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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.9 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh104-il-1000000-n5.txt
Download as CSV file: xf-mh104-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 104  15.28%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9670   0.08448   0.08137  -0.0175   1.0000   0.0030
 -16.250  -0.9828   0.07797   0.07475  -0.0211   1.0000   0.0030
 -16.000  -1.0008   0.07137   0.06804  -0.0247   1.0000   0.0030
 -15.750  -1.0232   0.06433   0.06087  -0.0285   1.0000   0.0030
 -15.500  -1.0363   0.05878   0.05519  -0.0315   1.0000   0.0030
 -15.250  -1.0496   0.05332   0.04962  -0.0345   1.0000   0.0030
 -15.000  -1.0561   0.04894   0.04514  -0.0368   1.0000   0.0030
 -14.750  -1.0666   0.04420   0.04027  -0.0392   1.0000   0.0030
 -14.500  -1.0757   0.03996   0.03589  -0.0410   1.0000   0.0030
 -14.250  -1.0759   0.03707   0.03291  -0.0419   1.0000   0.0030
 -14.000  -1.0792   0.03416   0.02989  -0.0424   1.0000   0.0030
 -13.750  -1.0806   0.03176   0.02739  -0.0422   1.0000   0.0030
 -13.500  -1.0874   0.02923   0.02473  -0.0412   1.0000   0.0030
 -13.250  -1.0807   0.02794   0.02338  -0.0401   1.0000   0.0030
 -13.000  -1.0775   0.02654   0.02190  -0.0385   1.0000   0.0030
 -12.750  -1.0743   0.02526   0.02053  -0.0364   1.0000   0.0030
 -12.500  -1.0693   0.02416   0.01936  -0.0341   1.0000   0.0030
 -12.250  -1.0672   0.02299   0.01810  -0.0311   1.0000   0.0031
 -12.000  -1.0641   0.02194   0.01696  -0.0279   1.0000   0.0031
 -11.750  -1.0416   0.02101   0.01582  -0.0281   0.8982   0.0031
 -11.500  -1.0365   0.02051   0.01505  -0.0244   0.8390   0.0032
 -11.250  -1.0254   0.01979   0.01415  -0.0219   0.8076   0.0032
 -11.000  -1.0115   0.01911   0.01332  -0.0199   0.7831   0.0033
 -10.750  -0.9951   0.01848   0.01257  -0.0182   0.7618   0.0034
 -10.500  -0.9764   0.01798   0.01195  -0.0168   0.7428   0.0034
 -10.250  -0.9572   0.01745   0.01132  -0.0155   0.7262   0.0035
 -10.000  -0.9366   0.01699   0.01077  -0.0144   0.7107   0.0036
  -9.750  -0.9158   0.01651   0.01020  -0.0133   0.6964   0.0037
  -9.500  -0.8938   0.01610   0.00970  -0.0124   0.6825   0.0038
  -9.250  -0.8719   0.01566   0.00917  -0.0114   0.6697   0.0039
  -9.000  -0.8492   0.01526   0.00870  -0.0106   0.6579   0.0041
  -8.750  -0.8262   0.01486   0.00821  -0.0097   0.6461   0.0042
  -8.500  -0.8028   0.01448   0.00775  -0.0090   0.6346   0.0043
  -8.250  -0.7790   0.01413   0.00732  -0.0083   0.6229   0.0045
  -7.750  -0.7304   0.01346   0.00651  -0.0070   0.6023   0.0048
  -7.500  -0.7060   0.01311   0.00610  -0.0063   0.5931   0.0052
  -7.250  -0.6810   0.01281   0.00575  -0.0058   0.5834   0.0056
  -7.000  -0.6556   0.01255   0.00543  -0.0053   0.5740   0.0061
  -6.750  -0.6300   0.01231   0.00513  -0.0048   0.5641   0.0068
  -6.500  -0.6045   0.01203   0.00482  -0.0044   0.5547   0.0080
  -6.250  -0.5786   0.01180   0.00454  -0.0040   0.5464   0.0094
  -6.000  -0.5526   0.01157   0.00428  -0.0036   0.5381   0.0118
  -5.750  -0.5266   0.01133   0.00403  -0.0032   0.5306   0.0155
  -5.500  -0.5004   0.01110   0.00380  -0.0028   0.5225   0.0202
  -5.250  -0.4743   0.01088   0.00356  -0.0024   0.5149   0.0262
  -5.000  -0.4482   0.01064   0.00333  -0.0021   0.5067   0.0359
  -4.750  -0.4230   0.01031   0.00307  -0.0016   0.4995   0.0561
  -4.500  -0.3989   0.00984   0.00278  -0.0010   0.4925   0.0957
  -4.250  -0.3751   0.00937   0.00251  -0.0003   0.4863   0.1465
  -4.000  -0.3498   0.00903   0.00232   0.0002   0.4803   0.1866
  -3.750  -0.3235   0.00883   0.00219   0.0005   0.4738   0.2117
  -3.500  -0.2965   0.00869   0.00208   0.0007   0.4681   0.2318
  -3.250  -0.2699   0.00850   0.00197   0.0010   0.4616   0.2595
  -3.000  -0.2430   0.00837   0.00188   0.0012   0.4557   0.2810
  -2.750  -0.2153   0.00828   0.00181   0.0013   0.4503   0.2946
  -2.500  -0.1876   0.00821   0.00174   0.0014   0.4450   0.3069
  -2.250  -0.1600   0.00815   0.00168   0.0016   0.4401   0.3196
  -2.000  -0.1321   0.00808   0.00162   0.0016   0.4359   0.3319
  -1.750  -0.1043   0.00802   0.00158   0.0017   0.4311   0.3445
  -1.500  -0.0765   0.00799   0.00154   0.0018   0.4262   0.3569
  -1.000  -0.0207   0.00788   0.00147   0.0020   0.4178   0.3842
  -0.750   0.0071   0.00784   0.00145   0.0020   0.4137   0.3983
  -0.500   0.0348   0.00781   0.00143   0.0021   0.4099   0.4134
  -0.250   0.0628   0.00776   0.00142   0.0022   0.4068   0.4278
   0.000   0.0906   0.00772   0.00141   0.0023   0.4030   0.4447
   0.250   0.1183   0.00768   0.00141   0.0023   0.3991   0.4616
   0.500   0.1459   0.00766   0.00142   0.0024   0.3955   0.4785
   0.750   0.1736   0.00761   0.00142   0.0025   0.3926   0.4983
   1.000   0.2012   0.00756   0.00143   0.0026   0.3892   0.5198
   1.250   0.2286   0.00752   0.00145   0.0028   0.3856   0.5423
   1.500   0.2557   0.00748   0.00148   0.0030   0.3820   0.5685
   1.750   0.2828   0.00744   0.00151   0.0031   0.3787   0.5950
   2.250   0.3367   0.00733   0.00159   0.0036   0.3724   0.6544
   2.500   0.3632   0.00729   0.00163   0.0039   0.3690   0.6862
   2.750   0.3894   0.00726   0.00169   0.0043   0.3654   0.7173
   3.000   0.4156   0.00721   0.00175   0.0047   0.3626   0.7498
   3.250   0.4417   0.00715   0.00181   0.0051   0.3595   0.7829
   3.500   0.4677   0.00712   0.00188   0.0056   0.3562   0.8146
   3.750   0.4938   0.00710   0.00197   0.0061   0.3526   0.8464
   4.000   0.5205   0.00711   0.00207   0.0064   0.3490   0.8769
   4.250   0.5499   0.00712   0.00217   0.0062   0.3459   0.9039
   4.500   0.5825   0.00718   0.00229   0.0052   0.3418   0.9254
   4.750   0.6179   0.00730   0.00242   0.0036   0.3371   0.9404
   5.000   0.6545   0.00742   0.00255   0.0017   0.3326   0.9501
   5.250   0.6893   0.00753   0.00266   0.0002   0.3275   0.9573
   5.500   0.7237   0.00767   0.00279  -0.0013   0.3217   0.9630
   5.750   0.7533   0.00780   0.00292  -0.0017   0.3164   0.9695
   6.000   0.7877   0.00794   0.00306  -0.0032   0.3091   0.9727
   6.250   0.8196   0.00810   0.00320  -0.0042   0.3029   0.9768
   6.500   0.8478   0.00826   0.00336  -0.0043   0.2952   0.9821
   6.750   0.8849   0.00846   0.00353  -0.0065   0.2856   0.9844
   7.000   0.9206   0.00869   0.00373  -0.0083   0.2745   0.9872
   7.250   0.9533   0.00892   0.00393  -0.0096   0.2628   0.9899
   7.500   0.9835   0.00920   0.00416  -0.0104   0.2498   0.9923
   7.750   1.0144   0.00949   0.00441  -0.0114   0.2365   0.9941
   8.000   1.0467   0.00980   0.00468  -0.0127   0.2231   0.9956
   8.250   1.0783   0.01015   0.00497  -0.0140   0.2090   0.9973
   8.500   1.1093   0.01054   0.00530  -0.0151   0.1942   0.9989
   8.750   1.1390   0.01097   0.00567  -0.0161   0.1791   1.0000
   9.000   1.1580   0.01138   0.00603  -0.0147   0.1660   1.0000
   9.250   1.1761   0.01184   0.00643  -0.0133   0.1520   1.0000
   9.500   1.1937   0.01230   0.00684  -0.0118   0.1393   1.0000
   9.750   1.2099   0.01283   0.00731  -0.0101   0.1255   1.0000
  10.000   1.2251   0.01339   0.00780  -0.0082   0.1122   1.0000
  10.250   1.2411   0.01387   0.00826  -0.0065   0.1031   1.0000
  10.500   1.2553   0.01442   0.00877  -0.0046   0.0938   1.0000
  10.750   1.2688   0.01496   0.00928  -0.0025   0.0858   1.0000
  11.000   1.2813   0.01551   0.00982  -0.0003   0.0779   1.0000
  11.250   1.2916   0.01612   0.01042   0.0021   0.0712   1.0000
  11.500   1.2959   0.01683   0.01111   0.0055   0.0635   1.0000
  11.750   1.2968   0.01753   0.01181   0.0093   0.0577   1.0000
  12.000   1.2953   0.01863   0.01288   0.0126   0.0500   1.0000
  12.250   1.2957   0.01999   0.01424   0.0148   0.0433   1.0000
  12.500   1.2969   0.02162   0.01587   0.0162   0.0366   1.0000
  12.750   1.3012   0.02326   0.01754   0.0170   0.0330   1.0000
  13.000   1.3028   0.02530   0.01959   0.0176   0.0286   1.0000
  13.250   1.3063   0.02729   0.02163   0.0179   0.0258   1.0000
  13.500   1.3063   0.02973   0.02410   0.0180   0.0226   1.0000
  13.750   1.3050   0.03236   0.02677   0.0180   0.0192   1.0000
  14.000   1.3061   0.03481   0.02927   0.0179   0.0181   1.0000
  14.250   1.3034   0.03768   0.03218   0.0177   0.0155   1.0000
  14.500   1.3036   0.04030   0.03486   0.0175   0.0147   1.0000
  14.750   1.2989   0.04343   0.03804   0.0171   0.0129   1.0000
  15.000   1.2977   0.04625   0.04093   0.0168   0.0124   1.0000
  15.250   1.2940   0.04937   0.04411   0.0163   0.0115   1.0000
  15.500   1.2906   0.05258   0.04738   0.0158   0.0108   1.0000
  15.750   1.2872   0.05586   0.05072   0.0151   0.0098   1.0000
  16.000   1.2842   0.05914   0.05406   0.0144   0.0093   1.0000
  16.250   1.2784   0.06281   0.05779   0.0135   0.0084   1.0000
  16.500   1.2761   0.06610   0.06115   0.0127   0.0080   1.0000
  16.750   1.2735   0.06948   0.06460   0.0119   0.0078   1.0000
  17.000   1.2692   0.07312   0.06830   0.0109   0.0072   1.0000
  17.250   1.2655   0.07673   0.07198   0.0099   0.0068   1.0000
  17.500   1.2609   0.08048   0.07578   0.0088   0.0065   1.0000
  17.750   1.2557   0.08436   0.07973   0.0076   0.0062   1.0000
  18.000   1.2520   0.08808   0.08352   0.0065   0.0059   1.0000
  18.250   1.2475   0.09195   0.08746   0.0053   0.0056   1.0000
  18.500   1.2421   0.09596   0.09154   0.0040   0.0053   1.0000
  18.750   1.2366   0.10004   0.09568   0.0026   0.0049   1.0000
  19.000   1.2316   0.10412   0.09983   0.0012   0.0048   1.0000
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