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AH 93-157 (ah93157-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 93-157 (ah93157-il)
Reynolds number: 500,000
Max Cl/Cd: 91.96 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93157-il-500000-n5.txt
Download as CSV file: xf-ah93157-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-157                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.6057   0.05348   0.04973  -0.1179   0.8253   0.0112
 -14.500  -0.6357   0.04544   0.04143  -0.1236   0.8198   0.0113
 -14.250  -0.6564   0.04072   0.03648  -0.1253   0.8149   0.0113
 -14.000  -0.6696   0.03750   0.03308  -0.1251   0.8105   0.0114
 -13.750  -0.6774   0.03509   0.03050  -0.1241   0.8064   0.0116
 -13.500  -0.6851   0.03288   0.02809  -0.1223   0.8025   0.0116
 -13.250  -0.6868   0.03121   0.02624  -0.1203   0.7990   0.0118
 -13.000  -0.6876   0.02960   0.02446  -0.1181   0.7953   0.0120
 -12.750  -0.6864   0.02817   0.02286  -0.1158   0.7918   0.0121
 -12.500  -0.6827   0.02692   0.02143  -0.1135   0.7885   0.0122
 -12.250  -0.6759   0.02587   0.02021  -0.1113   0.7857   0.0124
 -12.000  -0.6703   0.02476   0.01897  -0.1088   0.7830   0.0126
 -11.750  -0.6626   0.02382   0.01794  -0.1065   0.7801   0.0128
 -11.500  -0.6536   0.02296   0.01699  -0.1041   0.7770   0.0130
 -11.250  -0.6417   0.02233   0.01628  -0.1020   0.7741   0.0132
 -11.000  -0.6295   0.02174   0.01560  -0.0999   0.7716   0.0135
 -10.750  -0.6156   0.02115   0.01491  -0.0980   0.7694   0.0138
 -10.500  -0.5991   0.02056   0.01420  -0.0965   0.7673   0.0141
 -10.250  -0.5818   0.01991   0.01346  -0.0952   0.7649   0.0145
 -10.000  -0.5626   0.01938   0.01283  -0.0940   0.7624   0.0150
  -9.750  -0.5431   0.01883   0.01217  -0.0929   0.7598   0.0155
  -9.500  -0.5242   0.01822   0.01148  -0.0918   0.7575   0.0159
  -9.250  -0.5042   0.01769   0.01090  -0.0908   0.7554   0.0165
  -9.000  -0.4831   0.01724   0.01037  -0.0899   0.7534   0.0169
  -8.750  -0.4615   0.01680   0.00986  -0.0891   0.7512   0.0174
  -8.500  -0.4393   0.01638   0.00939  -0.0884   0.7490   0.0181
  -8.250  -0.4170   0.01595   0.00889  -0.0876   0.7466   0.0186
  -8.000  -0.3939   0.01558   0.00845  -0.0870   0.7443   0.0193
  -7.750  -0.3719   0.01511   0.00795  -0.0862   0.7420   0.0201
  -7.500  -0.3485   0.01477   0.00758  -0.0856   0.7397   0.0210
  -7.250  -0.3246   0.01447   0.00722  -0.0851   0.7377   0.0221
  -7.000  -0.3007   0.01415   0.00683  -0.0846   0.7358   0.0229
  -6.750  -0.2769   0.01382   0.00646  -0.0841   0.7336   0.0239
  -6.500  -0.2531   0.01348   0.00613  -0.0835   0.7312   0.0252
  -6.250  -0.2284   0.01323   0.00585  -0.0831   0.7288   0.0268
  -6.000  -0.2035   0.01299   0.00557  -0.0828   0.7265   0.0284
  -5.750  -0.1792   0.01269   0.00526  -0.0823   0.7242   0.0304
  -5.500  -0.1541   0.01246   0.00500  -0.0819   0.7221   0.0326
  -5.250  -0.1286   0.01228   0.00475  -0.0816   0.7200   0.0348
  -5.000  -0.1038   0.01202   0.00454  -0.0813   0.7177   0.0382
  -4.750  -0.0783   0.01184   0.00434  -0.0810   0.7151   0.0417
  -4.500  -0.0532   0.01162   0.00415  -0.0806   0.7125   0.0463
  -4.250  -0.0274   0.01145   0.00396  -0.0804   0.7100   0.0512
  -4.000  -0.0019   0.01125   0.00378  -0.0801   0.7077   0.0587
  -3.750   0.0238   0.01108   0.00361  -0.0799   0.7055   0.0672
  -3.500   0.0494   0.01091   0.00347  -0.0796   0.7031   0.0784
  -3.250   0.0748   0.01072   0.00335  -0.0793   0.7004   0.0936
  -3.000   0.1002   0.01053   0.00324  -0.0791   0.6975   0.1143
  -2.750   0.1253   0.01031   0.00311  -0.0788   0.6947   0.1415
  -2.500   0.1502   0.01009   0.00299  -0.0784   0.6919   0.1774
  -2.250   0.1748   0.00983   0.00287  -0.0780   0.6893   0.2246
  -2.000   0.1981   0.00951   0.00279  -0.0775   0.6863   0.2910
  -1.750   0.2205   0.00913   0.00271  -0.0768   0.6832   0.3758
  -1.500   0.2407   0.00862   0.00259  -0.0757   0.6800   0.4882
  -1.250   0.2564   0.00789   0.00246  -0.0736   0.6770   0.6548
  -1.000   0.2758   0.00777   0.00278  -0.0714   0.6742   0.7776
  -0.750   0.3016   0.00794   0.00300  -0.0707   0.6708   0.8106
  -0.500   0.3283   0.00806   0.00310  -0.0705   0.6670   0.8293
  -0.250   0.3548   0.00821   0.00322  -0.0701   0.6634   0.8422
   0.000   0.3809   0.00842   0.00339  -0.0695   0.6600   0.8511
   0.250   0.4065   0.00861   0.00357  -0.0689   0.6561   0.8613
   0.500   0.4311   0.00885   0.00381  -0.0680   0.6519   0.8692
   0.750   0.4562   0.00899   0.00393  -0.0673   0.6477   0.8764
   1.000   0.4812   0.00911   0.00401  -0.0665   0.6437   0.8803
   1.250   0.5076   0.00914   0.00404  -0.0664   0.6389   0.8825
   1.500   0.5343   0.00915   0.00403  -0.0663   0.6339   0.8843
   1.750   0.5612   0.00917   0.00400  -0.0664   0.6294   0.8861
   2.000   0.5882   0.00918   0.00400  -0.0664   0.6243   0.8877
   2.250   0.6150   0.00920   0.00400  -0.0665   0.6183   0.8893
   2.500   0.6408   0.00923   0.00398  -0.0663   0.6129   0.8903
   2.750   0.6667   0.00924   0.00401  -0.0661   0.6069   0.8913
   3.000   0.6919   0.00928   0.00404  -0.0657   0.6006   0.8924
   3.250   0.7172   0.00933   0.00408  -0.0654   0.5943   0.8935
   3.500   0.7423   0.00938   0.00412  -0.0651   0.5870   0.8946
   3.750   0.7672   0.00944   0.00416  -0.0647   0.5801   0.8957
   4.000   0.7917   0.00951   0.00423  -0.0643   0.5722   0.8970
   4.250   0.8156   0.00960   0.00429  -0.0638   0.5641   0.8984
   4.500   0.8391   0.00969   0.00437  -0.0632   0.5550   0.8997
   4.750   0.8627   0.00979   0.00447  -0.0626   0.5461   0.9009
   5.000   0.8848   0.00992   0.00457  -0.0618   0.5365   0.9021
   5.250   0.9074   0.01005   0.00469  -0.0611   0.5266   0.9034
   5.500   0.9280   0.01018   0.00481  -0.0600   0.5169   0.9045
   6.000   0.9647   0.01049   0.00510  -0.0568   0.4952   0.9066
   6.250   0.9791   0.01066   0.00525  -0.0544   0.4836   0.9079
   6.500   0.9920   0.01087   0.00545  -0.0518   0.4721   0.9095
   6.750   1.0038   0.01116   0.00571  -0.0491   0.4596   0.9115
   7.000   1.0179   0.01145   0.00599  -0.0469   0.4480   0.9130
   7.250   1.0310   0.01178   0.00631  -0.0446   0.4364   0.9144
   7.500   1.0417   0.01220   0.00671  -0.0420   0.4227   0.9160
   7.750   1.0514   0.01269   0.00716  -0.0393   0.4084   0.9174
   8.000   1.0602   0.01319   0.00764  -0.0366   0.3951   0.9192
   8.250   1.0689   0.01375   0.00818  -0.0339   0.3820   0.9208
   8.500   1.0786   0.01434   0.00876  -0.0315   0.3688   0.9223
   8.750   1.0853   0.01509   0.00946  -0.0288   0.3524   0.9240
   9.000   1.0881   0.01605   0.01034  -0.0257   0.3288   0.9258
   9.250   1.0892   0.01717   0.01134  -0.0226   0.3048   0.9277
   9.500   1.0938   0.01820   0.01229  -0.0201   0.2831   0.9295
   9.750   1.0996   0.01923   0.01324  -0.0178   0.2643   0.9313
  10.000   1.1043   0.02035   0.01429  -0.0155   0.2445   0.9328
  10.250   1.1113   0.02140   0.01528  -0.0136   0.2263   0.9343
  10.500   1.1166   0.02258   0.01639  -0.0116   0.2062   0.9359
  10.750   1.1209   0.02389   0.01762  -0.0096   0.1859   0.9376
  11.000   1.1259   0.02521   0.01885  -0.0078   0.1649   0.9393
  11.250   1.1292   0.02669   0.02025  -0.0060   0.1438   0.9410
  11.500   1.1344   0.02819   0.02166  -0.0046   0.1240   0.9426
  11.750   1.1374   0.02988   0.02325  -0.0031   0.1033   0.9443
  12.000   1.1437   0.03150   0.02480  -0.0021   0.0862   0.9460
  12.250   1.1488   0.03337   0.02660  -0.0014   0.0687   0.9481
  12.500   1.1560   0.03520   0.02837  -0.0010   0.0547   0.9502
  12.750   1.1640   0.03706   0.03020  -0.0007   0.0440   0.9523
  13.000   1.1737   0.03884   0.03199  -0.0007   0.0372   0.9543
  13.250   1.1835   0.04069   0.03386  -0.0008   0.0316   0.9563
  13.500   1.1949   0.04252   0.03572  -0.0012   0.0277   0.9584
  13.750   1.2066   0.04446   0.03771  -0.0019   0.0241   0.9612
  14.000   1.2176   0.04657   0.03986  -0.0027   0.0215   0.9640
  14.250   1.2294   0.04856   0.04192  -0.0034   0.0193   0.9671
  14.500   1.2371   0.05070   0.04412  -0.0038   0.0175   0.9773
  14.750   1.2403   0.05265   0.04612  -0.0028   0.0163   1.0000
  15.000   1.2463   0.05475   0.04828  -0.0026   0.0153   1.0000
  15.250   1.2505   0.05707   0.05066  -0.0024   0.0144   1.0000
  15.500   1.2537   0.05952   0.05317  -0.0023   0.0135   1.0000
  15.750   1.2585   0.06184   0.05556  -0.0023   0.0126   1.0000
  16.000   1.2616   0.06442   0.05822  -0.0023   0.0121   1.0000
  16.250   1.2647   0.06701   0.06087  -0.0024   0.0114   1.0000
  16.500   1.2653   0.06995   0.06388  -0.0026   0.0109   1.0000
  16.750   1.2663   0.07289   0.06691  -0.0029   0.0105   1.0000
  17.000   1.2680   0.07580   0.06990  -0.0033   0.0101   1.0000
  17.250   1.2687   0.07888   0.07307  -0.0038   0.0098   1.0000
  17.500   1.2689   0.08209   0.07637  -0.0044   0.0094   1.0000
  17.750   1.2684   0.08542   0.07978  -0.0051   0.0091   1.0000
  18.000   1.2667   0.08896   0.08341  -0.0059   0.0089   1.0000
  18.250   1.2638   0.09270   0.08723  -0.0068   0.0087   1.0000
  18.500   1.2589   0.09682   0.09145  -0.0079   0.0084   1.0000
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