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AH 93-156 (ah93156-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 93-156 (ah93156-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.9 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93156-il-1000000-n5.txt
Download as CSV file: xf-ah93156-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-156                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.6207   0.08885   0.08578  -0.0934   0.7957   0.0083
 -16.750  -0.7688   0.05978   0.05632  -0.1100   0.7954   0.0077
 -16.500  -0.8215   0.04636   0.04260  -0.1199   0.7922   0.0077
 -16.000  -0.8580   0.03687   0.03277  -0.1239   0.7856   0.0078
 -15.750  -0.8688   0.03397   0.02974  -0.1235   0.7823   0.0078
 -15.500  -0.8755   0.03172   0.02736  -0.1224   0.7790   0.0079
 -15.250  -0.8804   0.02979   0.02530  -0.1207   0.7757   0.0080
 -15.000  -0.8789   0.02838   0.02379  -0.1190   0.7724   0.0081
 -14.750  -0.8770   0.02702   0.02233  -0.1171   0.7698   0.0082
 -14.500  -0.8710   0.02595   0.02116  -0.1153   0.7670   0.0083
 -14.250  -0.8643   0.02494   0.02007  -0.1134   0.7641   0.0084
 -14.000  -0.8564   0.02403   0.01907  -0.1115   0.7615   0.0085
 -13.750  -0.8487   0.02313   0.01807  -0.1094   0.7590   0.0086
 -13.500  -0.8375   0.02241   0.01728  -0.1076   0.7567   0.0088
 -13.250  -0.8260   0.02171   0.01650  -0.1058   0.7547   0.0089
 -13.000  -0.8127   0.02110   0.01584  -0.1041   0.7523   0.0091
 -12.750  -0.8020   0.02037   0.01502  -0.1019   0.7498   0.0092
 -12.500  -0.7895   0.01976   0.01432  -0.0999   0.7474   0.0094
 -12.250  -0.7765   0.01920   0.01367  -0.0979   0.7451   0.0096
 -12.000  -0.7634   0.01867   0.01305  -0.0958   0.7431   0.0097
 -11.750  -0.7483   0.01825   0.01256  -0.0939   0.7412   0.0099
 -11.500  -0.7316   0.01777   0.01201  -0.0924   0.7396   0.0100
 -11.250  -0.7127   0.01731   0.01149  -0.0912   0.7377   0.0101
 -11.000  -0.6960   0.01665   0.01076  -0.0897   0.7357   0.0105
 -10.750  -0.6762   0.01619   0.01023  -0.0886   0.7336   0.0107
 -10.500  -0.6557   0.01575   0.00975  -0.0877   0.7316   0.0111
 -10.250  -0.6345   0.01534   0.00929  -0.0868   0.7298   0.0113
 -10.000  -0.6124   0.01500   0.00889  -0.0861   0.7281   0.0117
  -9.750  -0.5902   0.01465   0.00848  -0.0853   0.7264   0.0120
  -9.500  -0.5673   0.01430   0.00809  -0.0847   0.7250   0.0123
  -9.250  -0.5441   0.01396   0.00770  -0.0841   0.7234   0.0127
  -9.000  -0.5203   0.01365   0.00735  -0.0836   0.7216   0.0130
  -8.750  -0.4972   0.01327   0.00693  -0.0830   0.7198   0.0135
  -8.500  -0.4733   0.01295   0.00659  -0.0825   0.7180   0.0141
  -8.250  -0.4490   0.01268   0.00629  -0.0821   0.7164   0.0147
  -8.000  -0.4243   0.01242   0.00600  -0.0817   0.7148   0.0154
  -7.750  -0.3996   0.01217   0.00571  -0.0813   0.7132   0.0159
  -7.500  -0.3747   0.01195   0.00543  -0.0810   0.7115   0.0164
  -7.250  -0.3499   0.01166   0.00513  -0.0806   0.7099   0.0173
  -7.000  -0.3246   0.01141   0.00488  -0.0803   0.7084   0.0182
  -6.750  -0.2990   0.01119   0.00465  -0.0801   0.7068   0.0192
  -6.500  -0.2731   0.01099   0.00443  -0.0799   0.7053   0.0200
  -6.250  -0.2473   0.01078   0.00421  -0.0797   0.7035   0.0212
  -6.000  -0.2216   0.01057   0.00399  -0.0795   0.7017   0.0228
  -5.750  -0.1956   0.01040   0.00380  -0.0793   0.7000   0.0243
  -5.500  -0.1693   0.01025   0.00362  -0.0792   0.6983   0.0254
  -5.250  -0.1434   0.01006   0.00343  -0.0790   0.6967   0.0279
  -5.000  -0.1170   0.00991   0.00327  -0.0789   0.6951   0.0302
  -4.750  -0.0904   0.00975   0.00312  -0.0788   0.6936   0.0325
  -4.500  -0.0639   0.00958   0.00298  -0.0787   0.6919   0.0358
  -4.250  -0.0370   0.00944   0.00284  -0.0787   0.6901   0.0390
  -4.000  -0.0105   0.00928   0.00271  -0.0786   0.6883   0.0445
  -3.750   0.0163   0.00915   0.00259  -0.0786   0.6864   0.0498
  -3.500   0.0430   0.00902   0.00247  -0.0785   0.6846   0.0566
  -3.250   0.0696   0.00888   0.00237  -0.0784   0.6827   0.0660
  -3.000   0.0962   0.00877   0.00227  -0.0784   0.6807   0.0767
  -2.750   0.1230   0.00861   0.00218  -0.0784   0.6789   0.0921
  -2.500   0.1498   0.00846   0.00210  -0.0784   0.6768   0.1103
  -2.250   0.1762   0.00829   0.00202  -0.0783   0.6744   0.1354
  -2.000   0.2026   0.00812   0.00195  -0.0782   0.6719   0.1648
  -1.750   0.2284   0.00793   0.00187  -0.0781   0.6690   0.2053
  -1.500   0.2531   0.00769   0.00179  -0.0777   0.6658   0.2641
  -1.250   0.2785   0.00743   0.00174  -0.0775   0.6629   0.3231
  -1.000   0.3031   0.00713   0.00169  -0.0772   0.6600   0.4008
  -0.750   0.3270   0.00679   0.00162  -0.0768   0.6569   0.4876
  -0.500   0.3461   0.00616   0.00150  -0.0754   0.6539   0.6487
  -0.250   0.3662   0.00582   0.00159  -0.0739   0.6510   0.7771
   0.000   0.3932   0.00587   0.00172  -0.0737   0.6482   0.8129
   0.250   0.4214   0.00594   0.00179  -0.0738   0.6448   0.8281
   0.500   0.4491   0.00605   0.00190  -0.0738   0.6410   0.8390
   0.750   0.4766   0.00617   0.00201  -0.0737   0.6375   0.8474
   1.000   0.5043   0.00630   0.00214  -0.0737   0.6343   0.8545
   1.250   0.5321   0.00641   0.00224  -0.0738   0.6304   0.8602
   1.500   0.5593   0.00653   0.00236  -0.0737   0.6260   0.8637
   1.750   0.5865   0.00661   0.00242  -0.0737   0.6215   0.8660
   2.000   0.6146   0.00665   0.00245  -0.0739   0.6171   0.8673
   2.250   0.6424   0.00669   0.00248  -0.0741   0.6115   0.8685
   2.500   0.6694   0.00675   0.00251  -0.0741   0.6056   0.8697
   2.750   0.6971   0.00679   0.00254  -0.0743   0.5985   0.8708
   3.000   0.7234   0.00688   0.00258  -0.0743   0.5905   0.8719
   3.250   0.7506   0.00694   0.00263  -0.0744   0.5826   0.8729
   3.500   0.7766   0.00704   0.00269  -0.0743   0.5738   0.8737
   3.750   0.8015   0.00714   0.00276  -0.0739   0.5623   0.8746
   4.000   0.8260   0.00726   0.00285  -0.0735   0.5494   0.8755
   4.250   0.8495   0.00742   0.00296  -0.0728   0.5352   0.8763
   4.500   0.8721   0.00759   0.00309  -0.0721   0.5203   0.8771
   4.750   0.8937   0.00780   0.00324  -0.0711   0.5046   0.8779
   5.000   0.9142   0.00803   0.00341  -0.0700   0.4883   0.8789
   5.250   0.9341   0.00826   0.00360  -0.0687   0.4728   0.8801
   5.500   0.9532   0.00850   0.00379  -0.0673   0.4578   0.8812
   5.750   0.9712   0.00875   0.00399  -0.0657   0.4430   0.8822
   6.000   0.9870   0.00900   0.00420  -0.0636   0.4287   0.8834
   6.250   0.9994   0.00925   0.00440  -0.0609   0.4153   0.8847
   6.500   1.0106   0.00957   0.00468  -0.0579   0.4010   0.8862
   6.750   1.0226   0.00992   0.00499  -0.0553   0.3884   0.8875
   7.000   1.0337   0.01031   0.00534  -0.0526   0.3763   0.8885
   7.500   1.0524   0.01123   0.00620  -0.0469   0.3489   0.8908
   7.750   1.0624   0.01175   0.00669  -0.0443   0.3355   0.8921
   8.000   1.0684   0.01245   0.00733  -0.0412   0.3179   0.8936
   8.250   1.0750   0.01320   0.00801  -0.0383   0.2984   0.8949
   8.500   1.0794   0.01408   0.00879  -0.0353   0.2757   0.8963
   8.750   1.0816   0.01511   0.00970  -0.0321   0.2498   0.8976
   9.000   1.0858   0.01611   0.01058  -0.0293   0.2279   0.8989
   9.250   1.0895   0.01717   0.01153  -0.0265   0.2032   0.9001
   9.500   1.0923   0.01832   0.01255  -0.0237   0.1786   0.9012
   9.750   1.0919   0.01968   0.01373  -0.0206   0.1482   0.9025
  10.000   1.1032   0.02049   0.01451  -0.0191   0.1382   0.9033
  10.250   1.1032   0.02190   0.01577  -0.0163   0.1104   0.9044
  10.500   1.1099   0.02300   0.01680  -0.0144   0.0936   0.9054
  10.750   1.1163   0.02417   0.01790  -0.0126   0.0790   0.9063
  11.000   1.1230   0.02537   0.01903  -0.0108   0.0646   0.9072
  11.250   1.1303   0.02657   0.02019  -0.0092   0.0528   0.9081
  11.500   1.1395   0.02771   0.02129  -0.0079   0.0441   0.9089
  11.750   1.1477   0.02894   0.02250  -0.0066   0.0360   0.9098
  12.000   1.1572   0.03011   0.02365  -0.0054   0.0301   0.9106
  12.250   1.1663   0.03135   0.02489  -0.0043   0.0249   0.9115
  12.500   1.1745   0.03269   0.02621  -0.0031   0.0194   0.9123
  12.750   1.1854   0.03386   0.02741  -0.0023   0.0172   0.9132
  13.000   1.1950   0.03515   0.02871  -0.0014   0.0148   0.9142
  13.250   1.2050   0.03645   0.03004  -0.0006   0.0128   0.9150
  13.500   1.2141   0.03786   0.03147   0.0002   0.0111   0.9158
  13.750   1.2239   0.03924   0.03287   0.0009   0.0098   0.9164
  14.000   1.2323   0.04075   0.03442   0.0016   0.0085   0.9170
  14.250   1.2423   0.04217   0.03588   0.0021   0.0079   0.9179
  14.500   1.2507   0.04377   0.03752   0.0026   0.0073   0.9188
  14.750   1.2590   0.04539   0.03920   0.0031   0.0065   0.9197
  15.000   1.2670   0.04708   0.04095   0.0036   0.0060   0.9205
  15.250   1.2744   0.04885   0.04276   0.0040   0.0055   0.9214
  15.500   1.2816   0.05069   0.04465   0.0043   0.0053   0.9223
  15.750   1.2876   0.05268   0.04670   0.0046   0.0050   0.9232
  16.000   1.2943   0.05464   0.04873   0.0048   0.0048   0.9242
  16.250   1.3008   0.05666   0.05081   0.0049   0.0046   0.9252
  16.500   1.3053   0.05895   0.05316   0.0050   0.0042   0.9262
  16.750   1.3099   0.06126   0.05555   0.0050   0.0041   0.9271
  17.000   1.3142   0.06365   0.05801   0.0049   0.0041   0.9281
  17.250   1.3183   0.06613   0.06055   0.0047   0.0040   0.9291
  17.500   1.3178   0.06919   0.06369   0.0044   0.0036   0.9301
  18.000   1.3221   0.07488   0.06953   0.0035   0.0036   0.9325
  18.250   1.3229   0.07797   0.07271   0.0028   0.0035   0.9338
  18.500   1.3245   0.08105   0.07588   0.0021   0.0035   0.9354
  18.750   1.3264   0.08415   0.07906   0.0012   0.0034   0.9371
  19.000   1.3253   0.08771   0.08273   0.0002   0.0034   0.9389
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