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AH 83-159 (ah83159-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 83-159 (ah83159-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.8 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah83159-il-1000000.txt
Download as CSV file: xf-ah83159-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 83-159                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.1438   0.08027   0.07767  -0.0892   0.7448   0.0119
 -11.000  -0.1464   0.07554   0.07294  -0.0911   0.7430   0.0119
 -10.750  -0.1473   0.07145   0.06884  -0.0928   0.7410   0.0121
 -10.500  -0.1556   0.06537   0.06278  -0.0955   0.7397   0.0121
 -10.250  -0.1651   0.05917   0.05660  -0.0985   0.7382   0.0122
 -10.000  -0.2383   0.03917   0.03643  -0.1109   0.7378   0.0118
  -9.750  -0.2640   0.03497   0.03214  -0.1110   0.7356   0.0119
  -9.500  -0.2839   0.03198   0.02905  -0.1096   0.7332   0.0120
  -9.250  -0.3059   0.02903   0.02595  -0.1068   0.7308   0.0119
  -9.000  -0.3241   0.02705   0.02385  -0.1028   0.7282   0.0120
  -8.750  -0.3293   0.02508   0.02177  -0.1002   0.7259   0.0121
  -8.500  -0.3296   0.02298   0.01956  -0.0981   0.7238   0.0122
  -8.250  -0.3988   0.02169   0.01671  -0.0921   0.7252   0.0088
  -8.000  -0.3821   0.01976   0.01452  -0.0908   0.7232   0.0088
  -7.750  -0.3597   0.01934   0.01404  -0.0904   0.7209   0.0092
  -7.500  -0.3387   0.01800   0.01252  -0.0897   0.7187   0.0092
  -7.250  -0.3163   0.01682   0.01117  -0.0890   0.7167   0.0093
  -7.000  -0.2930   0.01589   0.01011  -0.0885   0.7147   0.0094
  -6.750  -0.2689   0.01515   0.00925  -0.0882   0.7125   0.0096
  -6.500  -0.2449   0.01433   0.00835  -0.0877   0.7109   0.0096
  -6.250  -0.2209   0.01362   0.00757  -0.0873   0.7090   0.0098
  -6.000  -0.1958   0.01316   0.00707  -0.0871   0.7069   0.0102
  -5.750  -0.1712   0.01266   0.00651  -0.0867   0.7049   0.0104
  -5.500  -0.1466   0.01216   0.00595  -0.0864   0.7030   0.0107
  -5.250  -0.1221   0.01168   0.00540  -0.0860   0.7011   0.0110
  -5.000  -0.0969   0.01133   0.00497  -0.0858   0.6991   0.0112
  -4.750  -0.0726   0.01082   0.00440  -0.0854   0.6972   0.0118
  -4.500  -0.0472   0.01041   0.00398  -0.0852   0.6954   0.0132
  -4.250  -0.0204   0.01018   0.00374  -0.0853   0.6935   0.0149
  -4.000   0.0059   0.00987   0.00340  -0.0852   0.6916   0.0176
  -3.750   0.0328   0.00963   0.00317  -0.0853   0.6897   0.0231
  -3.500   0.0597   0.00940   0.00296  -0.0853   0.6879   0.0330
  -3.250   0.0867   0.00920   0.00281  -0.0855   0.6859   0.0493
  -3.000   0.1129   0.00890   0.00267  -0.0856   0.6838   0.0956
  -2.750   0.1381   0.00841   0.00250  -0.0857   0.6823   0.1858
  -2.500   0.1613   0.00762   0.00231  -0.0857   0.6804   0.3553
  -2.250   0.1836   0.00661   0.00207  -0.0856   0.6784   0.5790
  -2.000   0.2079   0.00614   0.00209  -0.0852   0.6765   0.7256
  -1.750   0.2362   0.00620   0.00220  -0.0853   0.6747   0.7614
  -1.500   0.2650   0.00632   0.00229  -0.0855   0.6728   0.7773
  -1.250   0.2941   0.00650   0.00241  -0.0858   0.6708   0.7901
  -1.000   0.3226   0.00675   0.00265  -0.0859   0.6689   0.7978
  -0.750   0.3513   0.00692   0.00281  -0.0861   0.6672   0.8055
  -0.500   0.3792   0.00713   0.00304  -0.0860   0.6652   0.8101
  -0.250   0.4078   0.00729   0.00318  -0.0862   0.6632   0.8149
   0.000   0.4368   0.00740   0.00326  -0.0866   0.6612   0.8192
   0.250   0.4644   0.00752   0.00338  -0.0865   0.6592   0.8217
   0.500   0.4924   0.00765   0.00350  -0.0866   0.6571   0.8242
   0.750   0.5209   0.00780   0.00361  -0.0869   0.6548   0.8268
   1.000   0.5495   0.00783   0.00365  -0.0872   0.6529   0.8294
   1.250   0.5788   0.00786   0.00367  -0.0878   0.6505   0.8317
   1.500   0.6079   0.00786   0.00366  -0.0884   0.6479   0.8333
   1.750   0.6359   0.00784   0.00364  -0.0886   0.6454   0.8344
   2.000   0.6641   0.00787   0.00365  -0.0889   0.6428   0.8355
   2.250   0.6923   0.00792   0.00369  -0.0892   0.6399   0.8366
   2.500   0.7202   0.00791   0.00371  -0.0895   0.6367   0.8377
   2.750   0.7485   0.00791   0.00372  -0.0898   0.6333   0.8389
   3.000   0.7767   0.00793   0.00374  -0.0902   0.6303   0.8402
   3.250   0.8052   0.00798   0.00377  -0.0906   0.6272   0.8414
   3.500   0.8336   0.00800   0.00382  -0.0911   0.6243   0.8427
   3.750   0.8620   0.00801   0.00386  -0.0915   0.6209   0.8440
   4.000   0.8905   0.00803   0.00389  -0.0920   0.6174   0.8454
   4.250   0.9190   0.00809   0.00394  -0.0925   0.6139   0.8465
   4.500   0.9471   0.00811   0.00398  -0.0929   0.6103   0.8474
   4.750   0.9744   0.00808   0.00400  -0.0931   0.6063   0.8482
   5.000   1.0014   0.00810   0.00403  -0.0933   0.6015   0.8491
   5.250   1.0281   0.00815   0.00410  -0.0934   0.5964   0.8500
   5.500   1.0550   0.00816   0.00417  -0.0935   0.5902   0.8510
   5.750   1.0809   0.00824   0.00423  -0.0935   0.5832   0.8519
   6.000   1.1073   0.00828   0.00432  -0.0935   0.5744   0.8528
   6.250   1.1328   0.00836   0.00442  -0.0934   0.5650   0.8538
   6.500   1.1573   0.00848   0.00453  -0.0932   0.5537   0.8548
   6.750   1.1806   0.00863   0.00467  -0.0927   0.5381   0.8560
   7.250   1.2161   0.00932   0.00518  -0.0897   0.4850   0.8586
   7.500   1.2294   0.00980   0.00554  -0.0875   0.4558   0.8598
   7.750   1.2359   0.01041   0.00600  -0.0840   0.4215   0.8608
   8.000   1.2319   0.01096   0.00642  -0.0784   0.3918   0.8627
   8.250   1.2212   0.01193   0.00725  -0.0722   0.3571   0.8646
   8.500   1.2206   0.01282   0.00805  -0.0681   0.3345   0.8661
   8.750   1.2113   0.01419   0.00925  -0.0631   0.2987   0.8678
   9.000   1.2100   0.01540   0.01034  -0.0595   0.2717   0.8693
   9.250   1.2052   0.01686   0.01164  -0.0556   0.2399   0.8710
   9.500   1.2005   0.01842   0.01303  -0.0521   0.2071   0.8723
   9.750   1.1978   0.01998   0.01443  -0.0489   0.1767   0.8733
  10.000   1.1964   0.02155   0.01585  -0.0461   0.1487   0.8741
  10.250   1.1969   0.02305   0.01723  -0.0436   0.1252   0.8749
  10.500   1.1974   0.02457   0.01863  -0.0412   0.1021   0.8760
  10.750   1.2003   0.02601   0.01998  -0.0391   0.0827   0.8771
  11.000   1.2035   0.02751   0.02140  -0.0372   0.0658   0.8780
  11.250   1.2083   0.02899   0.02283  -0.0356   0.0517   0.8788
  11.500   1.2149   0.03040   0.02418  -0.0342   0.0408   0.8795
  11.750   1.2210   0.03190   0.02565  -0.0329   0.0314   0.8802
  12.000   1.2289   0.03331   0.02704  -0.0317   0.0250   0.8808
  12.250   1.2380   0.03467   0.02841  -0.0308   0.0209   0.8815
  12.500   1.2451   0.03622   0.02995  -0.0298   0.0153   0.8822
  12.750   1.2505   0.03796   0.03167  -0.0287   0.0107   0.8829
  13.000   1.2568   0.03967   0.03341  -0.0277   0.0080   0.8837
  13.250   1.2615   0.04156   0.03534  -0.0268   0.0065   0.8844
  13.500   1.2701   0.04318   0.03702  -0.0261   0.0060   0.8850
  13.750   1.2796   0.04475   0.03864  -0.0256   0.0056   0.8856
  14.000   1.2863   0.04661   0.04055  -0.0250   0.0050   0.8861
  14.250   1.2898   0.04883   0.04284  -0.0243   0.0046   0.8866
  14.500   1.2932   0.05112   0.04521  -0.0238   0.0044   0.8870
  14.750   1.2970   0.05344   0.04762  -0.0233   0.0043   0.8874
  15.000   1.3038   0.05549   0.04973  -0.0231   0.0043   0.8878
  15.250   1.3094   0.05770   0.05203  -0.0229   0.0041   0.8881
  15.500   1.3155   0.05989   0.05429  -0.0228   0.0041   0.8885
  15.750   1.3169   0.06270   0.05720  -0.0227   0.0040   0.8891
  16.000   1.3216   0.06517   0.05975  -0.0228   0.0039   0.8897
  16.250   1.3241   0.06794   0.06262  -0.0229   0.0038   0.8902
  16.500   1.3270   0.07072   0.06548  -0.0231   0.0037   0.8909
  16.750   1.3272   0.07389   0.06875  -0.0234   0.0037   0.8915
  17.000   1.3286   0.07699   0.07194  -0.0238   0.0036   0.8921
  17.250   1.3297   0.08020   0.07524  -0.0244   0.0036   0.8927
  17.500   1.3294   0.08368   0.07882  -0.0251   0.0035   0.8931
  17.750   1.3259   0.08768   0.08293  -0.0259   0.0034   0.8935
  18.000   1.3272   0.09104   0.08637  -0.0269   0.0034   0.8940
  18.250   1.3262   0.09482   0.09024  -0.0280   0.0033   0.8944
  18.500   1.3248   0.09871   0.09422  -0.0292   0.0032   0.8948
  18.750   1.3218   0.10292   0.09854  -0.0306   0.0032   0.8952
  19.000   1.3169   0.10747   0.10319  -0.0323   0.0031   0.8956
  19.250   1.3132   0.11192   0.10775  -0.0340   0.0031   0.8959
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