 0.59 722 1 82 45.603 0.000 0.000 -0.015 0.00000 0.00000 -0.80489 169 12 0.59 722 1 83 46.166 0.000 0.000 -0.015 0.00000 0.00000 -0.80488 169 12 0.59 722 1 84 46.729 0.000 0.000 -0.014 0.00000 0.00000 -0.80488 169 12 0.59 722 1 85 47.292 0.000 0.000 -0.014 0.00000 0.00000 -0.80487 169 12 0.59 722 1 86 47.855 0.000 0.000 -0.014 0.00000 0.00000 -0.80487 169 12 0.59 722 1 87 48.418 0.000 0.000 -0.014 0.00000 0.00000 -0.80487 169 12 0.59 722 1 88 48.981 0.000 0.000 -0.014 0.00000 0.00000 -0.80487 169 12 0.59 722 1 89 49.544 0.000 0.000 -0.014 0.00000 0.00000 -0.80486 169 12 0.59 722 1 90 50.107 0.000 0.000 -0.013 0.00000 0.00000 -0.80486 169 12 0.59 722 1 91 50.670 0.000 0.000 -0.013 0.00000 0.00000 -0.80486 169 12 0.59 722 1 92 51.233 0.000 0.000 -0.013 0.00000 0.00000 -0.80486 169 12 0.59 722 1 93 51.796 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 94 52.359 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 95 52.922 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 96 53.485 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 97 54.048 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 98 54.611 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 99 55.174 0.000 0.000 -0.013 0.00000 0.00000 -0.80485 169 12 0.59 722 1 100 55.737 0.000 0.000 -0.012 0.00000 0.00000 -0.80485 169 12 0.59 722 1 101 56.300 0.000 0.000 -0.012 0.00000 0.00000 -0.80485

3.14.3.3.-Pile Internal Force Report (Esfuerzos en pilotes) Load Load Load Pilehead Pilehead ***** Forces (KG ) ***** *** Moments (CM-KG ) *** Step Cond Factor Joint Seg Subseg Distance X Y Z Mx My Mz 169 12 0.59 102 1 1 0.000 553873.125 129270.570 115.925 1490.9 -153751.8 77981720.0 169 12 0.59 102 1 2 0.508 552426.000 127241.883 114.310 1407.1 -147860.1 71411592.0 169 12 0.59 102 1 3 1.017 551203.250 125034.273 112.666 1337.0 -142050.3 64944576.0 169 12 0.59 102 1 4 1.525 549900.000 122654.203 110.969 1279.2 -136323.9 58589756.0 169 12 0.59 102 1 5 2.033 548516.625 120107.922 109.201 1232.1 -130683.7 52355904.0 169 12 0.59 102 1 6 2.542 547053.563 117401.938 107.349 1194.5 -125133.4 46251468.0 169 12 0.59 102 2 1 3.050 545544.438 114380.359 105.143 1157.4 -119677.1 40284560.0 169 12 0.59 102 2 2 3.598 543950.125 110996.570 102.652 1128.9 -113919.5 34021524.0 169 12 0.59 102 2 3 4.145 542093.813 106682.586 99.717 1108.1 -108298.4 27943774.0 169 12 0.59 102 2 4 4.693 539977.375 101469.547 96.283 1093.3 -102838.0 22102238.0 169 12 0.59 102 2 5 5.241 537739.313 95979.438 92.610 1082.9 -97565.7 16546150.0 169 12 0.59 102 2 6 5.788 535555.063 90965.766 89.097 1075.6 -92494.6 11290679.0 169 12 0.59 102 2 7 6.336 533430.000 86430.758 85.785 1070.1 -87615.9 6309738.0 169 12 0.59 102 2 8 6.884 531433.188 82567.461 82.824 1065.5 -82918.7 1577116.5





3.327

169 12 0.59 102 2 9 7.431 529564.813 79353.453 80.240 1060.7 -78383.7 -2943965.3 169 12 0.59 102 2 10 7.979 527737.563 76494.219 77.877 1055.1 -73990.2 -7289060.5 169 12 0.59 102 2 11 8.527 525602.000 72904.469 75.027 1047.7 -69726.1 -11477594.0 169 12 0.59 102 2 12 9.074 523173.125 68633.344 71.702 1037.9 -65618.2 -15469567.0 169 12 0.59 102 2 13 9.622 520705.469 64099.070 68.180 1025.3 -61692.3 -19227670.0 169 12 0.59 102 2 14 10.170 518202.094 59363.492 64.505 1009.5 -57959.4 -22737490.0 169 12 0.59 102 2 15 10.717 515705.625 54783.934 60.938 990.4 -54427.7 -25988010.0 169 12 0.59 102 2 16 11.265 513220.125 50372.551 57.499 967.9 -51091.4 -28987772.0 169 12 0.59 102 2 17 11.813 510747.250 46121.645 54.193 941.9 -47943.3 -31745982.0 169 12 0.59 102 2 18 12.360 508288.625 42023.086 51.025 912.5 -44976.3 -34271428.0 169 12 0.59 102 2 19 12.908 505845.781 38068.375 47.999 879.6 -42182.7 -36572456.0 169 12 0.59 102 2 20 13.455 503420.938 34324.930 45.176 843.5 -39554.9 -38656936.0 169 12 0.59 102 2 21 14.003 501015.438 30795.482 42.568 804.3 -37081.6 -40536436.0 169 12 0.59 102 2 22 14.551 497792.219 25912.322 39.069 761.9 -34751.1 -42222684.0 169 12 0.59 102 2 23 15.098 494588.875 21339.846 35.904 717.0 -32612.1 -43641544.0 169 12 0.59 102 2 24 15.646 491406.813 17050.170 33.072 670.0 -30646.5 -44810032.0 169 12 0.59 102 2 25 16.194 488247.531 13026.380 30.586 621.3 -28835.9 -45743636.0 169 12 0.59 102 2 26 16.741 485113.281 9464.837 28.593 571.3 -27161.4 -46456912.0 169 12 0.59 102 2 27 17.289 482004.594 6307.589 27.077 520.5 -25596.1 -46975172.0 169 12 0.59 102 2 28 17.837 475037.344 -27388.551 12.745 463.0 -24113.7 -47320552.0 169 12 0.59 102 2 29 18.384 467907.969 -55895.785 4.263 410.0 -23416.1 -45820852.0 169 12 0.59 102 2 30 18.932 460600.438 -79747.195 1.556 363.9 -23182.9 -42760212.0 169 12 0.59 102 2 31 19.480 453101.500 -97977.750 4.981 326.8 -23097.8 -38393560.0 169 12 0.59 102 2 32 20.027 445398.906 -106985.508 12.975 299.3 -22825.3 -33028668.0 169 12 0.59 102 2 33 20.575 435396.656 -108583.516 29.377 280.3 -22114.9 -27170546.0 169 12 0.59 102 2 34 21.123 425041.563 -100620.758 43.829 268.0 -20506.5 -21224924.0 169 12 0.59 102 2 35 21.670 414328.594 -87479.750 54.181 260.0 -18106.6 -15715312.0 169 12 0.59 102 2 36 22.218 403259.250 -72476.320 59.689 254.3 -15139.9 -10925252.0 169 12 0.59 102 2 37 22.766 391837.188 -57949.664 60.604 249.7 -11871.6 -6956723.0 169 12 0.59 102 2 38 23.313 380065.688 -45395.480 57.787 245.6 -8553.1 -3783618.8 169 12 0.59 102 2 39 23.861 365212.625 -27078.273 47.668 241.7 -5388.9 -1297933.9 169 12 0.59 102 2 40 24.409 349940.938 -13795.028 35.412 237.6 -2778.8 184769.9 169 12 0.59 102 2 41 24.956 334250.750 -4878.850 23.134 233.5 -839.8 940133.4 169 12 0.59 102 2 42 25.504 318141.719 558.459 12.218 229.4 427.0 1207280.9 169 12 0.59 102 2 43 26.052 301613.531 3413.978 3.374 225.3 1096.0 1176701.8 169 12 0.59 102 2 44 26.599 287751.938 3974.809 -0.141 221.2 1280.8 989765.3 169 12 0.59 102 2 45 27.147 273597.688 3875.252 -2.409 217.1 1273.1 772119.8 169 12 0.59 102 2 46 27.695 259150.719 3345.091 -3.512 213.0 1141.2 559925.6 169 12 0.59 102 2 47 28.242 244652.797 2539.054 -3.585 208.9 948.8 376761.1 169 12 0.59 102 2 48 28.790 230122.609 1545.927 -2.774 204.8 752.5 237732.1 169 12 0.59 102 2 49 29.337 215555.031 402.077 -1.217 200.7 600.6 153083.0 169 12 0.59 102 2 50 29.885 210857.078 369.905 -1.162 196.6 534.0 131066.7 169 12 0.59 102 2 51 30.433 206296.031 336.562 -1.097 192.5 470.3 110812.2 169 12 0.59 102 2 52 30.980 201868.656 303.054 -1.025 188.4 410.2 92383.3 169 12 0.59 102 2 53 31.528 197571.797 270.169 -0.949 184.3 354.1 75789.2 169 12 0.59 102 2 54 32.076 193402.391 238.508 -0.871 180.2 302.1 60995.7 169 12 0.59 102 2 55 32.623 189357.438 208.511 -0.792 176.1 254.5 47935.9 169 12 0.59 102 2 56 33.171 185434.109 180.483 -0.715 172.0 211.1 36518.7 169 12 0.59 102 2 57 33.719 181629.594 154.619 -0.640 167.9 172.0 26636.1 169 12 0.59 102 2 58 34.266 177941.219 131.021 -0.568 163.8 136.9 18169.7 169 12 0.59 102 2 59 34.814 174366.328 109.719 -0.501 159.7 105.8 10995.5 169 12 0.59 102 2 60 35.362 170902.406 90.684 -0.438 155.6 78.4 4987.7 169 12 0.59 102 2 61 35.909 167546.984 73.841 -0.380 151.5 54.4 22.2 169 12 0.59 102 2 62 36.457 164297.688 59.085 -0.328 147.4 33.6 -4021.1 169 12 0.59 102 2 63 37.005 161152.188 46.285 -0.280 143.3 15.6 -7256.4 169 12 0.59 102 2 64 37.552 158108.250 35.294 -0.238 139.2 0.3 -9790.8 169 12 0.59 102 3 1 38.100 155197.797 26.306 -0.202 131.0 -12.7 -11723.4 169 12 0.59 102 3 2 38.607 152400.844 18.919 -0.171 127.0 -23.0 -13056.0 169 12 0.59 102 3 3 39.113 149683.203 12.632 -0.143 122.9 -31.6 -14014.4 169 12 0.59 102 4 1 39.620 147016.203 7.137 -0.118 114.7 -38.9 -14654.3 169 12 0.59 102 4 2 40.169 144416.453 2.497 -0.096 110.6 -45.4 -15045.9 169 12 0.59 102 4 3 40.718 141909.391 -1.199 -0.077 106.5 -50.7 -15182.9 169 12 0.59 102 4 4 41.266 139493.094 -4.075 -0.062 102.4 -54.9 -15117.1 169 12 0.59 102 4 5 41.815 134564.531 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3.330

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3.331

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-6548.1 169 12 0.59 722 1 48 26.461 -8236.343 -30.919 0.682 2048.8 -178.4 -4146.2 169 12 0.59 722 1 49 27.024 -7643.719 -21.992 0.820 2010.1 -140.0 -2405.7 169 12 0.59 722 1 50 27.587 -7045.938 -13.627 0.724 1971.5 -93.9 -1167.8 169 12 0.59 722 1 51 28.150 -6442.493 -7.112 0.522 1932.8 -53.2 -400.7 169 12 0.59 722 1 52 28.713 -5832.803 -2.616 0.285 1894.1 -23.8 -0.4 169 12 0.59 722 1 53 29.276 -5216.197 0.223 0.039 1855.5 -7.7 146.9 169 12 0.59 722 1 54 29.839 -5081.313 0.264 0.033 1816.8 -5.5 134.3 169 12 0.59 722 1 55 30.402 -4959.348 0.282 0.027 1778.2 -3.7 119.5 169 12 0.59 722 1 56 30.965 -4850.005 0.281 0.021 1739.5 -2.2 103.6 169 12 0.59 722 1 57 31.528 -4753.005 0.269 0.016 1700.8 -1.0 87.8 169 12 0.59 722 1 58 32.091 -4668.085 0.248 0.012 1662.2 -0.1 72.6 169 12 0.59 722 1 59 32.654 -4594.996 0.222 0.008 1623.5 0.6 58.7 169 12 0.59 722 1 60 33.217 -4533.504 0.194 0.005 1584.8 1.1 46.2 169 12 0.59 722 1 61 33.780 -4483.389 0.166 0.003 1546.2 1.4 35.2 169 12 0.59 722 1 62 34.343 -4444.440 0.139 0.001 1507.5 1.5 25.9 169 12 0.59 722 1 63 34.906 -4416.458 0.114 0.000 1468.9 1.6 18.0 169 12 0.59 722 1 64 35.469 -4399.257 0.091 -0.001 1430.2 1.5 11.6 169 12 0.59 722 1 65 36.032 -4392.653 0.071 -0.002 1391.6 1.5 6.5 169 12 0.59 722 1 66 36.595 -4396.478 0.054 -0.002 1352.9 1.3 2.5 169 12 0.59 722 1 67 37.158 -4410.563 0.039 -0.003 1314.2 1.2 -0.5 169 12 0.59 722 1 68 37.721 -4434.751 0.027 -0.003 1275.6 1.1 -2.7 169 12 0.59 722 1 69 38.284 -4468.889 0.018 -0.003 1236.9 0.9 -4.3 169 12 0.59 722 1 70 38.847 -4512.994 0.010 -0.003 1198.3 0.7 -5.3 169 12 0.59 722 1 71 39.410 -4566.976 0.004 -0.002 1159.6 0.6 -5.8 169 12 0.59 722 1 72 39.973 -4630.685 0.000 -0.002 1121.0 0.5 -6.1 169 12 0.59 722 1 73 40.536 -4703.974 -0.003 -0.002 1082.3 0.3 -6.1 169 12 0.59 722 1 74 41.099 -4786.699 -0.006 -0.002 1043.6 0.2 -5.9 169 12 0.59 722 1 75 41.662 -4628.721 -0.009 -0.001 1005.0 0.1 -5.6 169 12 0.59 722 1 76 42.225 -4475.196 -0.011 -0.001 966.3 0.0 -5.1 169 12 0.59 722 1 77 42.788 -4325.968 -0.012 -0.001 927.7 0.0 -4.4 169 12 0.59 722 1 78 43.351 -4180.885 -0.012 0.000 889.0 -0.1 -3.7 169 12 0.59 722 1 79 43.914 -4039.800 -0.011 0.000 850.4 -0.1 -3.1 169 12 0.59 722 1 80 44.477 -3902.568 -0.010 0.000 811.7 -0.1 -2.4 169 12 0.59 722 1 81 45.040 -3769.048 -0.009 0.000 773.1 -0.1 -1.8 169 12 0.59 722 1 82 45.603 -3639.101 -0.008 0.000 734.4 -0.1 -1.3 169 12 0.59 722 1 83 46.166 -3512.594 -0.006 0.000 695.7 -0.1 -0.9 169 12 0.59 722 1 84 46.729 -3389.393 -0.005 0.000 657.1 -0.1 -0.5 169 12 0.59 722 1 85 47.292 -3269.371 -0.004 0.000 618.4 -0.1 -0.3 169 12 0.59 722 1 86 47.855 -3152.401 -0.003 0.000 579.8 -0.1 -0.1 169 12 0.59 722 1 87 48.418 -3038.359 -0.002 0.000 541.1 0.0 0.1 169 12 0.59 722 1 88 48.981 -2927.124 -0.001 0.000 502.5 0.0 0.2 169 12 0.59 722 1 89 49.544 -2818.578 0.000 0.000 463.8 0.0 0.2 169 12 0.59 722 1 90 50.107 -2712.605 0.000 0.000 425.2 0.0 0.2 169 12 0.59 722 1 91 50.670 -2609.090 0.000 0.000 386.5 0.0 0.2 169 12 0.59 722 1 92 51.233 -2507.922 0.000 0.000 347.9 0.0 0.2 169 12 0.59 722 1 93 51.796 -2408.989 0.001 0.000 309.2 0.0 0.2 169 12 0.59 722 1 94 52.359 -2312.185 0.001 0.000 270.6 0.0 0.2 169 12 0.59 722 1 95 52.922 -2217.403 0.001 0.000 231.9 0.0 0.1





3.332

169 12 0.59 722 1 96 53.485 -2124.537 0.001 0.000 193.3 0.0 0.1 169 12 0.59 722 1 97 54.048 -2064.190 0.000 0.000 154.6 0.0 0.1 169 12 0.59 722 1 98 54.611 -2006.211 0.000 0.000 116.0 0.0 0.0 169 12 0.59 722 1 99 55.174 -1950.533 0.000 0.000 77.3 0.0 0.0 169 12 0.59 722 1 100 55.737 -1897.094 0.000 0.000 38.7 0.0 0.0 169 12 0.59 722 1 101 56.300 -1897.094 0.000 0.000 38.7 0.0 0.0

3.14.3.4.-Pile Capacity Used Report (Capacidad de pilotes en kg) Load Load Load Pilehead Axial Total Capacity Step Cond Factor Joint Load Capacity Used (%) 169 12 0.59 102 553873.1 1038374.3 53.3 Tension 169 12 0.59 119 -357998.2 -792154.5 45.2 Compession 169 12 0.59 199 -358084.4 -792154.5 45.2 Compession 169 12 0.59 841 9831.6 703213.8 1.4 Tension 169 12 0.59 722 -18199.7 -651519.0 2.8 Compession

3.14.3.5.-Special Event History Report (Elemento plastificado) Load Load Load Length Step Cond Factor Joint Member Plate (M ) Subseg Plasticity Event 169 12 0.59 6 613 0.910 5 0.583 Plastic 169 12 0.59 6 613 1.094 6 0.583 Plastic 169 12 0.59 613 538 0.457 5 0.333 Plastic

proyecto f.32065 ” ingenierÍa bÁsica y de detalle … · con el propósito de determinar su...

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