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AH 93-157 (ah93157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 93-157 (ah93157-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.6 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah93157-il-1000000.txt
Download as CSV file: xf-ah93157-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.6515   0.05018   0.04711  -0.1225   0.8423   0.0112
 -15.000  -0.6746   0.04346   0.04016  -0.1273   0.8354   0.0112
 -14.750  -0.6923   0.03904   0.03555  -0.1290   0.8295   0.0112
 -14.500  -0.6999   0.03628   0.03265  -0.1290   0.8244   0.0114
 -14.250  -0.7089   0.03379   0.02999  -0.1280   0.8193   0.0115
 -14.000  -0.7160   0.03165   0.02768  -0.1264   0.8146   0.0115
 -13.750  -0.7167   0.03009   0.02600  -0.1247   0.8108   0.0118
 -13.500  -0.7214   0.02830   0.02405  -0.1222   0.8069   0.0118
 -13.250  -0.7172   0.02719   0.02281  -0.1201   0.8033   0.0120
 -13.000  -0.7133   0.02607   0.02154  -0.1179   0.7994   0.0121
 -12.750  -0.7077   0.02503   0.02040  -0.1156   0.7966   0.0122
 -12.500  -0.7007   0.02409   0.01934  -0.1133   0.7934   0.0123
 -12.250  -0.6893   0.02349   0.01865  -0.1114   0.7905   0.0125
 -12.000  -0.6958   0.02152   0.01646  -0.1072   0.7874   0.0128
 -11.750  -0.6887   0.02061   0.01543  -0.1045   0.7842   0.0130
 -11.500  -0.6773   0.02002   0.01480  -0.1022   0.7819   0.0133
 -11.250  -0.6641   0.01957   0.01431  -0.1000   0.7794   0.0136
 -11.000  -0.6480   0.01922   0.01391  -0.0983   0.7769   0.0140
 -10.750  -0.6309   0.01867   0.01329  -0.0969   0.7744   0.0142
 -10.500  -0.6130   0.01812   0.01265  -0.0955   0.7721   0.0146
 -10.250  -0.5946   0.01756   0.01198  -0.0942   0.7696   0.0149
 -10.000  -0.5741   0.01715   0.01148  -0.0932   0.7671   0.0153
  -9.750  -0.5527   0.01676   0.01103  -0.0924   0.7653   0.0156
  -9.500  -0.5367   0.01574   0.00991  -0.0907   0.7630   0.0161
  -9.250  -0.5165   0.01519   0.00932  -0.0897   0.7607   0.0167
  -9.000  -0.4943   0.01479   0.00889  -0.0890   0.7585   0.0171
  -8.750  -0.4713   0.01446   0.00852  -0.0883   0.7563   0.0176
  -8.500  -0.4480   0.01414   0.00813  -0.0877   0.7540   0.0183
  -8.250  -0.4240   0.01390   0.00782  -0.0872   0.7515   0.0189
  -8.000  -0.3993   0.01365   0.00754  -0.0868   0.7499   0.0193
  -7.750  -0.3798   0.01290   0.00674  -0.0856   0.7478   0.0203
  -7.500  -0.3559   0.01257   0.00640  -0.0851   0.7456   0.0211
  -7.250  -0.3311   0.01231   0.00612  -0.0847   0.7434   0.0221
  -7.000  -0.3063   0.01204   0.00581  -0.0843   0.7413   0.0229
  -6.750  -0.2811   0.01182   0.00554  -0.0839   0.7391   0.0237
  -6.500  -0.2580   0.01142   0.00511  -0.0833   0.7366   0.0254
  -6.250  -0.2325   0.01121   0.00489  -0.0830   0.7346   0.0268
  -6.000  -0.2069   0.01100   0.00466  -0.0827   0.7326   0.0281
  -5.750  -0.1823   0.01068   0.00433  -0.0822   0.7304   0.0300
  -5.500  -0.1569   0.01044   0.00410  -0.0819   0.7281   0.0323
  -5.250  -0.1306   0.01029   0.00392  -0.0817   0.7259   0.0345
  -5.000  -0.1054   0.01003   0.00366  -0.0814   0.7237   0.0383
  -4.750  -0.0790   0.00990   0.00350  -0.0812   0.7212   0.0416
  -4.500  -0.0534   0.00969   0.00331  -0.0810   0.7190   0.0469
  -4.250  -0.0271   0.00952   0.00316  -0.0808   0.7169   0.0523
  -4.000  -0.0011   0.00933   0.00301  -0.0806   0.7145   0.0604
  -3.750   0.0249   0.00913   0.00286  -0.0804   0.7120   0.0712
  -3.500   0.0510   0.00895   0.00272  -0.0802   0.7095   0.0856
  -3.250   0.0768   0.00876   0.00259  -0.0800   0.7069   0.1076
  -3.000   0.1026   0.00858   0.00250  -0.0798   0.7041   0.1359
  -2.750   0.1276   0.00832   0.00240  -0.0795   0.7020   0.1777
  -2.500   0.1519   0.00801   0.00230  -0.0791   0.6992   0.2351
  -2.250   0.1753   0.00764   0.00220  -0.0785   0.6965   0.3144
  -2.000   0.1977   0.00721   0.00209  -0.0778   0.6938   0.4138
  -1.750   0.2173   0.00664   0.00195  -0.0766   0.6909   0.5516
  -1.500   0.2326   0.00593   0.00189  -0.0742   0.6880   0.7392
  -1.250   0.2570   0.00593   0.00211  -0.0733   0.6851   0.8083
  -1.000   0.2848   0.00601   0.00218  -0.0733   0.6819   0.8289
  -0.750   0.3127   0.00613   0.00228  -0.0732   0.6787   0.8388
  -0.500   0.3408   0.00626   0.00235  -0.0732   0.6755   0.8463
  -0.250   0.3686   0.00641   0.00250  -0.0731   0.6723   0.8522
   0.000   0.3964   0.00653   0.00259  -0.0731   0.6687   0.8592
   0.250   0.4236   0.00665   0.00273  -0.0729   0.6649   0.8631
   0.500   0.4504   0.00684   0.00290  -0.0725   0.6612   0.8684
   0.750   0.4774   0.00705   0.00307  -0.0722   0.6576   0.8754
   1.000   0.5021   0.00721   0.00328  -0.0713   0.6537   0.8800
   1.250   0.5278   0.00736   0.00343  -0.0707   0.6493   0.8851
   1.500   0.5546   0.00750   0.00352  -0.0705   0.6449   0.8901
   1.750   0.5791   0.00752   0.00355  -0.0697   0.6406   0.8927
   2.000   0.6057   0.00752   0.00356  -0.0696   0.6359   0.8942
   2.250   0.6325   0.00754   0.00355  -0.0695   0.6310   0.8954
   2.500   0.6593   0.00756   0.00355  -0.0695   0.6261   0.8968
   2.750   0.6865   0.00756   0.00356  -0.0696   0.6206   0.8982
   3.000   0.7132   0.00760   0.00357  -0.0696   0.6151   0.8995
   3.250   0.7404   0.00762   0.00359  -0.0697   0.6093   0.9008
   3.500   0.7673   0.00766   0.00362  -0.0698   0.6025   0.9022
   3.750   0.7941   0.00773   0.00366  -0.0699   0.5960   0.9032
   4.000   0.8206   0.00776   0.00369  -0.0699   0.5887   0.9042
   4.250   0.8444   0.00777   0.00368  -0.0692   0.5818   0.9054
   4.500   0.8695   0.00779   0.00371  -0.0689   0.5739   0.9063
   4.750   0.8935   0.00786   0.00376  -0.0684   0.5659   0.9073
   5.000   0.9179   0.00792   0.00382  -0.0679   0.5571   0.9082
   5.250   0.9411   0.00802   0.00390  -0.0673   0.5476   0.9094
   5.750   0.9865   0.00824   0.00409  -0.0658   0.5270   0.9118
   6.000   1.0085   0.00837   0.00420  -0.0649   0.5168   0.9129
   6.250   1.0287   0.00853   0.00434  -0.0637   0.5055   0.9140
   6.500   1.0478   0.00871   0.00449  -0.0623   0.4922   0.9154
   6.750   1.0648   0.00890   0.00464  -0.0605   0.4781   0.9167
   7.000   1.0801   0.00908   0.00481  -0.0583   0.4653   0.9176
   7.250   1.0932   0.00925   0.00495  -0.0558   0.4531   0.9189
   7.500   1.1050   0.00950   0.00517  -0.0530   0.4402   0.9204
   7.750   1.1109   0.00990   0.00550  -0.0491   0.4193   0.9223
   8.000   1.1143   0.01041   0.00592  -0.0451   0.3986   0.9243
   8.250   1.1215   0.01091   0.00636  -0.0419   0.3799   0.9259
   8.500   1.1271   0.01151   0.00689  -0.0385   0.3593   0.9275
   8.750   1.1331   0.01217   0.00749  -0.0354   0.3406   0.9291
   9.000   1.1382   0.01293   0.00816  -0.0324   0.3221   0.9307
   9.250   1.1471   0.01359   0.00878  -0.0300   0.3072   0.9321
   9.500   1.1533   0.01435   0.00949  -0.0272   0.2896   0.9337
   9.750   1.1602   0.01516   0.01023  -0.0247   0.2718   0.9352
  10.000   1.1670   0.01601   0.01103  -0.0223   0.2543   0.9368
  10.250   1.1739   0.01691   0.01187  -0.0200   0.2370   0.9383
  10.500   1.1789   0.01794   0.01282  -0.0176   0.2182   0.9399
  10.750   1.1829   0.01905   0.01384  -0.0151   0.1983   0.9418
  11.000   1.1859   0.02026   0.01495  -0.0127   0.1764   0.9434
  11.250   1.1887   0.02155   0.01613  -0.0103   0.1556   0.9448
  11.500   1.1912   0.02296   0.01744  -0.0082   0.1331   0.9467
  11.750   1.1948   0.02437   0.01876  -0.0064   0.1140   0.9486
  12.000   1.1951   0.02608   0.02034  -0.0043   0.0911   0.9507
  12.250   1.1995   0.02763   0.02182  -0.0029   0.0737   0.9526
  12.500   1.2021   0.02941   0.02352  -0.0015   0.0575   0.9547
  12.750   1.2085   0.03106   0.02512  -0.0006   0.0452   0.9567
  13.000   1.2168   0.03279   0.02682  -0.0003   0.0362   0.9591
  13.250   1.2287   0.03444   0.02848  -0.0005   0.0302   0.9616
  13.500   1.2410   0.03625   0.03028  -0.0011   0.0248   0.9639
  13.750   1.2540   0.03818   0.03222  -0.0019   0.0212   0.9658
  14.000   1.2698   0.03992   0.03401  -0.0031   0.0189   0.9673
  14.250   1.2821   0.04201   0.03614  -0.0041   0.0168   0.9687
  14.500   1.2971   0.04387   0.03805  -0.0052   0.0154   0.9700
  15.000   1.3203   0.04827   0.04255  -0.0074   0.0131   0.9801
  15.250   1.3273   0.05031   0.04465  -0.0071   0.0124   1.0000
  15.500   1.3321   0.05247   0.04686  -0.0067   0.0118   1.0000
  15.750   1.3330   0.05504   0.04949  -0.0063   0.0111   1.0000
  16.000   1.3361   0.05746   0.05197  -0.0061   0.0105   1.0000
  16.250   1.3418   0.05960   0.05417  -0.0060   0.0102   1.0000
  16.500   1.3441   0.06214   0.05678  -0.0058   0.0098   1.0000
  16.750   1.3459   0.06477   0.05948  -0.0058   0.0095   1.0000
  17.000   1.3475   0.06746   0.06224  -0.0058   0.0092   1.0000
  17.250   1.3467   0.07047   0.06530  -0.0059   0.0088   1.0000
  17.500   1.3378   0.07445   0.06938  -0.0060   0.0084   1.0000
  17.750   1.3363   0.07766   0.07267  -0.0063   0.0083   1.0000
  18.000   1.3359   0.08077   0.07586  -0.0066   0.0082   1.0000
  18.250   1.3335   0.08419   0.07937  -0.0071   0.0080   1.0000
  18.500   1.3321   0.08752   0.08277  -0.0076   0.0078   1.0000
  18.750   1.3297   0.09099   0.08633  -0.0083   0.0077   1.0000
  19.000   1.3258   0.09475   0.09017  -0.0091   0.0074   1.0000
  19.250   1.3240   0.09825   0.09375  -0.0100   0.0073   1.0000
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