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MH 201 13.08% (mh201-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 201 13.08% (mh201-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.93 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh201-il-1000000-n5.txt
Download as CSV file: xf-mh201-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 201  13.08%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6475   0.06594   0.06399  -0.0617   0.9999   0.0034
 -12.250  -0.6646   0.05399   0.05183  -0.0735   0.9988   0.0035
 -12.000  -0.6921   0.04322   0.04074  -0.0848   0.9961   0.0034
 -11.750  -0.7013   0.03749   0.03473  -0.0901   0.9933   0.0034
 -11.500  -0.6993   0.03429   0.03136  -0.0923   0.9896   0.0034
 -11.250  -0.6949   0.03098   0.02781  -0.0949   0.9857   0.0034
 -11.000  -0.6924   0.02841   0.02502  -0.0953   0.9793   0.0034
 -10.750  -0.6812   0.02600   0.02239  -0.0962   0.9731   0.0034
 -10.500  -0.6726   0.02404   0.02020  -0.0952   0.9641   0.0034
 -10.000  -0.6330   0.02087   0.01666  -0.0959   0.9519   0.0035
  -9.750  -0.6029   0.01984   0.01550  -0.0977   0.9478   0.0036
  -9.500  -0.5705   0.01857   0.01407  -0.1000   0.9438   0.0036
  -9.250  -0.5382   0.01762   0.01299  -0.1020   0.9373   0.0036
  -8.750  -0.4742   0.01585   0.01094  -0.1055   0.9218   0.0037
  -8.500  -0.4458   0.01510   0.01007  -0.1064   0.9117   0.0037
  -8.250  -0.4210   0.01426   0.00908  -0.1065   0.9001   0.0038
  -8.000  -0.3978   0.01358   0.00827  -0.1061   0.8883   0.0038
  -7.750  -0.3746   0.01299   0.00758  -0.1056   0.8782   0.0038
  -7.500  -0.3519   0.01234   0.00681  -0.1051   0.8689   0.0039
  -7.250  -0.3283   0.01184   0.00622  -0.1046   0.8598   0.0039
  -7.000  -0.3039   0.01141   0.00571  -0.1043   0.8517   0.0040
  -6.750  -0.2794   0.01098   0.00520  -0.1039   0.8438   0.0041
  -6.500  -0.2540   0.01066   0.00481  -0.1036   0.8367   0.0041
  -6.250  -0.2284   0.01033   0.00442  -0.1034   0.8292   0.0043
  -6.000  -0.2024   0.01007   0.00411  -0.1032   0.8225   0.0044
  -5.750  -0.1761   0.00982   0.00381  -0.1031   0.8155   0.0046
  -5.250  -0.1227   0.00938   0.00327  -0.1029   0.8031   0.0053
  -5.000  -0.0958   0.00918   0.00302  -0.1028   0.7969   0.0059
  -4.750  -0.0688   0.00898   0.00279  -0.1027   0.7915   0.0076
  -4.500  -0.0414   0.00879   0.00260  -0.1028   0.7859   0.0104
  -4.250  -0.0142   0.00859   0.00242  -0.1028   0.7803   0.0179
  -4.000   0.0132   0.00841   0.00225  -0.1028   0.7751   0.0278
  -3.750   0.0407   0.00817   0.00208  -0.1030   0.7694   0.0489
  -3.500   0.0676   0.00781   0.00190  -0.1031   0.7636   0.0986
  -3.250   0.0946   0.00730   0.00172  -0.1035   0.7581   0.1861
  -3.000   0.1224   0.00704   0.00160  -0.1037   0.7518   0.2362
  -2.750   0.1501   0.00672   0.00148  -0.1041   0.7459   0.3061
  -2.500   0.1785   0.00641   0.00138  -0.1045   0.7399   0.3739
  -2.250   0.2067   0.00622   0.00130  -0.1048   0.7333   0.4239
  -2.000   0.2353   0.00602   0.00123  -0.1051   0.7270   0.4751
  -1.750   0.2638   0.00585   0.00118  -0.1055   0.7198   0.5255
  -1.500   0.2922   0.00573   0.00115  -0.1057   0.7129   0.5713
  -1.250   0.3207   0.00566   0.00115  -0.1059   0.7049   0.6062
  -1.000   0.3489   0.00564   0.00116  -0.1060   0.6968   0.6315
  -0.750   0.3770   0.00566   0.00118  -0.1060   0.6869   0.6493
  -0.500   0.4051   0.00569   0.00120  -0.1061   0.6767   0.6629
  -0.250   0.4329   0.00575   0.00122  -0.1061   0.6652   0.6740
   0.000   0.4603   0.00582   0.00125  -0.1060   0.6515   0.6827
   0.250   0.4875   0.00591   0.00128  -0.1058   0.6354   0.6905
   0.500   0.5144   0.00601   0.00134  -0.1056   0.6168   0.6989
   0.750   0.5406   0.00616   0.00139  -0.1053   0.5949   0.7061
   1.000   0.5667   0.00632   0.00147  -0.1050   0.5731   0.7117
   1.250   0.5927   0.00650   0.00155  -0.1046   0.5500   0.7163
   1.500   0.6187   0.00669   0.00163  -0.1043   0.5267   0.7201
   1.750   0.6441   0.00689   0.00174  -0.1039   0.5014   0.7234
   2.000   0.6698   0.00709   0.00185  -0.1035   0.4772   0.7268
   2.250   0.6951   0.00732   0.00198  -0.1031   0.4518   0.7304
   2.500   0.7204   0.00756   0.00210  -0.1027   0.4258   0.7342
   2.750   0.7455   0.00780   0.00224  -0.1023   0.4012   0.7378
   3.250   0.7953   0.00829   0.00256  -0.1013   0.3527   0.7444
   3.750   0.8450   0.00881   0.00288  -0.1004   0.3087   0.7496
   4.250   0.8939   0.00934   0.00325  -0.0994   0.2682   0.7540
   4.500   0.9186   0.00958   0.00344  -0.0989   0.2512   0.7563
   4.750   0.9428   0.00985   0.00364  -0.0983   0.2330   0.7586
   5.000   0.9670   0.01012   0.00385  -0.0978   0.2172   0.7609
   5.250   0.9910   0.01039   0.00406  -0.0972   0.2016   0.7633
   5.500   1.0148   0.01068   0.00429  -0.0966   0.1867   0.7656
   5.750   1.0388   0.01095   0.00452  -0.0960   0.1747   0.7676
   6.000   1.0620   0.01124   0.00476  -0.0953   0.1619   0.7699
   6.250   1.0849   0.01155   0.00503  -0.0946   0.1489   0.7722
   6.500   1.1074   0.01187   0.00531  -0.0938   0.1366   0.7746
   6.750   1.1303   0.01216   0.00558  -0.0930   0.1267   0.7770
   7.000   1.1530   0.01246   0.00586  -0.0922   0.1180   0.7794
   7.250   1.1746   0.01280   0.00617  -0.0913   0.1082   0.7820
   7.500   1.1962   0.01313   0.00648  -0.0903   0.0997   0.7843
   7.750   1.2169   0.01346   0.00680  -0.0892   0.0920   0.7868
   8.250   1.2555   0.01412   0.00746  -0.0863   0.0788   0.7922
   8.500   1.2738   0.01452   0.00784  -0.0848   0.0727   0.7954
   8.750   1.2931   0.01487   0.00820  -0.0835   0.0680   0.7984
   9.000   1.3106   0.01530   0.00863  -0.0818   0.0622   0.8014
   9.250   1.3290   0.01568   0.00904  -0.0804   0.0578   0.8046
   9.500   1.3457   0.01617   0.00952  -0.0787   0.0522   0.8081
   9.750   1.3634   0.01660   0.00997  -0.0772   0.0485   0.8117
  10.000   1.3791   0.01714   0.01051  -0.0755   0.0434   0.8154
  10.250   1.3954   0.01763   0.01103  -0.0738   0.0396   0.8198
  10.500   1.4100   0.01824   0.01165  -0.0720   0.0351   0.8245
  10.750   1.4248   0.01885   0.01227  -0.0703   0.0310   0.8291
  11.000   1.4382   0.01952   0.01296  -0.0684   0.0273   0.8340
  11.250   1.4527   0.02015   0.01363  -0.0667   0.0249   0.8397
  11.750   1.4788   0.02160   0.01517  -0.0632   0.0202   0.8525
  12.250   1.5019   0.02328   0.01695  -0.0595   0.0160   0.8709
  12.500   1.5111   0.02426   0.01800  -0.0575   0.0139   0.8834
  12.750   1.5210   0.02516   0.01899  -0.0556   0.0123   0.9006
  13.000   1.5256   0.02606   0.02002  -0.0528   0.0110   0.9505
  13.250   1.5363   0.02713   0.02116  -0.0514   0.0100   1.0000
  13.500   1.5458   0.02834   0.02242  -0.0500   0.0090   1.0000
  13.750   1.5545   0.02966   0.02378  -0.0486   0.0082   1.0000
  14.000   1.5633   0.03099   0.02517  -0.0474   0.0074   1.0000
  14.250   1.5708   0.03247   0.02671  -0.0461   0.0067   1.0000
  14.500   1.5773   0.03407   0.02837  -0.0449   0.0062   1.0000
  14.750   1.5842   0.03569   0.03006  -0.0438   0.0057   1.0000
  15.000   1.5894   0.03750   0.03193  -0.0428   0.0051   1.0000
  15.250   1.5937   0.03947   0.03398  -0.0418   0.0046   1.0000
  15.500   1.5975   0.04156   0.03614  -0.0410   0.0042   1.0000
  15.750   1.6012   0.04372   0.03839  -0.0404   0.0039   1.0000
  16.000   1.6027   0.04619   0.04094  -0.0398   0.0034   1.0000
  16.250   1.6028   0.04892   0.04375  -0.0394   0.0030   1.0000
  16.500   1.6028   0.05177   0.04669  -0.0393   0.0026   1.0000
  16.750   1.6016   0.05487   0.04988  -0.0393   0.0023   1.0000
  17.000   1.5985   0.05835   0.05345  -0.0396   0.0020   1.0000
  17.250   1.5954   0.06198   0.05719  -0.0401   0.0019   1.0000
  17.500   1.5911   0.06592   0.06124  -0.0409   0.0017   1.0000
  17.750   1.5846   0.07033   0.06576  -0.0421   0.0015   1.0000
  18.000   1.5785   0.07486   0.07041  -0.0435   0.0014   1.0000
  18.250   1.5674   0.08034   0.07601  -0.0454   0.0012   1.0000
  18.500   1.5558   0.08610   0.08190  -0.0477   0.0011   1.0000
  18.750   1.5450   0.09190   0.08783  -0.0502   0.0011   1.0000
  19.000   1.5320   0.09826   0.09433  -0.0531   0.0010   1.0000
  19.250   1.5173   0.10511   0.10131  -0.0565   0.0010   1.0000
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