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AH 82-150 F (ah82150f-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 82-150 F (ah82150f-il)
Reynolds number: 500,000
Max Cl/Cd: 99.21 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah82150f-il-500000-n5.txt
Download as CSV file: xf-ah82150f-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 F                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1444   0.08655   0.08334  -0.1045   0.7959   0.0082
 -12.000  -0.4269   0.04449   0.04097  -0.1365   0.7982   0.0067
 -11.750  -0.4724   0.03847   0.03468  -0.1344   0.7967   0.0066
 -11.500  -0.5035   0.03430   0.03019  -0.1304   0.7954   0.0066
 -11.250  -0.5149   0.03186   0.02751  -0.1270   0.7941   0.0066
 -11.000  -0.5251   0.02947   0.02484  -0.1231   0.7928   0.0068
 -10.750  -0.5266   0.02780   0.02293  -0.1197   0.7917   0.0069
 -10.500  -0.5219   0.02670   0.02161  -0.1169   0.7909   0.0071
 -10.250  -0.5154   0.02531   0.01997  -0.1143   0.7900   0.0073
 -10.000  -0.5074   0.02376   0.01818  -0.1119   0.7893   0.0075
  -9.750  -0.4981   0.02218   0.01640  -0.1097   0.7885   0.0078
  -9.500  -0.4827   0.02122   0.01530  -0.1083   0.7877   0.0080
  -9.250  -0.4647   0.02047   0.01443  -0.1072   0.7870   0.0083
  -9.000  -0.4458   0.01970   0.01354  -0.1062   0.7862   0.0086
  -8.750  -0.4259   0.01899   0.01272  -0.1053   0.7854   0.0089
  -8.500  -0.4053   0.01833   0.01195  -0.1045   0.7847   0.0093
  -8.250  -0.3841   0.01769   0.01118  -0.1038   0.7840   0.0097
  -8.000  -0.3626   0.01707   0.01045  -0.1031   0.7832   0.0102
  -7.750  -0.3407   0.01650   0.00977  -0.1024   0.7824   0.0106
  -7.500  -0.3183   0.01600   0.00917  -0.1018   0.7815   0.0110
  -7.250  -0.2971   0.01537   0.00849  -0.1011   0.7807   0.0120
  -7.000  -0.2736   0.01503   0.00811  -0.1007   0.7801   0.0131
  -6.750  -0.2498   0.01470   0.00774  -0.1003   0.7794   0.0142
  -6.500  -0.2261   0.01437   0.00734  -0.0999   0.7788   0.0154
  -6.250  -0.2029   0.01397   0.00687  -0.0993   0.7782   0.0170
  -6.000  -0.1789   0.01368   0.00656  -0.0990   0.7776   0.0190
  -5.750  -0.1542   0.01345   0.00629  -0.0987   0.7771   0.0211
  -5.500  -0.1291   0.01326   0.00605  -0.0985   0.7765   0.0228
  -5.250  -0.1050   0.01299   0.00576  -0.0982   0.7759   0.0259
  -5.000  -0.0803   0.01282   0.00560  -0.0979   0.7752   0.0293
  -4.750  -0.0553   0.01270   0.00545  -0.0977   0.7744   0.0320
  -4.500  -0.0314   0.01245   0.00520  -0.0973   0.7735   0.0356
  -4.250  -0.0068   0.01228   0.00504  -0.0970   0.7727   0.0393
  -4.000   0.0184   0.01216   0.00490  -0.0969   0.7719   0.0431
  -3.750   0.0432   0.01200   0.00473  -0.0966   0.7711   0.0480
  -3.500   0.0683   0.01186   0.00460  -0.0964   0.7703   0.0542
  -3.250   0.0934   0.01171   0.00447  -0.0962   0.7694   0.0638
  -3.000   0.1182   0.01153   0.00436  -0.0960   0.7684   0.0820
  -2.750   0.1423   0.01129   0.00424  -0.0957   0.7676   0.1186
  -2.500   0.1650   0.01094   0.00414  -0.0952   0.7667   0.1896
  -2.250   0.1864   0.01049   0.00404  -0.0945   0.7658   0.2923
  -2.000   0.2074   0.01001   0.00393  -0.0938   0.7649   0.4031
  -1.750   0.2282   0.00951   0.00381  -0.0929   0.7640   0.5169
  -1.500   0.2461   0.00882   0.00369  -0.0914   0.7629   0.6735
  -1.250   0.2669   0.00899   0.00426  -0.0894   0.7617   0.8014
  -1.000   0.2910   0.00928   0.00456  -0.0885   0.7597   0.8296
  -0.750   0.3153   0.00956   0.00484  -0.0877   0.7578   0.8429
  -0.500   0.3416   0.00964   0.00490  -0.0875   0.7559   0.8485
  -0.250   0.3682   0.00972   0.00497  -0.0873   0.7541   0.8521
   0.000   0.3954   0.00979   0.00500  -0.0872   0.7522   0.8585
   0.250   0.4213   0.00990   0.00510  -0.0866   0.7504   0.8654
   0.500   0.4488   0.00997   0.00513  -0.0864   0.7487   0.8719
   0.750   0.4742   0.00997   0.00514  -0.0863   0.7459   0.8741
   1.000   0.5003   0.00994   0.00511  -0.0863   0.7431   0.8752
   1.250   0.5271   0.00989   0.00506  -0.0864   0.7407   0.8758
   1.500   0.5553   0.00982   0.00498  -0.0868   0.7386   0.8764
   1.750   0.5843   0.00974   0.00489  -0.0873   0.7367   0.8768
   2.000   0.6137   0.00967   0.00480  -0.0880   0.7350   0.8774
   2.250   0.6373   0.00970   0.00488  -0.0875   0.7317   0.8783
   2.500   0.6626   0.00969   0.00490  -0.0873   0.7284   0.8790
   2.750   0.6898   0.00964   0.00488  -0.0875   0.7254   0.8796
   3.000   0.7182   0.00956   0.00481  -0.0879   0.7228   0.8802
   3.250   0.7445   0.00953   0.00480  -0.0880   0.7195   0.8808
   3.500   0.7680   0.00954   0.00488  -0.0875   0.7147   0.8816
   3.750   0.7941   0.00949   0.00487  -0.0875   0.7105   0.8824
   4.000   0.8202   0.00945   0.00487  -0.0874   0.7061   0.8833
   4.250   0.8428   0.00947   0.00495  -0.0868   0.6990   0.8842
   4.500   0.8679   0.00942   0.00493  -0.0865   0.6925   0.8849
   4.750   0.8906   0.00941   0.00498  -0.0858   0.6834   0.8857
   5.000   0.9127   0.00934   0.00490  -0.0849   0.6675   0.8864
   5.250   0.9256   0.00933   0.00470  -0.0820   0.6278   0.8875
   5.500   0.9221   0.00969   0.00482  -0.0759   0.5874   0.8891
   5.750   0.9156   0.01032   0.00529  -0.0695   0.5521   0.8909
   6.000   0.9141   0.01100   0.00585  -0.0645   0.5235   0.8927
   6.250   0.9113   0.01183   0.00656  -0.0595   0.4920   0.8943
   6.500   0.9056   0.01289   0.00744  -0.0543   0.4550   0.8961
   6.750   0.9052   0.01389   0.00829  -0.0503   0.4204   0.8977
   7.000   0.9057   0.01495   0.00918  -0.0465   0.3846   0.8992
   7.250   0.9020   0.01625   0.01021  -0.0423   0.3327   0.9007
   7.500   0.8907   0.01802   0.01150  -0.0373   0.2500   0.9023
   7.750   0.8840   0.01966   0.01269  -0.0330   0.1684   0.9039
   8.000   0.8721   0.02172   0.01418  -0.0282   0.0664   0.9054
   8.250   0.8745   0.02312   0.01532  -0.0254   0.0170   0.9065
   8.500   0.8895   0.02384   0.01606  -0.0242   0.0129   0.9074
   8.750   0.9057   0.02449   0.01678  -0.0232   0.0117   0.9083
   9.000   0.9205   0.02524   0.01758  -0.0221   0.0101   0.9092
   9.250   0.9347   0.02605   0.01843  -0.0209   0.0089   0.9102
   9.500   0.9471   0.02699   0.01946  -0.0196   0.0082   0.9112
   9.750   0.9614   0.02783   0.02036  -0.0185   0.0079   0.9123
  10.000   0.9748   0.02875   0.02134  -0.0174   0.0075   0.9133
  10.250   0.9869   0.02978   0.02245  -0.0161   0.0071   0.9143
  10.500   0.9985   0.03086   0.02362  -0.0149   0.0069   0.9154
  10.750   1.0096   0.03202   0.02484  -0.0137   0.0065   0.9164
  11.000   1.0204   0.03317   0.02604  -0.0126   0.0061   0.9176
  11.250   1.0289   0.03452   0.02746  -0.0112   0.0058   0.9188
  11.500   1.0305   0.03645   0.02948  -0.0093   0.0053   0.9201
  11.750   1.0430   0.03756   0.03065  -0.0085   0.0051   0.9215
  12.000   1.0511   0.03908   0.03227  -0.0073   0.0050   0.9230
  12.250   1.0590   0.04065   0.03393  -0.0061   0.0048   0.9247
  12.500   1.0677   0.04219   0.03556  -0.0052   0.0046   0.9265
  12.750   1.0743   0.04396   0.03742  -0.0041   0.0044   0.9284
  13.250   1.0876   0.04762   0.04131  -0.0022   0.0042   0.9320
  13.500   1.0967   0.04923   0.04301  -0.0016   0.0039   0.9344
  13.750   1.1031   0.05121   0.04509  -0.0008   0.0039   0.9367
  14.000   1.1112   0.05307   0.04704  -0.0004   0.0037   0.9395
  14.250   1.1179   0.05518   0.04926   0.0001   0.0037   0.9422
  14.750   1.1325   0.05949   0.05377   0.0004   0.0035   0.9504
  15.000   1.1388   0.06191   0.05631   0.0003   0.0034   0.9553
  15.250   1.1449   0.06454   0.05907   0.0000   0.0033   0.9619
  15.500   1.1501   0.06730   0.06197  -0.0003   0.0033   0.9725
  15.750   1.1471   0.07069   0.06558   0.0005   0.0031   1.0000
  16.000   1.1483   0.07385   0.06891   0.0004   0.0031   1.0000
  16.250   1.1480   0.07728   0.07250   0.0001   0.0031   1.0000
  16.500   1.1454   0.08114   0.07656  -0.0004   0.0030   1.0000
  16.750   1.1411   0.08530   0.08089  -0.0011   0.0031   1.0000
  17.000   1.1352   0.08980   0.08558  -0.0021   0.0030   1.0000
  17.250   1.1276   0.09469   0.09065  -0.0035   0.0030   1.0000
  17.500   1.1173   0.10018   0.09634  -0.0052   0.0030   1.0000
  17.750   1.1061   0.10599   0.10235  -0.0074   0.0030   1.0000
  18.000   1.0939   0.11216   0.10871  -0.0100   0.0030   1.0000
  18.250   1.0804   0.11876   0.11550  -0.0131   0.0030   1.0000
  18.500   1.0678   0.12538   0.12228  -0.0165   0.0030   1.0000
  18.750   1.0526   0.13284   0.12991  -0.0205   0.0030   1.0000
  19.000   1.0384   0.14034   0.13756  -0.0248   0.0030   1.0000
  19.250   1.0195   0.14934   0.14675  -0.0301   0.0030   1.0000
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