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AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AS5045 (15%) (as5045-il)
Reynolds number: 500,000
Max Cl/Cd: 79.37 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-as5045-il-500000.txt
Download as CSV file: xf-as5045-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5045 (15%)                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5148   0.07714   0.07421  -0.0429   0.7762   0.0226
 -11.500  -0.5576   0.06720   0.06413  -0.0477   0.7755   0.0221
 -11.250  -0.7494   0.06820   0.06433  -0.0470   0.7804   0.0204
 -11.000  -0.7537   0.06078   0.05694  -0.0477   0.7782   0.0209
 -10.750  -0.7568   0.05764   0.05372  -0.0480   0.7754   0.0211
 -10.500  -0.7609   0.05476   0.05074  -0.0481   0.7727   0.0212
 -10.250  -0.7631   0.05224   0.04809  -0.0478   0.7702   0.0214
 -10.000  -0.7591   0.04979   0.04551  -0.0476   0.7679   0.0217
  -9.750  -0.7533   0.04734   0.04292  -0.0474   0.7657   0.0221
  -9.500  -0.7455   0.04488   0.04028  -0.0471   0.7635   0.0227
  -8.250  -0.6753   0.02780   0.02102  -0.0424   0.7541   0.0166
  -8.000  -0.6501   0.02489   0.01811  -0.0421   0.7524   0.0159
  -7.750  -0.6256   0.02323   0.01631  -0.0416   0.7506   0.0156
  -7.500  -0.6007   0.02185   0.01484  -0.0412   0.7490   0.0155
  -7.250  -0.5760   0.02068   0.01359  -0.0408   0.7473   0.0154
  -7.000  -0.5511   0.01981   0.01266  -0.0405   0.7457   0.0157
  -6.750  -0.5260   0.01908   0.01186  -0.0403   0.7440   0.0161
  -6.500  -0.5010   0.01834   0.01107  -0.0401   0.7424   0.0163
  -6.250  -0.4766   0.01753   0.01022  -0.0399   0.7407   0.0164
  -6.000  -0.4517   0.01683   0.00947  -0.0398   0.7390   0.0165
  -5.750  -0.4284   0.01577   0.00839  -0.0398   0.7373   0.0169
  -5.500  -0.4028   0.01507   0.00766  -0.0401   0.7356   0.0175
  -5.250  -0.3757   0.01453   0.00711  -0.0405   0.7343   0.0184
  -5.000  -0.3479   0.01406   0.00662  -0.0409   0.7329   0.0196
  -4.750  -0.3198   0.01359   0.00611  -0.0414   0.7312   0.0209
  -4.500  -0.2914   0.01316   0.00567  -0.0419   0.7293   0.0236
  -4.250  -0.2626   0.01273   0.00524  -0.0424   0.7275   0.0319
  -4.000  -0.2343   0.00915   0.00371  -0.0467   0.7259   0.4867
  -3.750  -0.2044   0.00908   0.00394  -0.0472   0.7242   0.5807
  -3.500  -0.1745   0.00928   0.00409  -0.0474   0.7225   0.6039
  -3.250  -0.1453   0.00970   0.00450  -0.0474   0.7207   0.6234
  -3.000  -0.1169   0.01029   0.00511  -0.0470   0.7190   0.6395
  -2.750  -0.0869   0.01051   0.00527  -0.0473   0.7171   0.6476
  -2.500  -0.0577   0.01055   0.00532  -0.0475   0.7149   0.6511
  -2.250  -0.0286   0.01065   0.00542  -0.0476   0.7124   0.6547
  -2.000   0.0008   0.01074   0.00548  -0.0478   0.7100   0.6588
  -1.750   0.0309   0.01079   0.00545  -0.0483   0.7076   0.6626
  -1.500   0.0607   0.01081   0.00539  -0.0488   0.7053   0.6653
  -1.250   0.0897   0.01085   0.00544  -0.0490   0.7027   0.6674
  -1.000   0.1190   0.01085   0.00545  -0.0492   0.6997   0.6698
  -0.750   0.1485   0.01084   0.00545  -0.0496   0.6965   0.6722
  -0.500   0.1782   0.01083   0.00540  -0.0500   0.6933   0.6748
  -0.250   0.2081   0.01083   0.00534  -0.0504   0.6902   0.6775
   0.000   0.2382   0.01092   0.00536  -0.0509   0.6872   0.6802
   0.250   0.2674   0.01078   0.00528  -0.0512   0.6835   0.6822
   0.500   0.2967   0.01071   0.00523  -0.0515   0.6795   0.6838
   0.750   0.3262   0.01066   0.00517  -0.0518   0.6759   0.6854
   1.000   0.3557   0.01065   0.00512  -0.0521   0.6725   0.6872
   1.250   0.3852   0.01058   0.00509  -0.0525   0.6679   0.6891
   1.500   0.4149   0.01049   0.00500  -0.0529   0.6628   0.6908
   1.750   0.4447   0.01040   0.00489  -0.0533   0.6584   0.6926
   2.000   0.4746   0.01035   0.00483  -0.0537   0.6537   0.6945
   2.250   0.5045   0.01026   0.00476  -0.0542   0.6477   0.6960
   2.500   0.5339   0.01010   0.00461  -0.0545   0.6424   0.6974
   2.750   0.5631   0.00998   0.00454  -0.0548   0.6363   0.6987
   3.000   0.5924   0.00986   0.00446  -0.0550   0.6289   0.7002
   3.250   0.6216   0.00976   0.00441  -0.0553   0.6211   0.7018
   3.500   0.6508   0.00966   0.00433  -0.0555   0.6112   0.7034
   3.750   0.6801   0.00957   0.00427  -0.0558   0.5976   0.7050
   4.000   0.7089   0.00951   0.00420  -0.0560   0.5801   0.7065
   4.250   0.7375   0.00953   0.00418  -0.0562   0.5572   0.7081
   4.500   0.7651   0.00966   0.00419  -0.0562   0.5250   0.7098
   4.750   0.7913   0.00997   0.00432  -0.0561   0.4834   0.7114
   5.000   0.8168   0.01032   0.00451  -0.0559   0.4431   0.7129
   5.250   0.8417   0.01074   0.00477  -0.0557   0.4014   0.7142
   5.500   0.8660   0.01123   0.00509  -0.0554   0.3587   0.7156
   5.750   0.8907   0.01168   0.00540  -0.0552   0.3224   0.7171
   6.000   0.9155   0.01213   0.00573  -0.0550   0.2914   0.7187
   6.250   0.9401   0.01259   0.00608  -0.0548   0.2619   0.7205
   6.500   0.9645   0.01307   0.00644  -0.0545   0.2354   0.7224
   6.750   0.9893   0.01350   0.00679  -0.0543   0.2121   0.7241
   7.000   1.0133   0.01400   0.00718  -0.0541   0.1905   0.7257
   7.250   1.0377   0.01445   0.00757  -0.0539   0.1721   0.7272
   7.500   1.0616   0.01488   0.00795  -0.0536   0.1553   0.7287
   7.750   1.0849   0.01534   0.00838  -0.0532   0.1398   0.7305
   8.000   1.1078   0.01582   0.00883  -0.0527   0.1258   0.7324
   8.250   1.1304   0.01633   0.00931  -0.0522   0.1132   0.7343
   8.500   1.1523   0.01688   0.00983  -0.0516   0.1019   0.7362
   8.750   1.1734   0.01748   0.01039  -0.0510   0.0916   0.7381
   9.000   1.1952   0.01800   0.01092  -0.0504   0.0834   0.7400
   9.250   1.2154   0.01863   0.01155  -0.0496   0.0759   0.7419
   9.500   1.2344   0.01931   0.01221  -0.0487   0.0695   0.7437
   9.750   1.2531   0.01993   0.01291  -0.0477   0.0646   0.7458
  10.000   1.2706   0.02060   0.01360  -0.0466   0.0601   0.7480
  10.250   1.2841   0.02149   0.01452  -0.0450   0.0561   0.7504
  10.500   1.2979   0.02209   0.01521  -0.0433   0.0534   0.7530
  10.750   1.3108   0.02295   0.01610  -0.0417   0.0506   0.7556
  11.000   1.3170   0.02442   0.01759  -0.0399   0.0477   0.7580
  11.250   1.3327   0.02526   0.01855  -0.0392   0.0460   0.7605
  11.500   1.3463   0.02632   0.01972  -0.0385   0.0439   0.7631
  11.750   1.3575   0.02767   0.02112  -0.0379   0.0421   0.7660
  12.000   1.3621   0.02966   0.02316  -0.0370   0.0401   0.7691
  12.250   1.3727   0.03114   0.02474  -0.0364   0.0387   0.7723
  12.500   1.3855   0.03242   0.02612  -0.0360   0.0372   0.7756
  12.750   1.3964   0.03384   0.02764  -0.0356   0.0356   0.7791
  13.000   1.4038   0.03558   0.02945  -0.0350   0.0342   0.7831
  13.250   1.4017   0.03821   0.03213  -0.0340   0.0328   0.7875
  13.500   1.4117   0.03975   0.03381  -0.0336   0.0319   0.7923
  13.750   1.4204   0.04140   0.03560  -0.0332   0.0308   0.7980
  14.000   1.4270   0.04327   0.03757  -0.0327   0.0297   0.8045
  14.250   1.4322   0.04527   0.03969  -0.0324   0.0288   0.8121
  14.500   1.4338   0.04766   0.04217  -0.0320   0.0279   0.8220
  14.750   1.4278   0.05078   0.04541  -0.0313   0.0270   0.8357
  15.000   1.4287   0.05315   0.04803  -0.0308   0.0264   0.8653
  15.250   1.4244   0.05511   0.05024  -0.0290   0.0259   1.0000
  15.500   1.4268   0.05782   0.05305  -0.0293   0.0251   1.0000
  15.750   1.4282   0.06075   0.05607  -0.0297   0.0244   1.0000
  16.000   1.4287   0.06389   0.05929  -0.0302   0.0237   1.0000
  16.250   1.4273   0.06736   0.06283  -0.0310   0.0231   1.0000
  16.500   1.4215   0.07143   0.06697  -0.0319   0.0225   1.0000
  16.750   1.4103   0.07620   0.07180  -0.0329   0.0218   1.0000
  17.000   1.4087   0.08008   0.07584  -0.0342   0.0214   1.0000
  17.250   1.4049   0.08433   0.08022  -0.0356   0.0209   1.0000
  17.500   1.3997   0.08884   0.08485  -0.0373   0.0204   1.0000
  17.750   1.3934   0.09356   0.08968  -0.0391   0.0198   1.0000
  18.000   1.3859   0.09856   0.09478  -0.0411   0.0194   1.0000
  18.250   1.3776   0.10377   0.10010  -0.0434   0.0190   1.0000
  18.500   1.3680   0.10924   0.10565  -0.0458   0.0186   1.0000
  18.750   1.3567   0.11492   0.11140  -0.0484   0.0181   1.0000
  19.000   1.3442   0.12073   0.11728  -0.0509   0.0177   1.0000
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