curvas polares nacas4110

7/24/2019 curvas polares nacas4110

1/21

X FOIL Version 6.99

Calcula ted polar for: S4110

1 1 Re nolds nu! "er #$ed % ac& nu!"e r #$ed

$trf ' 1.000 ( top) 1.000 (" otto!)

%ac& ' 0 Re ' 0.4*0 e 6 +cr it ' 9.

alp&a CL C, CL-C,

1 0.*164 0.00*9* *9.* /6./9916

1.1 0.*1 0.00*9/ *9./ //.142/1

1. 0.*2/ 0.00601 60.1 /9.4/4192

1.2 0.*4/4 0.00604 60.4 90.940

1.4 0.**9 0.0060/ 60./ 91.940/9*1.* 0.*69 0.00611 61.1 92.40*/9

1.6 0.*/02 0.0061* 61.* 94.2*26

1. 0.*909 0.00619 61.9 9*.4604

1./ 0.6014 0.0062 6.2 96.*290*2

1.9 0.61 0.006 6. 9.606***

0.6* 0.00622 62.2 9/.2412

.1 0.622 0.0062 62. 99.20*6*

. 0.6424 0.00642 64.2 100.060/

.2 0.6*2/ 0.0064/ 64./ 100./9*06

.4 0.664 0.006*4 6*.4 101.**9622

.* 0.64* 0.00661 66.1 10.0426

.6 0.6/49 0.00666 66.6 10./2/2/

. 0.69*2 0.0062 6.2 102.212*

./ 0.0** 0.006/1 6/.1 102.*96*1

.9 0.1*/ 0.006// 6/./ 104.04069/

2 0.6 0.00696 69.6 104.21024*

2.1 0.261 0.000* 0.* 104.41124/

2. 0.461 0.0014 1.4 104.49*9/

2.2 0.*6 0.004 .4 104.419/9

2.4 0.66 0.0024 2.4 104.2*962

2.* 0.6 0.004* 4.* 104.16104

2.6 0./*/ 0.00*6 *.6 102.94199

2. 0.9*6 0.006/ 6./ 102.*92*

2./ 0./0*2 0.00/ /. 10.99*4

2.9 0./149 0.0096 9.6 10.242

4 0./4* 0.00/1 /1 101.9012

4. 0./426 0.00/4 /4 100.4/*1

4.2 0./*2 0.00/*6 /*.6 99.6/9


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4.4 0./6 0.00/ /. 9/.9224/6

4.* 0./1 0.00//9 //.9 9/.09/9/6

4.6 0.//14 0.0090/ 90./ 9.004/46

4. 0./909 0.009* 9.* 96.212*12*

4./ 0.9002 0.00942 94.2 9*.41/9/

4.9 0.909/ 0.00961 96.1 94.6164

* 0.9191 0.009/ 9/ 92./*142*.1 0.9/* 0.00999 99.9 9.94949

*. 0.929 0.0101/ 101./ 9.1216206

*.2 0.942 0.0102 102. 91.2*004/

*.4 0.9*6 0.010** 10*.* 90.6/464*

*.* 0.966 0.0104 10.4 /9.96*61

*.6 0.9** 0.01092 109.2 /9.4912

*. 0.9/49 0.0111 111. //.*01429

*./ 0.9942 0.01121 112.1 /.9122*1

*.9 1.0029 0.0114/ 114./ /.442*

6 1.012 0.0116 116. /6./090/26.1 1.0* 0.011/ 11/. /6.141*222

6. 1.021 0.0104 10.4 /*.*914

6.2 1.0412 0.014 1.4 /*.02*94

6.4 1.0*1 0.014 14 /4.*/064*

6.* 1.0601 0.0161 16.1 /4.06/199/

6.6 1.0699 0.016 1.6 /2./4964

6. 1.0/9 0.019 19. /2.1/414

6./ 1.0//6 0.0121 121. /.9*61

6.9 1.099 0.0122 122. /.44949

1.10 0.012*1 12*.1 /1.929204

.1 1.116 0.01266 126.6 /1.49624

. 1.1* 0.012// 12/./ /1.1020**

.2 1.1249 0.0140 140. /0.6609/0/

.4 1.1444 0.014 14. /0.4/199

.* 1.1*22 0.01444 144.4 9./6/411

.6 1.162 0.0146* 146.* 9.22//4

. 1.11 0.014/ 14/ 9.16/91/9

./ 1.1/06 0.01*0 1*0. /.601/64

.9 1.1//9 0.01*9 1*.9 .*602

/ 1.19/* 0.01*42 1*4.2 .622626

/.1 1.02 0.01*64 1*6.4 .1920946

/. 1.1* 0.01*9 1*9. 6.0/01*02

/.2 1.46 0.0161 161 6.06111/

/.4 1.22* 0.0169 16.9 *.12014

/.* 1.416 0.016* 16*. 4.920*9*

/.6 1.496 0.016/ 16/. 4.021

/. 1.*// 0.0102 10.2 2.91661

/./ 1.62 0.01* 1.* 2.466666


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/.9 1.*1 0.01*4 1*.4 .6966922

9 1./16 0.0196 19.6 1.2*/*46

9.1 1.90/ 0.01/11 1/1.1 1.**2/4

9. 1.992 0.01/21 1/2.1 0.96124

9.2 1.204 0.01/** 1/*.* 0.49/44

9.4 1.214/ 0.01//6 1//.6 69.1269

9.* 1.206 0.0192 192. 6/.2*40229.6 1.21 0.019 19 6.26*4/

9. 1.22*6 0.019/9 19/.9 6.149212

9./ 1.242* 0.001 01. 66.42*29

9.9 1.2*1 0.002 02. 66.22/44

10 1.2*/2 0.0066 06.6 6*.4*401

104.49*9/


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0 *0 100 1*0 00 *0 200 2*0 400

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X FOIL Version 6.99



$trf ' 1.000 ( top) 1.000 (" otto!)%ac& ' 0 Re ' 1.000 e 6 +cr it ' 9.

alp&a CL C, CL-C,

1.1 0.**2 0.004*/ 4*./ 114.69422

1. 0.*261 0.0046 46. 116.02/961

1.2 0.*46 0.0046/ 46./ 116./1629

1.4 0.**4 0.0042 4.2 11./42**

1.* 0.*6/1 0.004/ 4./ 11/./492

1. 0.*/92 0.00491 49.1 10.00261./ 0.*999 0.0049 49. 10.04*

1.9 0.6104 0.00*04 *0.4 11.111111

0.611 0.00*11 *1.1 11.*4*9//

.1 0.621 0.00*1 *1. 1.1/*6/

. 0.64 0.00** *.* 1.22/1

.2 0.6* 0.00*22 *2.2 1.4*/6

.4 0.6621 0.00*4 *4. 1.24212

.* 0.626 0.00**1 **.1 1.*04*4

.6 0.6/4 0.00*6 *6 1.14/*

. 0.6944 0.00*69 *6.9 1.02/664

./ 0.04/ 0.00*/ *./ 11.9216

.9 0.1*1 0.00*// */./ 11.61*646

2 0.*4 0.00*99 *9.9 11.101/26

2.1 0.2*6 0.00611 61.1 10.2999

2. 0.4* 0.0062 6.2 119.69*04

2.2 0.**9 0.0062* 62.* 119.0292

2.4 0.661 0.0064 64. 11/.40/02

2.6 0./66 0.0061 6.1 11./01/

2. 0.96 0.006/2 6/.2 116.6414*

2./ 0./06/ 0.0069 69. 11*.*2/

2.9 0./16/ 0.0011 1.1 114.//04*

4 0./69 0.004 .4 114.10

4.1 0./21 0.0026 2.6 112.26412

4. 0./42 0.0049 4.9 112.14166

4.2 0./*4 0.006 6. 11.*196/*

4.4 0./64 0.006 .6 111./2*1

4.* 0./4 0.009 9 111.06291

4.6 0.//4 0.00/0* /0.* 110.260*


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4. 0./9* 0.00/1/ /1./ 109.1//6

4./ 0.906 0.00/21 /2.1 109.1/1

4.9 0.916 0.00/4* /4.* 10/.*9116

*.1 0.92/ 0.00/1 /.1 10.669246

*. 0.94 0.00//* //.* 10.0/446

*.2 0.9*6 0.009 90 106.4

*.4 0.969 0.0091 91. 106.192/6*.* 0.9 0.009 9. 10*.469*6

*.6 0.9// 0.0092 92. 10*.44902

*. 0.999 0.009* 9*. 104./149

*./ 1.00/ 0.0096 96. 104./049*

*.9 1.01/ 0.009 9. 104.196*

6 1.0/ 0.009/9 9/.9 102.9626

6.1 1.02/1 0.0100 100. 102.6094

6. 1.04/1 0.01016 101.6 102.1*9449

6.2 1.0*/2 0.010 10. 102.041

6.4 1.06/1 0.01041 104.1 10.602666.* 1.0/1 0.010*4 10*.4 10./6*/

6.6 1.0// 0.0106* 106.* 10.1/404

6. 1.09/ 0.010/ 10/ 101.66666

6./ 1.10/ 0.01094 109.4 101.6146

6.9 1.11/ 0.01104 110.4 101.6/116

1.19 0.0111 111. 100.9*//

.1 1.12* 0.01122 112.2 100.2916

. 1.144 0.01146 114.6 100.1164

.2 1.1*4 0.011* 11*. 100.024*

.4 1.1669 0.0112 11.2 99.4996*9

.* 1.162 0.01191 119.1 9/.6*421

.6 1.1/6 0.0102 10.2 9/.6024912

. 1.19* 0.0119 11.9 9/.0//*9

./ 1.04/ 0.0129 12.9 9.29094

.9 1.14 0.01*1 1*.1 9.09/212

/ 1.4 0.0166 16.6 96.69/6

/.1 1.224 0.01/6 1/.6 9*.9099/

/. 1.46 0.0120* 120.* 9*.1/290/

/.2 1.*2 0.0121 121. 9*.0/219

/.4 1.616 0.01222 122.2 94.6426609

/.* 1.0 0.012*2 12*.2 92.911

/.6 1.94 0.012* 12.* 92.04

/. 1./// 0.01291 129.1 9.6*6/

/./ 1.9/2 0.0140* 140.* 9.40*694

/.9 1.20* 0.014 14. 91.949606

9 1.2162 0.01441 144.1 91.246/2

9.1 1.249 0.01464 146.4 90.49/6229

9. 1.222 0.01491 149.1 /9.416499


12/21

9.2 1.24 0.01*02 1*0.2 /9.224664

9.4 1.2*19 0.01*1/ 1*1./ /9.0*91

9.* 1.2609 0.01*24 1*2.4 //.1**

9.6 1.2696 0.01**4 1**.4 //.122/4/1

9. 1.2/ 0.01* 1*. /.2/11024

9./ 1.2/*/ 0.01606 160.6 /6.//9166

9.9 1.292 0.01622 162.2 /*.24*9/910 1.40/ 0.0164 164. /*.120419

1.4*/6


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X FOIL Version 6.99



$trf ' 1.000 ( top) 1.000 (" otto!)%ac& ' 0 Re ' 1.000 e 6 +cr it ' 9.

alp&a CL C, CL-C,

1.1 0.**2 0.004*/ 4*./ 114.69422

1. 0.*261 0.0046 46. 116.02/961

1.2 0.*46 0.0046/ 46./ 116./1629

1.4 0.**4 0.0042 4.2 11./42**

1.* 0.*6/1 0.004/ 4./ 11/./492

1. 0.*/92 0.00491 49.1 10.00261./ 0.*999 0.0049 49. 10.04*

1.9 0.6104 0.00*04 *0.4 11.111111

0.611 0.00*11 *1.1 11.*4*9//

.1 0.621 0.00*1 *1. 1.1/*6/

. 0.64 0.00** *.* 1.22/1

.2 0.6* 0.00*22 *2.2 1.4*/6

.4 0.6621 0.00*4 *4. 1.24212

.* 0.626 0.00**1 **.1 1.*04*4

.6 0.6/4 0.00*6 *6 1.14/*

. 0.6944 0.00*69 *6.9 1.02/664

./ 0.04/ 0.00*/ *./ 11.9216

.9 0.1*1 0.00*// */./ 11.61*646

2 0.*4 0.00*99 *9.9 11.101/26

2.1 0.2*6 0.00611 61.1 10.2999

2. 0.4* 0.0062 6.2 119.69*04

2.2 0.**9 0.0062* 62.* 119.0292

2.4 0.661 0.0064 64. 11/.40/02

2.6 0./66 0.0061 6.1 11./01/

2. 0.96 0.006/2 6/.2 116.6414*

2./ 0./06/ 0.0069 69. 11*.*2/

2.9 0./16/ 0.0011 1.1 114.//04*

4 0./69 0.004 .4 114.10

4.1 0./21 0.0026 2.6 112.26412

4. 0./42 0.0049 4.9 112.14166

4.2 0./*4 0.006 6. 11.*196/*

4.4 0./64 0.006 .6 111./2*1

4.* 0./4 0.009 9 111.06291

4.6 0.//4 0.00/0* /0.* 110.260*


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4. 0./9* 0.00/1/ /1./ 109.1//6

4./ 0.906 0.00/21 /2.1 109.1/1

4.9 0.916 0.00/4* /4.* 10/.*9116

*.1 0.92/ 0.00/1 /.1 10.669246

*. 0.94 0.00//* //.* 10.0/446

*.2 0.9*6 0.009 90 106.4

*.4 0.969 0.0091 91. 106.192/6*.* 0.9 0.009 9. 10*.469*6

*.6 0.9// 0.0092 92. 10*.44902

*. 0.999 0.009* 9*. 104./149

*./ 1.00/ 0.0096 96. 104./049*

*.9 1.01/ 0.009 9. 104.196*

6 1.0/ 0.009/9 9/.9 102.9626

6.1 1.02/1 0.0100 100. 102.6094

6. 1.04/1 0.01016 101.6 102.1*9449

6.2 1.0*/2 0.010 10. 102.041

6.4 1.06/1 0.01041 104.1 10.602666.* 1.0/1 0.010*4 10*.4 10./6*/

6.6 1.0// 0.0106* 106.* 10.1/404

6. 1.09/ 0.010/ 10/ 101.66666

6./ 1.10/ 0.01094 109.4 101.6146

6.9 1.11/ 0.01104 110.4 101.6/116

1.19 0.0111 111. 100.9*//

.1 1.12* 0.01122 112.2 100.2916

. 1.144 0.01146 114.6 100.1164

.2 1.1*4 0.011* 11*. 100.024*

.4 1.1669 0.0112 11.2 99.4996*9

.* 1.162 0.01191 119.1 9/.6*421

.6 1.1/6 0.0102 10.2 9/.6024912

. 1.19* 0.0119 11.9 9/.0//*9

./ 1.04/ 0.0129 12.9 9.29094

.9 1.14 0.01*1 1*.1 9.09/212

/ 1.4 0.0166 16.6 96.69/6

/.1 1.224 0.01/6 1/.6 9*.9099/

/. 1.46 0.0120* 120.* 9*.1/290/

/.2 1.*2 0.0121 121. 9*.0/219

/.4 1.616 0.01222 122.2 94.6426609

/.* 1.0 0.012*2 12*.2 92.911

/.6 1.94 0.012* 12.* 92.04

/. 1./// 0.01291 129.1 9.6*6/

/./ 1.9/2 0.0140* 140.* 9.40*694

/.9 1.20* 0.014 14. 91.949606

9 1.2162 0.01441 144.1 91.246/2

9.1 1.249 0.01464 146.4 90.49/6229

9. 1.222 0.01491 149.1 /9.416499


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9.2 1.24 0.01*02 1*0.2 /9.224664

9.4 1.2*19 0.01*1/ 1*1./ /9.0*91

9.* 1.2609 0.01*24 1*2.4 //.1**

9.6 1.2696 0.01**4 1**.4 //.122/4/1

9. 1.2/ 0.01* 1*. /.2/11024

9./ 1.2/*/ 0.01606 160.6 /6.//9166

9.9 1.292 0.01622 162.2 /*.24*9/910 1.40/ 0.0164 164. /*.120419

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curvas polares nacas4110

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