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MH 70 11.08% (mh70-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 70 11.08% (mh70-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.84 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh70-il-1000000-n5.txt
Download as CSV file: xf-mh70-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 70  11.08%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.4136   0.11259   0.11090  -0.0144   1.0000   0.0041
 -10.500  -0.7039   0.03552   0.03320  -0.0642   0.9182   0.0028
 -10.250  -0.7242   0.02986   0.02695  -0.0630   0.8831   0.0029
  -9.750  -0.7100   0.02434   0.02069  -0.0609   0.8522   0.0029
  -9.500  -0.6946   0.02242   0.01847  -0.0600   0.8410   0.0029
  -9.250  -0.6764   0.02089   0.01669  -0.0593   0.8309   0.0029
  -9.000  -0.6560   0.01963   0.01521  -0.0586   0.8210   0.0030
  -8.750  -0.6345   0.01848   0.01385  -0.0580   0.8125   0.0030
  -8.500  -0.6113   0.01765   0.01286  -0.0575   0.8036   0.0030
  -8.250  -0.5880   0.01671   0.01175  -0.0570   0.7959   0.0031
  -8.000  -0.5671   0.01520   0.00996  -0.0562   0.7874   0.0033
  -7.750  -0.5425   0.01446   0.00910  -0.0558   0.7800   0.0034
  -7.500  -0.5168   0.01396   0.00851  -0.0555   0.7721   0.0035
  -7.250  -0.4909   0.01346   0.00791  -0.0552   0.7653   0.0036
  -7.000  -0.4647   0.01303   0.00739  -0.0549   0.7578   0.0038
  -6.750  -0.4383   0.01260   0.00688  -0.0546   0.7511   0.0039
  -6.500  -0.4118   0.01217   0.00637  -0.0544   0.7438   0.0041
  -6.250  -0.3852   0.01177   0.00588  -0.0541   0.7371   0.0042
  -6.000  -0.3582   0.01140   0.00544  -0.0539   0.7302   0.0044
  -5.750  -0.3313   0.01107   0.00503  -0.0536   0.7232   0.0045
  -5.500  -0.3041   0.01073   0.00462  -0.0534   0.7166   0.0046
  -5.250  -0.2767   0.01045   0.00428  -0.0532   0.7095   0.0047
  -5.000  -0.2494   0.01015   0.00392  -0.0531   0.7030   0.0049
  -4.750  -0.2220   0.00983   0.00354  -0.0529   0.6959   0.0051
  -4.500  -0.1944   0.00959   0.00324  -0.0527   0.6892   0.0054
  -4.250  -0.1666   0.00936   0.00298  -0.0526   0.6819   0.0058
  -4.000  -0.1388   0.00919   0.00276  -0.0525   0.6746   0.0063
  -3.750  -0.1108   0.00900   0.00253  -0.0524   0.6673   0.0071
  -3.250  -0.0550   0.00865   0.00213  -0.0521   0.6515   0.0106
  -3.000  -0.0272   0.00850   0.00195  -0.0520   0.6431   0.0149
  -2.750   0.0009   0.00834   0.00180  -0.0519   0.6344   0.0221
  -2.500   0.0288   0.00820   0.00167  -0.0519   0.6258   0.0319
  -2.250   0.0565   0.00799   0.00153  -0.0518   0.6162   0.0564
  -2.000   0.0840   0.00773   0.00140  -0.0517   0.6068   0.0991
  -1.750   0.1114   0.00750   0.00130  -0.0516   0.5967   0.1485
  -1.500   0.1390   0.00732   0.00122  -0.0516   0.5857   0.1930
  -1.250   0.1669   0.00720   0.00117  -0.0515   0.5745   0.2280
  -1.000   0.1943   0.00704   0.00112  -0.0515   0.5624   0.2820
  -0.750   0.2219   0.00692   0.00109  -0.0514   0.5499   0.3291
  -0.500   0.2496   0.00684   0.00107  -0.0513   0.5364   0.3691
  -0.250   0.2773   0.00677   0.00106  -0.0513   0.5227   0.4105
   0.000   0.3049   0.00671   0.00107  -0.0512   0.5087   0.4525
   0.250   0.3324   0.00666   0.00108  -0.0511   0.4944   0.4965
   0.500   0.3598   0.00661   0.00110  -0.0510   0.4805   0.5426
   0.750   0.3870   0.00656   0.00113  -0.0509   0.4668   0.5938
   1.000   0.4140   0.00650   0.00118  -0.0507   0.4524   0.6504
   1.250   0.4406   0.00645   0.00123  -0.0504   0.4384   0.7082
   1.500   0.4667   0.00640   0.00130  -0.0499   0.4236   0.7694
   1.750   0.4921   0.00636   0.00138  -0.0493   0.4094   0.8277
   2.000   0.5169   0.00636   0.00147  -0.0485   0.3951   0.8796
   2.250   0.5417   0.00640   0.00155  -0.0476   0.3807   0.9240
   2.500   0.5715   0.00651   0.00163  -0.0479   0.3652   0.9582
   2.750   0.6075   0.00666   0.00171  -0.0497   0.3490   0.9790
   3.000   0.6431   0.00683   0.00181  -0.0514   0.3327   0.9925
   3.250   0.6754   0.00701   0.00190  -0.0525   0.3180   1.0000
   3.500   0.7012   0.00719   0.00201  -0.0521   0.3039   1.0000
   4.000   0.7531   0.00757   0.00226  -0.0514   0.2766   1.0000
   4.250   0.7792   0.00777   0.00239  -0.0511   0.2633   1.0000
   4.500   0.8055   0.00795   0.00253  -0.0508   0.2525   1.0000
   4.750   0.8317   0.00816   0.00269  -0.0506   0.2411   1.0000
   5.000   0.8576   0.00839   0.00285  -0.0503   0.2289   1.0000
   5.250   0.8838   0.00859   0.00301  -0.0500   0.2184   1.0000
   5.500   0.9098   0.00881   0.00319  -0.0498   0.2075   1.0000
   5.750   0.9358   0.00904   0.00338  -0.0495   0.1977   1.0000
   6.000   0.9616   0.00928   0.00357  -0.0492   0.1883   1.0000
   6.250   0.9875   0.00951   0.00378  -0.0490   0.1789   1.0000
   6.500   1.0131   0.00977   0.00400  -0.0487   0.1703   1.0000
   6.750   1.0385   0.01004   0.00422  -0.0484   0.1606   1.0000
   7.000   1.0641   0.01028   0.00446  -0.0481   0.1530   1.0000
   7.250   1.0889   0.01059   0.00472  -0.0477   0.1440   1.0000
   7.500   1.1143   0.01084   0.00496  -0.0474   0.1372   1.0000
   7.750   1.1389   0.01115   0.00524  -0.0470   0.1295   1.0000
   8.000   1.1634   0.01146   0.00553  -0.0466   0.1216   1.0000
   8.250   1.1878   0.01177   0.00583  -0.0462   0.1147   1.0000
   8.500   1.2116   0.01211   0.00615  -0.0458   0.1076   1.0000
   8.750   1.2356   0.01244   0.00647  -0.0453   0.1013   1.0000
   9.000   1.2586   0.01283   0.00683  -0.0447   0.0943   1.0000
   9.250   1.2819   0.01317   0.00718  -0.0442   0.0886   1.0000
   9.500   1.3039   0.01361   0.00759  -0.0435   0.0814   1.0000
   9.750   1.3262   0.01400   0.00798  -0.0428   0.0757   1.0000
  10.000   1.3474   0.01446   0.00841  -0.0420   0.0698   1.0000
  10.250   1.3688   0.01486   0.00884  -0.0412   0.0655   1.0000
  10.500   1.3885   0.01537   0.00933  -0.0402   0.0598   1.0000
  10.750   1.4081   0.01585   0.00982  -0.0392   0.0550   1.0000
  11.000   1.4259   0.01642   0.01037  -0.0380   0.0495   1.0000
  11.250   1.4430   0.01698   0.01094  -0.0367   0.0453   1.0000
  11.500   1.4579   0.01754   0.01152  -0.0350   0.0415   1.0000
  11.750   1.4701   0.01812   0.01211  -0.0328   0.0383   1.0000
  12.000   1.4804   0.01881   0.01282  -0.0305   0.0351   1.0000
  12.250   1.4911   0.01952   0.01355  -0.0285   0.0320   1.0000
  12.500   1.5001   0.02039   0.01444  -0.0264   0.0293   1.0000
  12.750   1.5091   0.02131   0.01538  -0.0246   0.0262   1.0000
  13.000   1.5165   0.02240   0.01649  -0.0228   0.0231   1.0000
  13.250   1.5259   0.02343   0.01757  -0.0213   0.0216   1.0000
  13.500   1.5325   0.02472   0.01889  -0.0198   0.0195   1.0000
  13.750   1.5385   0.02612   0.02032  -0.0185   0.0169   1.0000
  14.000   1.5458   0.02749   0.02175  -0.0174   0.0161   1.0000
  14.250   1.5514   0.02906   0.02336  -0.0163   0.0143   1.0000
  14.500   1.5537   0.03098   0.02532  -0.0153   0.0125   1.0000
  14.750   1.5582   0.03279   0.02721  -0.0145   0.0112   1.0000
  15.000   1.5595   0.03497   0.02944  -0.0139   0.0099   1.0000
  15.250   1.5624   0.03709   0.03162  -0.0134   0.0092   1.0000
  15.500   1.5649   0.03931   0.03393  -0.0131   0.0088   1.0000
  15.750   1.5646   0.04191   0.03660  -0.0129   0.0080   1.0000
  16.000   1.5632   0.04473   0.03950  -0.0130   0.0074   1.0000
  16.250   1.5624   0.04758   0.04244  -0.0132   0.0071   1.0000
  16.500   1.5597   0.05081   0.04575  -0.0137   0.0065   1.0000
  16.750   1.5552   0.05439   0.04942  -0.0144   0.0061   1.0000
  17.000   1.5502   0.05819   0.05333  -0.0153   0.0059   1.0000
  17.250   1.5445   0.06224   0.05748  -0.0165   0.0057   1.0000
  17.500   1.5358   0.06685   0.06220  -0.0181   0.0050   1.0000
  17.750   1.5296   0.07126   0.06672  -0.0197   0.0051   1.0000
  18.000   1.5191   0.07644   0.07201  -0.0218   0.0049   1.0000
  18.250   1.5075   0.08196   0.07765  -0.0241   0.0047   1.0000
  18.500   1.4947   0.08782   0.08362  -0.0267   0.0045   1.0000
  18.750   1.4795   0.09426   0.09019  -0.0297   0.0043   1.0000
  19.000   1.4641   0.10086   0.09690  -0.0329   0.0042   1.0000
  19.250   1.4483   0.10772   0.10389  -0.0363   0.0042   1.0000
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