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AH 93-157 (ah93157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 93-157 (ah93157-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.24 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93157-il-1000000-n5.txt
Download as CSV file: xf-ah93157-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7928   0.05737   0.05399  -0.1140   0.8232   0.0080
 -16.750  -0.8416   0.04515   0.04143  -0.1232   0.8175   0.0079
 -16.500  -0.8570   0.04034   0.03646  -0.1258   0.8125   0.0079
 -16.250  -0.8706   0.03664   0.03260  -0.1266   0.8075   0.0079
 -16.000  -0.8757   0.03419   0.03003  -0.1263   0.8026   0.0080
 -15.750  -0.8803   0.03204   0.02775  -0.1254   0.7984   0.0081
 -15.500  -0.8795   0.03041   0.02602  -0.1242   0.7945   0.0081
 -15.250  -0.8793   0.02886   0.02435  -0.1227   0.7905   0.0082
 -15.000  -0.8742   0.02768   0.02308  -0.1211   0.7869   0.0084
 -14.750  -0.8709   0.02647   0.02175  -0.1192   0.7836   0.0084
 -14.500  -0.8619   0.02556   0.02078  -0.1177   0.7811   0.0086
 -14.250  -0.8547   0.02458   0.01971  -0.1158   0.7781   0.0087
 -14.000  -0.8470   0.02366   0.01869  -0.1138   0.7749   0.0088
 -13.750  -0.8373   0.02287   0.01781  -0.1119   0.7718   0.0090
 -13.500  -0.8290   0.02202   0.01685  -0.1098   0.7689   0.0091
 -13.250  -0.8168   0.02137   0.01612  -0.1080   0.7666   0.0092
 -13.000  -0.8044   0.02070   0.01537  -0.1061   0.7643   0.0094
 -12.750  -0.7918   0.02007   0.01467  -0.1042   0.7617   0.0095
 -12.500  -0.7780   0.01953   0.01404  -0.1024   0.7590   0.0097
 -12.250  -0.7647   0.01897   0.01341  -0.1004   0.7564   0.0098
 -12.000  -0.7541   0.01830   0.01266  -0.0979   0.7540   0.0101
 -11.500  -0.7242   0.01735   0.01159  -0.0942   0.7500   0.0105
 -11.250  -0.7052   0.01691   0.01111  -0.0930   0.7480   0.0108
 -11.000  -0.6855   0.01650   0.01064  -0.0919   0.7458   0.0110
 -10.750  -0.6655   0.01607   0.01016  -0.0908   0.7434   0.0112
 -10.500  -0.6448   0.01568   0.00971  -0.0899   0.7411   0.0115
 -10.250  -0.6239   0.01529   0.00925  -0.0889   0.7391   0.0118
 -10.000  -0.6022   0.01493   0.00882  -0.0881   0.7371   0.0121
  -9.750  -0.5800   0.01459   0.00842  -0.0873   0.7351   0.0123
  -9.500  -0.5574   0.01423   0.00802  -0.0867   0.7332   0.0126
  -9.250  -0.5352   0.01380   0.00756  -0.0859   0.7311   0.0132
  -9.000  -0.5119   0.01347   0.00721  -0.0853   0.7290   0.0136
  -8.750  -0.4881   0.01320   0.00690  -0.0848   0.7268   0.0141
  -8.500  -0.4641   0.01292   0.00658  -0.0843   0.7246   0.0146
  -8.250  -0.4401   0.01266   0.00627  -0.0838   0.7224   0.0151
  -8.000  -0.4157   0.01241   0.00597  -0.0833   0.7204   0.0155
  -7.750  -0.3915   0.01210   0.00563  -0.0829   0.7187   0.0161
  -7.500  -0.3668   0.01181   0.00534  -0.0825   0.7167   0.0168
  -7.250  -0.3417   0.01157   0.00509  -0.0821   0.7145   0.0176
  -7.000  -0.3164   0.01136   0.00485  -0.0818   0.7122   0.0184
  -6.750  -0.2909   0.01116   0.00461  -0.0816   0.7100   0.0192
  -6.500  -0.2659   0.01092   0.00435  -0.0812   0.7078   0.0202
  -6.250  -0.2405   0.01072   0.00414  -0.0809   0.7056   0.0214
  -6.000  -0.2147   0.01054   0.00394  -0.0806   0.7035   0.0226
  -5.750  -0.1885   0.01036   0.00375  -0.0805   0.7015   0.0238
  -5.500  -0.1626   0.01015   0.00356  -0.0803   0.6991   0.0256
  -5.250  -0.1365   0.00999   0.00339  -0.0801   0.6966   0.0279
  -5.000  -0.1103   0.00983   0.00322  -0.0799   0.6942   0.0301
  -4.750  -0.0843   0.00967   0.00306  -0.0797   0.6918   0.0328
  -4.500  -0.0580   0.00955   0.00291  -0.0795   0.6894   0.0355
  -4.250  -0.0315   0.00938   0.00278  -0.0794   0.6873   0.0400
  -4.000  -0.0048   0.00924   0.00266  -0.0794   0.6848   0.0444
  -3.750   0.0217   0.00910   0.00254  -0.0793   0.6820   0.0498
  -3.500   0.0482   0.00896   0.00242  -0.0791   0.6791   0.0570
  -3.250   0.0745   0.00884   0.00231  -0.0790   0.6761   0.0657
  -3.000   0.1009   0.00872   0.00221  -0.0789   0.6734   0.0758
  -2.750   0.1275   0.00856   0.00212  -0.0788   0.6709   0.0917
  -2.500   0.1540   0.00841   0.00204  -0.0787   0.6678   0.1109
  -2.250   0.1801   0.00825   0.00196  -0.0786   0.6647   0.1356
  -2.000   0.2059   0.00809   0.00189  -0.0784   0.6616   0.1670
  -1.750   0.2314   0.00792   0.00182  -0.0782   0.6584   0.2037
  -1.500   0.2570   0.00769   0.00176  -0.0780   0.6551   0.2538
  -1.250   0.2816   0.00742   0.00170  -0.0776   0.6515   0.3215
  -1.000   0.3053   0.00711   0.00164  -0.0771   0.6476   0.4043
  -0.750   0.3284   0.00681   0.00157  -0.0765   0.6437   0.4888
  -0.500   0.3486   0.00625   0.00148  -0.0753   0.6400   0.6311
  -0.250   0.3684   0.00584   0.00152  -0.0738   0.6358   0.7612
   0.000   0.3935   0.00589   0.00169  -0.0731   0.6311   0.8115
   0.250   0.4209   0.00599   0.00176  -0.0730   0.6266   0.8282
   0.500   0.4485   0.00609   0.00188  -0.0730   0.6216   0.8387
   0.750   0.4757   0.00622   0.00198  -0.0729   0.6167   0.8473
   1.000   0.5025   0.00638   0.00213  -0.0727   0.6118   0.8547
   1.250   0.5299   0.00650   0.00222  -0.0727   0.6057   0.8603
   1.500   0.5560   0.00664   0.00235  -0.0723   0.5994   0.8637
   1.750   0.5831   0.00673   0.00243  -0.0722   0.5937   0.8663
   2.000   0.6102   0.00680   0.00247  -0.0723   0.5869   0.8676
   2.250   0.6370   0.00687   0.00251  -0.0722   0.5805   0.8689
   2.500   0.6639   0.00694   0.00255  -0.0722   0.5729   0.8700
   2.750   0.6902   0.00702   0.00259  -0.0721   0.5656   0.8713
   3.000   0.7168   0.00710   0.00265  -0.0721   0.5576   0.8724
   3.250   0.7426   0.00720   0.00271  -0.0719   0.5494   0.8734
   3.500   0.7679   0.00731   0.00278  -0.0717   0.5391   0.8742
   3.750   0.7932   0.00741   0.00286  -0.0714   0.5296   0.8751
   4.000   0.8172   0.00754   0.00295  -0.0708   0.5199   0.8760
   4.250   0.8415   0.00766   0.00305  -0.0704   0.5099   0.8767
   4.500   0.8653   0.00779   0.00316  -0.0698   0.4997   0.8775
   4.750   0.8879   0.00795   0.00329  -0.0690   0.4891   0.8783
   5.000   0.9103   0.00812   0.00343  -0.0682   0.4778   0.8793
   5.250   0.9316   0.00830   0.00358  -0.0672   0.4650   0.8803
   5.500   0.9518   0.00850   0.00374  -0.0659   0.4522   0.8813
   5.750   0.9712   0.00871   0.00391  -0.0646   0.4402   0.8823
   6.000   0.9881   0.00892   0.00409  -0.0627   0.4284   0.8834
   6.250   1.0043   0.00911   0.00426  -0.0606   0.4170   0.8845
   6.500   1.0179   0.00937   0.00448  -0.0581   0.4035   0.8860
   6.750   1.0303   0.00971   0.00476  -0.0555   0.3886   0.8873
   7.000   1.0422   0.01007   0.00508  -0.0528   0.3740   0.8884
   7.250   1.0552   0.01043   0.00541  -0.0504   0.3625   0.8893
   7.500   1.0664   0.01083   0.00577  -0.0478   0.3499   0.8904
   7.750   1.0749   0.01133   0.00622  -0.0448   0.3332   0.8917
   8.000   1.0799   0.01199   0.00680  -0.0414   0.3116   0.8932
   8.250   1.0825   0.01282   0.00751  -0.0378   0.2879   0.8946
   8.500   1.0851   0.01372   0.00831  -0.0344   0.2625   0.8960
   8.750   1.0897   0.01462   0.00910  -0.0314   0.2401   0.8973
   9.000   1.0963   0.01548   0.00988  -0.0288   0.2209   0.8985
   9.250   1.1030   0.01639   0.01071  -0.0263   0.2029   0.8996
   9.500   1.1086   0.01738   0.01161  -0.0238   0.1827   0.9009
   9.750   1.1141   0.01842   0.01255  -0.0214   0.1632   0.9021
  10.000   1.1183   0.01956   0.01360  -0.0190   0.1435   0.9031
  10.250   1.1233   0.02070   0.01464  -0.0167   0.1237   0.9039
  10.500   1.1299   0.02178   0.01566  -0.0147   0.1084   0.9049
  10.750   1.1342   0.02303   0.01683  -0.0126   0.0920   0.9059
  11.000   1.1399   0.02423   0.01797  -0.0107   0.0762   0.9069
  11.250   1.1442   0.02558   0.01925  -0.0088   0.0611   0.9079
  11.500   1.1498   0.02691   0.02052  -0.0070   0.0493   0.9088
  11.750   1.1579   0.02812   0.02171  -0.0057   0.0415   0.9097
  12.000   1.1650   0.02943   0.02300  -0.0043   0.0339   0.9105
  12.250   1.1754   0.03057   0.02415  -0.0033   0.0303   0.9114
  12.500   1.1841   0.03186   0.02544  -0.0022   0.0261   0.9123
  12.750   1.1931   0.03315   0.02674  -0.0012   0.0226   0.9133
  13.000   1.2026   0.03443   0.02804  -0.0003   0.0199   0.9143
  13.250   1.2120   0.03577   0.02940   0.0006   0.0180   0.9152
  13.500   1.2209   0.03718   0.03083   0.0013   0.0156   0.9159
  13.750   1.2301   0.03861   0.03229   0.0020   0.0145   0.9166
  14.000   1.2392   0.04007   0.03379   0.0027   0.0132   0.9173
  14.500   1.2561   0.04320   0.03699   0.0038   0.0113   0.9189
  14.750   1.2637   0.04489   0.03874   0.0043   0.0104   0.9198
  15.000   1.2724   0.04652   0.04042   0.0047   0.0100   0.9207
  15.250   1.2796   0.04831   0.04226   0.0050   0.0095   0.9217
  15.500   1.2858   0.05024   0.04424   0.0054   0.0088   0.9226
  15.750   1.2913   0.05229   0.04634   0.0057   0.0083   0.9236
  16.000   1.2983   0.05422   0.04834   0.0058   0.0079   0.9246
  16.250   1.3048   0.05624   0.05042   0.0059   0.0075   0.9256
  16.500   1.3096   0.05849   0.05274   0.0059   0.0074   0.9266
  16.750   1.3139   0.06082   0.05513   0.0059   0.0070   0.9277
  17.000   1.3177   0.06327   0.05764   0.0058   0.0068   0.9287
  17.250   1.3198   0.06595   0.06037   0.0055   0.0063   0.9298
  17.500   1.3241   0.06843   0.06293   0.0053   0.0061   0.9308
  18.000   1.3294   0.07395   0.06862   0.0043   0.0058   0.9335
  18.250   1.3315   0.07686   0.07161   0.0037   0.0057   0.9350
  18.500   1.3326   0.07998   0.07481   0.0029   0.0055   0.9366
  18.750   1.3335   0.08320   0.07811   0.0020   0.0054   0.9384
  19.000   1.3338   0.08655   0.08155   0.0010   0.0052   0.9403
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