LINEAS DE INFLUENCIA EN VIGAS CONTINUAS CURSO: PUENTES Y OBRAS DE ARTE, UNI. NAC. PEDRO RUIZ GALLO, CATED.: ING. ARTURO RODRIGUEZ SERQUEN

Tramo N° 1 2

Número de Tramos ( <=10 ): 2 12 12 26

N° de Secc. en el Tramo(<=30): 101 1 10 12 24 50 50 500 0 0 0 0 0

Localización de la SecciónTramo N° 1

Dist. del inicio del Tramo 12

2

Momento Cortante Deflex.RESULTADOS Máximo Valor: 0 0 0

X-Global Tramo X-Local Momento Cortante Deflex. Mínimo Valor: -1.152 -1 00 1 0 0 0 0 Area Positiva: 0 0 0

1.2 1.2 -0.297 -0.12475 0 Area Negativa: -17.82 -7.485 02.4 2.4 -0.576 -0.248 0 Area Total: -17.82 -7.485 03.6 3.6 -0.819 -0.36825 04.8 4.8 -1.008 -0.484 0

6 6 -1.125 -0.59375 07.2 7.2 -1.152 -0.696 08.4 8.4 -1.071 -0.78925 09.6 9.6 -0.864 -0.872 0

10.8 10.8 -0.513 -0.94275 012 12 0 -1 012 2 0 0 0 0

13.2 1.2 -0.513 -0.04275 014.4 2.4 -0.864 -0.072 015.6 3.6 -1.071 -0.08925 016.8 4.8 -1.152 -0.096 0

18 6 -1.125 -0.09375 019.2 7.2 -1.008 -0.084 020.4 8.4 -0.819 -0.06825 021.6 9.6 -0.576 -0.048 022.8 10.8 -0.297 -0.02475 0

Long. de Tramo:

RigidezEI

0 5 10 15 200

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

Fuerzas Internas

Reacción de Apoyo

Opciones de Análisis

24 12 0 0 0

Bending Moment Analysis OptionShear Force

DeflectionsReactions

11 8

Point load in span 2 Moment in simple beam under Point load:Distance from the beginning of span: 12 Msimple= 0

-X(L-X)/(6LEI): 0

01 2 3 4 5 6 7 8 9

0 0 0 0 0 0 0 00 0 0 0 #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!0 0 0 #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!0 0 0 #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!0 0 1 0 0 0 0 0 00 0 1 #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0! #DIV/0!

Section in span 1Distance from the beginning of span: 12

Mp 10 0

M = 0

Vp 10 0

V = 0

Simple span moments in statically determined structure1 20 0

R =

Defined Ranges

Stiffness Matrix [d]

Load Vector [Dp]

[Dp]

D_IL =OFFSET(X_Global,,5)deltaP =OFFSET(p1x10,0,0,1,Nspans-1)

DiagramLink =Input!$I$13EI =Input!$G$5:$P$5

InfluenceLine =CHOOSE(DiagramLink,M_IL,V_IL,D_IL)L =Input!$G$4:$P$4

LoadSpan =Solver!$E$17LoadX =Solver!$E$18

M_IL =OFFSET(X_Global,,3)m10x10 =Solver!$B$6:$J$14

matrix =OFFSET(m10x10,0,0,Nspans-1,Nspans-1)Moment =Solver!$B$30Msimple =Solver!$H$18

Msup =Solver!$B$22:$J$22Nsections =Input!$D$5

Nspans =Input!$D$4p1x10 =Solver!$B$21:$J$21

SectionSpan =Solver!$E$24SectionX =Solver!$E$25

Shear =Solver!$B$35V_IL =OFFSET(X_Global,,4)

X =Solver!$E$18X_Global =OFFSET(X_Global_Big,,,COUNT(X_Global_Big))

X_Global_Big =Input!$A$18:$A$848XGLOBAL =Input!$A$18:$A$61XLoc1 =Input!$C$17

1 Piers1

23456789

1011

Moment in simple beam under Point load:

10 11 Piers0 Msup

#DIV/0! 0 Msup/Li-1#DIV/0! 0 Msup/Li#DIV/0! #DIV/0! Reaction Msup/L

0 0 Reaction in statically determined structure#DIV/0! #DIV/0! Reaction Total