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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 1,000,000
Max Cl/Cd: 125.15 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah94156-il-1000000.txt
Download as CSV file: xf-ah94156-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-156                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.4249   0.04563   0.04278  -0.1104   0.7733   0.0102
 -10.750  -0.5322   0.03470   0.03126  -0.1029   0.7694   0.0097
 -10.500  -0.5663   0.03097   0.02719  -0.0962   0.7664   0.0096
 -10.250  -0.5739   0.02868   0.02463  -0.0922   0.7637   0.0099
 -10.000  -0.5752   0.02625   0.02188  -0.0890   0.7609   0.0100
  -9.750  -0.5686   0.02424   0.01961  -0.0866   0.7591   0.0102
  -9.500  -0.5564   0.02263   0.01778  -0.0848   0.7572   0.0104
  -9.250  -0.5411   0.02124   0.01618  -0.0833   0.7552   0.0105
  -9.000  -0.5228   0.02014   0.01492  -0.0822   0.7532   0.0107
  -8.750  -0.5020   0.01940   0.01403  -0.0814   0.7513   0.0109
  -8.500  -0.4810   0.01853   0.01301  -0.0806   0.7493   0.0111
  -8.250  -0.4603   0.01747   0.01177  -0.0798   0.7473   0.0113
  -8.000  -0.4413   0.01597   0.01012  -0.0788   0.7451   0.0117
  -7.750  -0.4181   0.01537   0.00949  -0.0783   0.7438   0.0121
  -7.500  -0.3942   0.01484   0.00892  -0.0779   0.7421   0.0124
  -7.250  -0.3695   0.01444   0.00848  -0.0777   0.7403   0.0129
  -7.000  -0.3445   0.01406   0.00805  -0.0774   0.7384   0.0135
  -6.750  -0.3193   0.01368   0.00761  -0.0771   0.7365   0.0140
  -6.500  -0.2940   0.01332   0.00720  -0.0769   0.7348   0.0143
  -6.250  -0.2700   0.01278   0.00658  -0.0764   0.7330   0.0146
  -6.000  -0.2480   0.01208   0.00582  -0.0757   0.7311   0.0155
  -5.750  -0.2227   0.01175   0.00548  -0.0755   0.7293   0.0162
  -5.500  -0.1969   0.01145   0.00517  -0.0753   0.7277   0.0170
  -5.250  -0.1708   0.01117   0.00486  -0.0752   0.7259   0.0178
  -5.000  -0.1447   0.01089   0.00455  -0.0750   0.7240   0.0187
  -4.750  -0.1195   0.01051   0.00415  -0.0748   0.7221   0.0205
  -4.500  -0.0928   0.01030   0.00393  -0.0747   0.7203   0.0221
  -4.250  -0.0661   0.01008   0.00367  -0.0747   0.7185   0.0238
  -4.000  -0.0398   0.00984   0.00342  -0.0746   0.7166   0.0274
  -3.750  -0.0130   0.00966   0.00322  -0.0746   0.7146   0.0319
  -3.500   0.0138   0.00943   0.00304  -0.0746   0.7130   0.0404
  -3.250   0.0403   0.00918   0.00288  -0.0746   0.7112   0.0577
  -3.000   0.0661   0.00886   0.00272  -0.0745   0.7091   0.0978
  -2.750   0.0912   0.00848   0.00256  -0.0743   0.7069   0.1609
  -2.500   0.1155   0.00802   0.00241  -0.0741   0.7049   0.2515
  -2.250   0.1392   0.00752   0.00228  -0.0738   0.7028   0.3620
  -1.750   0.1822   0.00622   0.00202  -0.0723   0.6982   0.6685
  -1.500   0.2048   0.00604   0.00228  -0.0711   0.6957   0.7889
  -1.250   0.2338   0.00615   0.00235  -0.0713   0.6930   0.8136
  -1.000   0.2625   0.00632   0.00249  -0.0714   0.6905   0.8265
  -0.750   0.2905   0.00654   0.00270  -0.0713   0.6881   0.8351
  -0.500   0.3194   0.00673   0.00282  -0.0715   0.6854   0.8421
  -0.250   0.3473   0.00682   0.00293  -0.0715   0.6830   0.8462
   0.000   0.3750   0.00696   0.00307  -0.0714   0.6804   0.8505
   0.250   0.4033   0.00709   0.00319  -0.0715   0.6775   0.8560
   0.500   0.4311   0.00716   0.00324  -0.0715   0.6748   0.8600
   0.750   0.4581   0.00728   0.00334  -0.0712   0.6721   0.8631
   1.000   0.4855   0.00741   0.00346  -0.0711   0.6693   0.8667
   1.250   0.5136   0.00747   0.00353  -0.0713   0.6664   0.8704
   1.500   0.5423   0.00752   0.00357  -0.0716   0.6634   0.8734
   1.750   0.5686   0.00750   0.00355  -0.0714   0.6601   0.8756
   2.000   0.5956   0.00756   0.00358  -0.0712   0.6566   0.8777
   2.250   0.6229   0.00758   0.00362  -0.0713   0.6530   0.8798
   2.500   0.6508   0.00759   0.00364  -0.0715   0.6491   0.8815
   2.750   0.6790   0.00760   0.00365  -0.0718   0.6451   0.8832
   3.000   0.7073   0.00765   0.00365  -0.0722   0.6410   0.8848
   3.250   0.7360   0.00765   0.00369  -0.0726   0.6362   0.8861
   3.500   0.7646   0.00768   0.00371  -0.0731   0.6307   0.8871
   3.750   0.7917   0.00767   0.00368  -0.0732   0.6257   0.8881
   4.000   0.8187   0.00763   0.00368  -0.0733   0.6199   0.8890
   4.250   0.8450   0.00765   0.00367  -0.0733   0.6128   0.8898
   4.500   0.8719   0.00766   0.00371  -0.0734   0.6055   0.8907
   4.750   0.8981   0.00771   0.00375  -0.0733   0.5980   0.8915
   5.000   0.9248   0.00775   0.00380  -0.0734   0.5892   0.8921
   5.250   0.9502   0.00783   0.00387  -0.0732   0.5795   0.8930
   5.500   0.9749   0.00794   0.00395  -0.0730   0.5682   0.8939
   5.750   0.9998   0.00804   0.00405  -0.0727   0.5556   0.8945
   6.000   1.0237   0.00818   0.00416  -0.0724   0.5421   0.8951
   6.250   1.0462   0.00836   0.00430  -0.0717   0.5273   0.8961
   6.500   1.0675   0.00857   0.00447  -0.0708   0.5115   0.8969
   6.750   1.0858   0.00885   0.00468  -0.0694   0.4906   0.8976
   7.000   1.1016   0.00918   0.00492  -0.0676   0.4677   0.8983
   7.250   1.1146   0.00953   0.00519  -0.0652   0.4470   0.8992
   7.500   1.1233   0.00986   0.00546  -0.0619   0.4271   0.9003
   7.750   1.1326   0.01027   0.00581  -0.0589   0.4095   0.9009
   8.000   1.1408   0.01078   0.00625  -0.0558   0.3912   0.9015
   8.250   1.1467   0.01133   0.00673  -0.0526   0.3712   0.9025
   8.500   1.1535   0.01194   0.00728  -0.0496   0.3512   0.9036
   8.750   1.1589   0.01268   0.00795  -0.0466   0.3304   0.9047
   9.000   1.1637   0.01354   0.00871  -0.0436   0.3064   0.9056
   9.250   1.1674   0.01451   0.00957  -0.0407   0.2825   0.9064
   9.500   1.1748   0.01538   0.01036  -0.0383   0.2619   0.9072
   9.750   1.1787   0.01646   0.01133  -0.0357   0.2386   0.9080
  10.000   1.1820   0.01761   0.01236  -0.0330   0.2127   0.9088
  10.250   1.1864   0.01876   0.01340  -0.0307   0.1893   0.9095
  10.500   1.1887   0.02007   0.01457  -0.0281   0.1633   0.9103
  10.750   1.1933   0.02129   0.01568  -0.0260   0.1420   0.9111
  11.000   1.1970   0.02261   0.01690  -0.0238   0.1200   0.9120
  11.250   1.1980   0.02415   0.01829  -0.0216   0.0957   0.9128
  11.500   1.2022   0.02556   0.01960  -0.0197   0.0780   0.9134
  11.750   1.2065   0.02703   0.02098  -0.0180   0.0618   0.9139
  12.000   1.2138   0.02835   0.02227  -0.0166   0.0510   0.9144
  12.250   1.2202   0.02978   0.02365  -0.0153   0.0406   0.9149
  12.500   1.2271   0.03123   0.02507  -0.0141   0.0325   0.9153
  12.750   1.2347   0.03266   0.02648  -0.0130   0.0264   0.9160
  13.000   1.2409   0.03422   0.02804  -0.0119   0.0210   0.9168
  13.250   1.2478   0.03580   0.02961  -0.0109   0.0173   0.9175
  13.500   1.2560   0.03731   0.03117  -0.0100   0.0151   0.9182
  13.750   1.2629   0.03896   0.03284  -0.0092   0.0134   0.9189
  14.000   1.2706   0.04059   0.03454  -0.0085   0.0123   0.9196
  14.250   1.2792   0.04217   0.03617  -0.0079   0.0113   0.9204
  14.500   1.2843   0.04412   0.03815  -0.0073   0.0103   0.9212
  14.750   1.2891   0.04615   0.04026  -0.0067   0.0096   0.9220
  15.000   1.2970   0.04793   0.04210  -0.0063   0.0093   0.9227
  15.250   1.3030   0.04993   0.04417  -0.0059   0.0087   0.9235
  15.500   1.3090   0.05198   0.04629  -0.0057   0.0085   0.9244
  15.750   1.3144   0.05415   0.04851  -0.0055   0.0081   0.9252
  16.000   1.3146   0.05694   0.05139  -0.0053   0.0077   0.9261
  16.250   1.3087   0.06051   0.05507  -0.0051   0.0074   0.9268
  16.500   1.3153   0.06272   0.05735  -0.0053   0.0071   0.9277
  16.750   1.3168   0.06559   0.06031  -0.0055   0.0072   0.9286
  17.000   1.3196   0.06839   0.06320  -0.0058   0.0069   0.9298
  17.250   1.3223   0.07120   0.06610  -0.0062   0.0067   0.9313
  17.500   1.3222   0.07445   0.06944  -0.0068   0.0065   0.9327
  17.750   1.3228   0.07767   0.07276  -0.0075   0.0064   0.9343
  18.000   1.3233   0.08099   0.07616  -0.0083   0.0062   0.9358
  18.250   1.3230   0.08448   0.07975  -0.0092   0.0061   0.9375
  18.500   1.3211   0.08826   0.08361  -0.0103   0.0058   0.9393
  18.750   1.3168   0.09248   0.08793  -0.0117   0.0057   0.9410
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