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AH 83-150 Q (ah83150q-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 83-150 Q (ah83150q-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.76 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah83150q-il-1000000-n5.txt
Download as CSV file: xf-ah83150q-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 83-150 Q                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.1838   0.10364   0.10080  -0.0438   0.6560   0.0057
 -11.000  -0.2537   0.10371   0.10066  -0.0514   0.6630   0.0048
 -10.750  -0.2521   0.09938   0.09633  -0.0535   0.6616   0.0048
 -10.500  -0.2458   0.09673   0.09368  -0.0549   0.6599   0.0046
 -10.250  -0.2466   0.09203   0.08899  -0.0571   0.6586   0.0046
 -10.000  -0.2465   0.08779   0.08475  -0.0592   0.6570   0.0046
  -9.750  -0.2490   0.08314   0.08012  -0.0618   0.6557   0.0054
  -9.250  -0.2549   0.07398   0.07099  -0.0670   0.6531   0.0045
  -9.000  -0.2211   0.05558   0.05281  -0.0649   0.6476   0.0053
  -8.500  -0.3289   0.05376   0.05071  -0.0770   0.6490   0.0052
  -8.250  -0.3363   0.04841   0.04522  -0.0764   0.6475   0.0050
  -8.000  -0.3477   0.04331   0.03993  -0.0752   0.6458   0.0051
  -7.750  -0.3484   0.03816   0.03454  -0.0736   0.6442   0.0051
  -7.500  -0.3441   0.03345   0.02957  -0.0719   0.6427   0.0050
  -7.250  -0.3391   0.02878   0.02453  -0.0699   0.6412   0.0050
  -7.000  -0.3233   0.02641   0.02190  -0.0689   0.6396   0.0050
  -6.750  -0.3123   0.02263   0.01766  -0.0672   0.6382   0.0051
  -6.500  -0.2929   0.02060   0.01538  -0.0665   0.6369   0.0052
  -6.250  -0.2702   0.01915   0.01373  -0.0660   0.6354   0.0053
  -6.000  -0.2467   0.01745   0.01175  -0.0654   0.6337   0.0051
  -5.750  -0.2214   0.01644   0.01058  -0.0651   0.6321   0.0051
  -5.500  -0.1954   0.01561   0.00961  -0.0649   0.6305   0.0051
  -5.250  -0.1695   0.01470   0.00857  -0.0647   0.6288   0.0050
  -5.000  -0.1430   0.01402   0.00778  -0.0646   0.6270   0.0050
  -4.750  -0.1168   0.01324   0.00689  -0.0644   0.6252   0.0050
  -4.500  -0.0904   0.01261   0.00617  -0.0642   0.6236   0.0050
  -4.250  -0.0640   0.01198   0.00549  -0.0641   0.6222   0.0051
  -4.000  -0.0375   0.01141   0.00487  -0.0640   0.6207   0.0051
  -3.750  -0.0108   0.01092   0.00434  -0.0639   0.6190   0.0052
  -3.500   0.0164   0.01053   0.00392  -0.0640   0.6172   0.0053
  -3.250   0.0439   0.01021   0.00357  -0.0640   0.6155   0.0054
  -3.000   0.0717   0.00995   0.00328  -0.0642   0.6138   0.0056
  -2.750   0.0997   0.00971   0.00303  -0.0643   0.6119   0.0059
  -2.500   0.1277   0.00952   0.00280  -0.0645   0.6100   0.0062
  -2.250   0.1560   0.00935   0.00261  -0.0646   0.6081   0.0068
  -2.000   0.1846   0.00919   0.00245  -0.0649   0.6066   0.0071
  -1.750   0.2131   0.00902   0.00227  -0.0652   0.6047   0.0078
  -1.500   0.2418   0.00889   0.00215  -0.0654   0.6025   0.0086
  -1.250   0.2706   0.00879   0.00203  -0.0657   0.6000   0.0098
  -1.000   0.2992   0.00868   0.00192  -0.0660   0.5975   0.0133
  -0.750   0.3267   0.00832   0.00180  -0.0663   0.5951   0.0922
  -0.500   0.3529   0.00762   0.00169  -0.0666   0.5928   0.2928
  -0.250   0.3746   0.00609   0.00166  -0.0665   0.5906   0.7542
   0.000   0.4030   0.00625   0.00187  -0.0665   0.5880   0.7930
   0.250   0.4315   0.00643   0.00205  -0.0665   0.5852   0.8073
   0.500   0.4607   0.00655   0.00212  -0.0668   0.5823   0.8138
   0.750   0.4896   0.00661   0.00214  -0.0671   0.5795   0.8167
   1.000   0.5187   0.00666   0.00218  -0.0674   0.5768   0.8186
   1.250   0.5480   0.00668   0.00219  -0.0678   0.5734   0.8196
   1.500   0.5773   0.00671   0.00220  -0.0683   0.5696   0.8203
   1.750   0.6064   0.00676   0.00221  -0.0687   0.5658   0.8212
   2.000   0.6355   0.00680   0.00223  -0.0691   0.5622   0.8221
   2.250   0.6648   0.00683   0.00225  -0.0696   0.5582   0.8229
   2.500   0.6939   0.00687   0.00228  -0.0700   0.5538   0.8236
   2.750   0.7227   0.00693   0.00231  -0.0704   0.5493   0.8243
   3.000   0.7518   0.00697   0.00235  -0.0709   0.5448   0.8252
   3.250   0.7807   0.00703   0.00240  -0.0713   0.5392   0.8261
   3.500   0.8092   0.00711   0.00245  -0.0716   0.5338   0.8269
   3.750   0.8381   0.00717   0.00251  -0.0721   0.5276   0.8276
   4.250   0.8946   0.00735   0.00265  -0.0728   0.5115   0.8289
   4.500   0.9219   0.00751   0.00275  -0.0730   0.4966   0.8294
   4.750   0.9482   0.00773   0.00289  -0.0730   0.4775   0.8301
   5.000   0.9740   0.00798   0.00306  -0.0730   0.4573   0.8308
   5.250   0.9999   0.00820   0.00323  -0.0730   0.4412   0.8316
   5.500   1.0254   0.00845   0.00342  -0.0730   0.4242   0.8322
   5.750   1.0502   0.00874   0.00365  -0.0728   0.4065   0.8329
   6.000   1.0751   0.00901   0.00387  -0.0727   0.3918   0.8335
   6.250   1.0995   0.00929   0.00411  -0.0725   0.3768   0.8341
   6.500   1.1227   0.00964   0.00440  -0.0721   0.3588   0.8348
   6.750   1.1452   0.01001   0.00470  -0.0716   0.3412   0.8355
   7.000   1.1677   0.01035   0.00499  -0.0711   0.3261   0.8364
   7.250   1.1890   0.01074   0.00533  -0.0704   0.3097   0.8373
   7.500   1.2087   0.01117   0.00570  -0.0695   0.2908   0.8382
   7.750   1.2248   0.01174   0.00615  -0.0681   0.2675   0.8391
   8.000   1.2357   0.01246   0.00673  -0.0658   0.2382   0.8401
   8.250   1.2390   0.01321   0.00735  -0.0622   0.2111   0.8413
   8.500   1.2384   0.01414   0.00816  -0.0581   0.1876   0.8426
   8.750   1.2452   0.01494   0.00892  -0.0556   0.1744   0.8437
   9.000   1.2522   0.01587   0.00980  -0.0534   0.1614   0.8446
   9.250   1.2597   0.01688   0.01078  -0.0515   0.1494   0.8457
   9.500   1.2687   0.01786   0.01174  -0.0498   0.1394   0.8469
   9.750   1.2786   0.01886   0.01274  -0.0484   0.1307   0.8479
  10.000   1.2875   0.01996   0.01382  -0.0470   0.1224   0.8489
  10.250   1.2963   0.02110   0.01495  -0.0456   0.1135   0.8498
  10.500   1.3070   0.02215   0.01601  -0.0444   0.1073   0.8507
  10.750   1.3132   0.02352   0.01734  -0.0430   0.0968   0.8517
  11.000   1.3229   0.02468   0.01851  -0.0419   0.0896   0.8526
  11.250   1.3291   0.02611   0.01990  -0.0406   0.0795   0.8536
  11.500   1.3385   0.02734   0.02114  -0.0396   0.0748   0.8545
  11.750   1.3463   0.02871   0.02250  -0.0385   0.0671   0.8554
  12.000   1.3489   0.03049   0.02422  -0.0372   0.0558   0.8563
  12.250   1.3551   0.03203   0.02576  -0.0361   0.0494   0.8573
  12.500   1.3622   0.03356   0.02729  -0.0352   0.0446   0.8583
  12.750   1.3697   0.03512   0.02886  -0.0345   0.0402   0.8591
  13.000   1.3766   0.03675   0.03050  -0.0337   0.0363   0.8598
  13.250   1.3854   0.03829   0.03208  -0.0332   0.0339   0.8606
  13.500   1.3941   0.03984   0.03366  -0.0327   0.0315   0.8615
  13.750   1.4017   0.04154   0.03539  -0.0321   0.0295   0.8624
  14.000   1.4097   0.04323   0.03713  -0.0317   0.0274   0.8632
  14.250   1.4175   0.04497   0.03891  -0.0313   0.0255   0.8641
  14.500   1.4236   0.04693   0.04089  -0.0310   0.0233   0.8650
  14.750   1.4316   0.04874   0.04276  -0.0307   0.0222   0.8659
  15.000   1.4393   0.05061   0.04468  -0.0306   0.0208   0.8667
  15.250   1.4446   0.05275   0.04685  -0.0304   0.0186   0.8676
  15.500   1.4503   0.05494   0.04908  -0.0303   0.0169   0.8685
  15.750   1.4565   0.05709   0.05128  -0.0303   0.0153   0.8694
  16.000   1.4595   0.05963   0.05387  -0.0304   0.0128   0.8703
  16.250   1.4592   0.06261   0.05685  -0.0305   0.0089   0.8712
  16.500   1.4579   0.06580   0.06007  -0.0307   0.0059   0.8720
  16.750   1.4560   0.06917   0.06349  -0.0310   0.0042   0.8727
  17.000   1.4555   0.07242   0.06681  -0.0315   0.0034   0.8734
  17.250   1.4567   0.07551   0.06997  -0.0320   0.0029   0.8741
  17.750   1.4596   0.08181   0.07645  -0.0334   0.0026   0.8759
  18.000   1.4597   0.08522   0.07995  -0.0343   0.0024   0.8770
  18.250   1.4581   0.08892   0.08374  -0.0352   0.0023   0.8780
  18.500   1.4553   0.09287   0.08780  -0.0364   0.0021   0.8791
  18.750   1.4547   0.09658   0.09160  -0.0376   0.0020   0.8802
  19.000   1.4540   0.10031   0.09543  -0.0389   0.0020   0.8814
  19.250   1.4517   0.10436   0.09958  -0.0404   0.0018   0.8825
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