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AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AS5045 (15%) (as5045-il)
Reynolds number: 200,000
Max Cl/Cd: 56.6 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5045-il-200000-n5.txt
Download as CSV file: xf-as5045-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6112   0.11480   0.11120  -0.0129   1.0000   0.0131
 -13.000  -0.6215   0.10631   0.10272  -0.0175   1.0000   0.0130
 -12.750  -0.6383   0.09656   0.09291  -0.0236   1.0000   0.0128
 -12.500  -0.6596   0.08730   0.08355  -0.0300   1.0000   0.0127
 -12.250  -0.6813   0.07964   0.07576  -0.0353   0.9135   0.0126
 -12.000  -0.6999   0.07259   0.06832  -0.0405   0.8503   0.0125
 -11.750  -0.7184   0.06710   0.06255  -0.0431   0.8309   0.0124
 -11.500  -0.7352   0.06219   0.05737  -0.0449   0.8195   0.0124
 -11.250  -0.7496   0.05778   0.05270  -0.0460   0.8112   0.0123
 -11.000  -0.7615   0.05376   0.04841  -0.0467   0.8043   0.0123
 -10.750  -0.7702   0.05014   0.04449  -0.0468   0.7987   0.0123
 -10.500  -0.7752   0.04683   0.04090  -0.0467   0.7937   0.0123
 -10.250  -0.7777   0.04397   0.03773  -0.0459   0.7891   0.0123
 -10.000  -0.7737   0.04120   0.03460  -0.0452   0.7851   0.0124
  -9.750  -0.7655   0.03859   0.03160  -0.0444   0.7816   0.0127
  -9.500  -0.7537   0.03626   0.02882  -0.0437   0.7781   0.0131
  -9.250  -0.7373   0.03423   0.02658  -0.0433   0.7751   0.0134
  -9.000  -0.7181   0.03263   0.02483  -0.0431   0.7724   0.0136
  -8.750  -0.6975   0.03103   0.02303  -0.0427   0.7700   0.0138
  -8.500  -0.6757   0.02953   0.02134  -0.0423   0.7678   0.0139
  -8.250  -0.6531   0.02817   0.01983  -0.0419   0.7654   0.0141
  -8.000  -0.6300   0.02692   0.01848  -0.0414   0.7628   0.0142
  -7.750  -0.6069   0.02579   0.01725  -0.0410   0.7602   0.0145
  -7.500  -0.5841   0.02475   0.01612  -0.0405   0.7579   0.0147
  -7.250  -0.5615   0.02377   0.01508  -0.0400   0.7558   0.0151
  -7.000  -0.5393   0.02286   0.01409  -0.0396   0.7539   0.0154
  -6.750  -0.5171   0.02200   0.01316  -0.0392   0.7521   0.0159
  -6.500  -0.4945   0.02119   0.01226  -0.0389   0.7502   0.0163
  -6.250  -0.4720   0.02031   0.01137  -0.0389   0.7478   0.0169
  -6.000  -0.4485   0.01955   0.01060  -0.0390   0.7455   0.0177
  -5.750  -0.4236   0.01896   0.00996  -0.0392   0.7435   0.0192
  -5.500  -0.3984   0.01835   0.00928  -0.0394   0.7416   0.0210
  -5.250  -0.3726   0.01778   0.00866  -0.0397   0.7398   0.0228
  -5.000  -0.3461   0.01729   0.00807  -0.0400   0.7380   0.0253
  -4.750  -0.3195   0.01676   0.00748  -0.0403   0.7362   0.0304
  -4.500  -0.2930   0.01606   0.00689  -0.0408   0.7343   0.0533
  -4.250  -0.2710   0.01320   0.00564  -0.0434   0.7323   0.3649
  -4.000  -0.2457   0.01276   0.00615  -0.0432   0.7304   0.5555
  -3.750  -0.2174   0.01357   0.00701  -0.0425   0.7284   0.6139
  -3.500  -0.1888   0.01405   0.00742  -0.0421   0.7262   0.6302
  -3.250  -0.1598   0.01416   0.00743  -0.0423   0.7241   0.6357
  -3.000  -0.1311   0.01432   0.00751  -0.0423   0.7224   0.6409
  -2.750  -0.1009   0.01435   0.00737  -0.0429   0.7206   0.6478
  -2.500  -0.0722   0.01443   0.00740  -0.0430   0.7187   0.6509
  -2.250  -0.0434   0.01448   0.00743  -0.0432   0.7163   0.6539
  -2.000  -0.0141   0.01451   0.00741  -0.0436   0.7137   0.6576
  -1.750   0.0159   0.01449   0.00731  -0.0442   0.7111   0.6619
  -1.500   0.0457   0.01447   0.00721  -0.0448   0.7086   0.6652
  -1.250   0.0743   0.01450   0.00721  -0.0449   0.7061   0.6673
  -1.000   0.1031   0.01454   0.00720  -0.0450   0.7039   0.6699
  -0.750   0.1322   0.01456   0.00722  -0.0454   0.7005   0.6728
  -0.500   0.1618   0.01454   0.00718  -0.0460   0.6969   0.6759
  -0.250   0.1919   0.01450   0.00708  -0.0466   0.6933   0.6789
   0.000   0.2214   0.01446   0.00700  -0.0471   0.6901   0.6810
   0.250   0.2502   0.01446   0.00698  -0.0472   0.6871   0.6826
   0.500   0.2789   0.01444   0.00701  -0.0475   0.6821   0.6843
   0.750   0.3079   0.01440   0.00698  -0.0478   0.6775   0.6861
   1.000   0.3371   0.01436   0.00691  -0.0481   0.6736   0.6882
   1.250   0.3663   0.01433   0.00689  -0.0485   0.6689   0.6904
   1.500   0.3957   0.01427   0.00687  -0.0489   0.6631   0.6924
   1.750   0.4255   0.01419   0.00676  -0.0494   0.6581   0.6945
   2.000   0.4549   0.01413   0.00672  -0.0498   0.6523   0.6965
   2.250   0.4833   0.01404   0.00670  -0.0499   0.6452   0.6980
   2.500   0.5120   0.01393   0.00662  -0.0500   0.6389   0.6995
   2.750   0.5406   0.01386   0.00663  -0.0502   0.6298   0.7010
   3.000   0.5694   0.01376   0.00657  -0.0504   0.6214   0.7026
   3.250   0.5983   0.01366   0.00653  -0.0506   0.6112   0.7045
   3.500   0.6271   0.01359   0.00652  -0.0509   0.5989   0.7066
   3.750   0.6560   0.01350   0.00647  -0.0511   0.5850   0.7087
   4.000   0.6848   0.01342   0.00638  -0.0513   0.5674   0.7106
   4.250   0.7130   0.01336   0.00629  -0.0514   0.5444   0.7122
   4.500   0.7395   0.01338   0.00622  -0.0511   0.5133   0.7135
   4.750   0.7644   0.01357   0.00625  -0.0505   0.4747   0.7152
   5.000   0.7885   0.01393   0.00643  -0.0500   0.4350   0.7170
   5.250   0.8124   0.01436   0.00671  -0.0496   0.3978   0.7189
   5.500   0.8362   0.01483   0.00706  -0.0492   0.3635   0.7207
   5.750   0.8599   0.01533   0.00743  -0.0489   0.3317   0.7225
   6.000   0.8835   0.01584   0.00783  -0.0486   0.3018   0.7244
   6.250   0.9070   0.01637   0.00826  -0.0483   0.2739   0.7264
   6.500   0.9295   0.01693   0.00874  -0.0479   0.2469   0.7283
   6.750   0.9513   0.01750   0.00924  -0.0473   0.2223   0.7301
   7.000   0.9734   0.01805   0.00974  -0.0468   0.2015   0.7319
   7.250   0.9954   0.01860   0.01028  -0.0463   0.1831   0.7338
   7.500   1.0170   0.01917   0.01083  -0.0457   0.1670   0.7357
   7.750   1.0383   0.01977   0.01140  -0.0452   0.1522   0.7378
   8.000   1.0591   0.02038   0.01202  -0.0446   0.1389   0.7399
   8.250   1.0794   0.02103   0.01265  -0.0439   0.1271   0.7422
   8.500   1.0983   0.02171   0.01334  -0.0431   0.1161   0.7444
   8.750   1.1168   0.02238   0.01404  -0.0422   0.1061   0.7465
   9.000   1.1346   0.02307   0.01480  -0.0412   0.0977   0.7489
   9.250   1.1504   0.02389   0.01562  -0.0400   0.0901   0.7514
   9.500   1.1661   0.02463   0.01644  -0.0388   0.0833   0.7539
   9.750   1.1770   0.02555   0.01738  -0.0371   0.0779   0.7565
  10.250   1.2030   0.02758   0.01955  -0.0348   0.0681   0.7616
  10.500   1.2159   0.02868   0.02077  -0.0339   0.0643   0.7643
  10.750   1.2282   0.02991   0.02209  -0.0332   0.0607   0.7673
  11.000   1.2379   0.03141   0.02363  -0.0325   0.0575   0.7707
  11.250   1.2494   0.03280   0.02514  -0.0320   0.0548   0.7745
  11.500   1.2603   0.03420   0.02667  -0.0313   0.0521   0.7779
  11.750   1.2693   0.03579   0.02837  -0.0307   0.0499   0.7818
  12.000   1.2752   0.03768   0.03031  -0.0300   0.0479   0.7860
  12.250   1.2842   0.03933   0.03209  -0.0294   0.0460   0.7906
  12.500   1.2921   0.04101   0.03392  -0.0288   0.0442   0.7950
  12.750   1.2989   0.04284   0.03587  -0.0282   0.0425   0.8003
  13.000   1.3035   0.04490   0.03803  -0.0277   0.0411   0.8064
  13.250   1.3046   0.04725   0.04046  -0.0270   0.0398   0.8130
  13.500   1.3093   0.04933   0.04270  -0.0264   0.0386   0.8216
  13.750   1.3130   0.05145   0.04502  -0.0259   0.0373   0.8326
  14.000   1.3149   0.05370   0.04746  -0.0253   0.0361   0.8485
  14.250   1.3136   0.05592   0.04989  -0.0242   0.0350   0.8835
  14.500   1.3085   0.05828   0.05240  -0.0231   0.0342   1.0000
  14.750   1.3075   0.06133   0.05552  -0.0233   0.0333   1.0000
  15.000   1.3056   0.06459   0.05883  -0.0237   0.0325   1.0000
  15.250   1.3064   0.06772   0.06215  -0.0242   0.0316   1.0000
  15.500   1.3057   0.07113   0.06572  -0.0250   0.0306   1.0000
  15.750   1.3038   0.07480   0.06953  -0.0260   0.0297   1.0000
  16.000   1.3010   0.07872   0.07356  -0.0273   0.0288   1.0000
  16.250   1.2972   0.08289   0.07784  -0.0287   0.0281   1.0000
  16.500   1.2920   0.08733   0.08239  -0.0304   0.0275   1.0000
  16.750   1.2856   0.09197   0.08710  -0.0322   0.0269   1.0000
  17.000   1.2787   0.09694   0.09224  -0.0343   0.0263   1.0000
  17.250   1.2709   0.10221   0.09770  -0.0366   0.0257   1.0000
  17.500   1.2618   0.10778   0.10343  -0.0392   0.0251   1.0000
  17.750   1.2522   0.11354   0.10936  -0.0421   0.0246   1.0000
  18.000   1.2419   0.11956   0.11552  -0.0453   0.0241   1.0000
  18.250   1.2314   0.12578   0.12187  -0.0487   0.0236   1.0000
  18.500   1.2208   0.13212   0.12833  -0.0523   0.0232   1.0000
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