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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 500,000
Max Cl/Cd: 95.23 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94156-il-500000-n5.txt
Download as CSV file: xf-ah94156-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-156                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5038   0.05373   0.05022  -0.1036   0.7867   0.0083
 -12.500  -0.5442   0.04553   0.04174  -0.1082   0.7831   0.0083
 -12.250  -0.5686   0.04115   0.03714  -0.1083   0.7798   0.0083
 -12.000  -0.5878   0.03778   0.03352  -0.1067   0.7769   0.0083
 -11.750  -0.6006   0.03511   0.03061  -0.1045   0.7743   0.0083
 -11.500  -0.6107   0.03269   0.02797  -0.1018   0.7714   0.0084
 -11.250  -0.6198   0.03047   0.02553  -0.0986   0.7686   0.0085
 -11.000  -0.6197   0.02907   0.02400  -0.0958   0.7659   0.0087
 -10.750  -0.6166   0.02792   0.02270  -0.0930   0.7633   0.0088
 -10.500  -0.6112   0.02667   0.02123  -0.0904   0.7610   0.0088
 -10.250  -0.5973   0.02596   0.02046  -0.0889   0.7588   0.0091
 -10.000  -0.5841   0.02486   0.01920  -0.0874   0.7566   0.0092
  -9.750  -0.5694   0.02377   0.01796  -0.0860   0.7545   0.0093
  -9.500  -0.5526   0.02282   0.01685  -0.0848   0.7523   0.0096
  -9.250  -0.5349   0.02181   0.01568  -0.0837   0.7502   0.0098
  -9.000  -0.5157   0.02094   0.01464  -0.0827   0.7482   0.0101
  -8.750  -0.4950   0.02023   0.01376  -0.0819   0.7463   0.0105
  -8.500  -0.4740   0.01942   0.01279  -0.0812   0.7445   0.0108
  -8.250  -0.4516   0.01879   0.01204  -0.0806   0.7427   0.0111
  -8.000  -0.4308   0.01786   0.01102  -0.0798   0.7408   0.0114
  -7.750  -0.4085   0.01723   0.01034  -0.0793   0.7387   0.0118
  -7.500  -0.3855   0.01669   0.00974  -0.0788   0.7367   0.0121
  -7.250  -0.3619   0.01620   0.00918  -0.0783   0.7347   0.0125
  -7.000  -0.3383   0.01573   0.00863  -0.0779   0.7329   0.0130
  -6.750  -0.3144   0.01526   0.00809  -0.0774   0.7314   0.0135
  -6.500  -0.2904   0.01483   0.00757  -0.0770   0.7298   0.0139
  -6.250  -0.2660   0.01441   0.00710  -0.0766   0.7280   0.0144
  -6.000  -0.2422   0.01396   0.00664  -0.0763   0.7260   0.0153
  -5.750  -0.2172   0.01363   0.00630  -0.0760   0.7239   0.0162
  -5.500  -0.1920   0.01332   0.00595  -0.0758   0.7219   0.0172
  -5.250  -0.1667   0.01301   0.00559  -0.0755   0.7202   0.0181
  -5.000  -0.1417   0.01267   0.00521  -0.0752   0.7185   0.0193
  -4.750  -0.1162   0.01240   0.00491  -0.0750   0.7167   0.0207
  -4.250  -0.0643   0.01192   0.00439  -0.0747   0.7131   0.0252
  -4.000  -0.0380   0.01172   0.00419  -0.0747   0.7111   0.0287
  -3.750  -0.0119   0.01148   0.00398  -0.0746   0.7089   0.0335
  -3.500   0.0144   0.01128   0.00378  -0.0745   0.7069   0.0408
  -3.250   0.0406   0.01106   0.00360  -0.0744   0.7049   0.0537
  -3.000   0.0665   0.01081   0.00343  -0.0743   0.7030   0.0759
  -2.750   0.0920   0.01052   0.00326  -0.0742   0.7012   0.1157
  -2.500   0.1167   0.01017   0.00312  -0.0740   0.6995   0.1776
  -2.250   0.1405   0.00974   0.00301  -0.0737   0.6972   0.2615
  -2.000   0.1632   0.00921   0.00288  -0.0733   0.6947   0.3727
  -1.750   0.1847   0.00860   0.00274  -0.0726   0.6921   0.5045
  -1.500   0.2043   0.00792   0.00262  -0.0714   0.6898   0.6560
  -1.250   0.2241   0.00801   0.00320  -0.0690   0.6876   0.7829
  -1.000   0.2525   0.00818   0.00328  -0.0691   0.6853   0.8109
  -0.750   0.2801   0.00832   0.00341  -0.0690   0.6824   0.8222
  -0.500   0.3077   0.00845   0.00351  -0.0690   0.6790   0.8312
  -0.250   0.3349   0.00861   0.00364  -0.0688   0.6758   0.8393
   0.000   0.3622   0.00873   0.00372  -0.0687   0.6730   0.8456
   0.250   0.3892   0.00888   0.00382  -0.0683   0.6705   0.8504
   0.500   0.4164   0.00897   0.00391  -0.0683   0.6670   0.8558
   0.750   0.4436   0.00902   0.00395  -0.0683   0.6634   0.8596
   1.000   0.4702   0.00909   0.00401  -0.0681   0.6601   0.8622
   1.250   0.4974   0.00914   0.00402  -0.0680   0.6570   0.8649
   1.500   0.5248   0.00918   0.00405  -0.0681   0.6535   0.8674
   1.750   0.5526   0.00920   0.00407  -0.0683   0.6495   0.8697
   2.000   0.5808   0.00922   0.00407  -0.0687   0.6455   0.8717
   2.250   0.6090   0.00923   0.00405  -0.0690   0.6420   0.8733
   2.500   0.6360   0.00924   0.00408  -0.0691   0.6380   0.8742
   2.750   0.6628   0.00925   0.00410  -0.0691   0.6329   0.8753
   3.000   0.6898   0.00927   0.00410  -0.0691   0.6280   0.8762
   3.250   0.7167   0.00930   0.00415  -0.0692   0.6227   0.8773
   3.500   0.7435   0.00933   0.00418  -0.0693   0.6168   0.8783
   3.750   0.7702   0.00937   0.00420  -0.0693   0.6112   0.8792
   4.000   0.7967   0.00941   0.00427  -0.0694   0.6039   0.8802
   4.250   0.8226   0.00947   0.00431  -0.0693   0.5963   0.8813
   4.500   0.8485   0.00953   0.00438  -0.0692   0.5873   0.8821
   4.750   0.8740   0.00961   0.00445  -0.0691   0.5785   0.8829
   5.000   0.8983   0.00972   0.00454  -0.0687   0.5678   0.8840
   5.250   0.9221   0.00984   0.00464  -0.0683   0.5549   0.8850
   5.500   0.9454   0.00998   0.00477  -0.0678   0.5422   0.8857
   5.750   0.9675   0.01016   0.00492  -0.0671   0.5288   0.8864
   6.000   0.9879   0.01038   0.00510  -0.0661   0.5136   0.8873
   6.250   1.0059   0.01061   0.00529  -0.0646   0.4985   0.8882
   6.500   1.0221   0.01087   0.00551  -0.0627   0.4829   0.8889
   6.750   1.0358   0.01113   0.00576  -0.0604   0.4685   0.8897
   7.000   1.0463   0.01143   0.00603  -0.0575   0.4543   0.8907
   7.250   1.0573   0.01181   0.00639  -0.0549   0.4406   0.8916
   7.500   1.0668   0.01228   0.00683  -0.0521   0.4256   0.8930
   7.750   1.0735   0.01289   0.00738  -0.0490   0.4073   0.8943
   8.250   1.0861   0.01437   0.00874  -0.0433   0.3682   0.8965
   8.500   1.0935   0.01518   0.00948  -0.0409   0.3492   0.8975
   8.750   1.0987   0.01613   0.01035  -0.0383   0.3284   0.8985
   9.000   1.1062   0.01705   0.01121  -0.0360   0.3079   0.8994
   9.250   1.1113   0.01812   0.01219  -0.0337   0.2852   0.9003
   9.500   1.1159   0.01928   0.01324  -0.0313   0.2604   0.9013
   9.750   1.1196   0.02048   0.01433  -0.0289   0.2365   0.9024
  10.000   1.1226   0.02179   0.01552  -0.0266   0.2109   0.9033
  10.250   1.1266   0.02308   0.01671  -0.0244   0.1858   0.9041
  10.500   1.1293   0.02451   0.01800  -0.0223   0.1593   0.9049
  10.750   1.1336   0.02590   0.01929  -0.0204   0.1371   0.9057
  11.000   1.1370   0.02741   0.02068  -0.0186   0.1139   0.9066
  11.250   1.1426   0.02883   0.02203  -0.0170   0.0949   0.9074
  11.500   1.1468   0.03040   0.02351  -0.0155   0.0772   0.9082
  11.750   1.1510   0.03204   0.02506  -0.0140   0.0603   0.9090
  12.000   1.1597   0.03340   0.02642  -0.0130   0.0522   0.9097
  12.250   1.1666   0.03493   0.02792  -0.0120   0.0427   0.9105
  12.500   1.1738   0.03649   0.02948  -0.0110   0.0352   0.9113
  12.750   1.1825   0.03798   0.03099  -0.0103   0.0299   0.9120
  13.000   1.1903   0.03958   0.03261  -0.0095   0.0253   0.9128
  13.250   1.1971   0.04131   0.03434  -0.0088   0.0212   0.9136
  13.500   1.2050   0.04298   0.03606  -0.0082   0.0182   0.9143
  13.750   1.2125   0.04474   0.03785  -0.0077   0.0162   0.9150
  14.250   1.2262   0.04847   0.04171  -0.0067   0.0132   0.9166
  14.500   1.2335   0.05035   0.04367  -0.0064   0.0122   0.9176
  14.750   1.2396   0.05240   0.04579  -0.0061   0.0112   0.9187
  15.000   1.2453   0.05455   0.04801  -0.0059   0.0106   0.9198
  15.250   1.2485   0.05702   0.05055  -0.0058   0.0098   0.9210
  15.500   1.2538   0.05932   0.05295  -0.0057   0.0095   0.9221
  15.750   1.2594   0.06164   0.05536  -0.0059   0.0091   0.9231
  16.000   1.2628   0.06429   0.05810  -0.0060   0.0086   0.9242
  16.250   1.2657   0.06705   0.06095  -0.0063   0.0082   0.9253
  16.500   1.2678   0.06998   0.06397  -0.0067   0.0077   0.9265
  16.750   1.2699   0.07298   0.06705  -0.0073   0.0076   0.9276
  17.000   1.2688   0.07649   0.07066  -0.0079   0.0072   0.9287
  17.500   1.2721   0.08304   0.07744  -0.0097   0.0068   0.9315
  17.750   1.2724   0.08658   0.08109  -0.0108   0.0065   0.9331
  18.000   1.2711   0.09042   0.08504  -0.0120   0.0065   0.9348
  18.250   1.2712   0.09412   0.08885  -0.0133   0.0063   0.9368
  18.500   1.2704   0.09803   0.09287  -0.0148   0.0060   0.9390
  18.750   1.2685   0.10221   0.09716  -0.0165   0.0059   0.9412
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