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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 200,000
Max Cl/Cd: 45.87 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh94-il-200000-n5.txt
Download as CSV file: xf-mh94-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 94  16.03%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6610   0.11895   0.11421  -0.0469   1.0000   0.0147
 -16.500  -0.7018   0.10613   0.10116  -0.0541   1.0000   0.0146
 -16.250  -0.7336   0.09620   0.09099  -0.0595   1.0000   0.0146
 -16.000  -0.7527   0.08936   0.08398  -0.0629   1.0000   0.0145
 -15.750  -0.7713   0.08302   0.07746  -0.0659   1.0000   0.0144
 -15.500  -0.7859   0.07766   0.07193  -0.0682   1.0000   0.0144
 -15.250  -0.8006   0.07258   0.06667  -0.0700   1.0000   0.0144
 -15.000  -0.8115   0.06832   0.06225  -0.0712   1.0000   0.0144
 -14.750  -0.8223   0.06431   0.05806  -0.0721   1.0000   0.0146
 -14.500  -0.8302   0.06086   0.05445  -0.0724   1.0000   0.0147
 -14.250  -0.8369   0.05772   0.05115  -0.0724   1.0000   0.0148
 -14.000  -0.8414   0.05495   0.04824  -0.0721   1.0000   0.0148
 -13.750  -0.8444   0.05245   0.04560  -0.0715   1.0000   0.0149
 -13.500  -0.8463   0.05014   0.04315  -0.0706   1.0000   0.0150
 -13.250  -0.8472   0.04802   0.04090  -0.0695   1.0000   0.0151
 -13.000  -0.8473   0.04604   0.03882  -0.0683   1.0000   0.0152
 -12.750  -0.8461   0.04430   0.03703  -0.0668   1.0000   0.0153
 -12.500  -0.8450   0.04264   0.03533  -0.0653   1.0000   0.0155
 -12.250  -0.8440   0.04107   0.03372  -0.0636   1.0000   0.0156
 -12.000  -0.8431   0.03957   0.03217  -0.0617   1.0000   0.0158
 -11.750  -0.8425   0.03815   0.03070  -0.0597   1.0000   0.0160
 -11.500  -0.8417   0.03682   0.02932  -0.0575   1.0000   0.0161
 -11.250  -0.8420   0.03550   0.02796  -0.0550   1.0000   0.0164
 -11.000  -0.8422   0.03430   0.02669  -0.0524   1.0000   0.0165
 -10.750  -0.8435   0.03314   0.02548  -0.0494   1.0000   0.0167
 -10.500  -0.8460   0.03202   0.02431  -0.0462   1.0000   0.0171
 -10.250  -0.8496   0.03099   0.02322  -0.0427   1.0000   0.0173
 -10.000  -0.8549   0.03005   0.02221  -0.0387   1.0000   0.0176
  -9.750  -0.8390   0.02889   0.02097  -0.0387   0.9969   0.0179
  -9.500  -0.8205   0.02779   0.01981  -0.0392   0.9933   0.0184
  -9.250  -0.8053   0.02684   0.01883  -0.0386   0.9885   0.0190
  -9.000  -0.7841   0.02594   0.01787  -0.0389   0.9846   0.0198
  -8.750  -0.7619   0.02505   0.01691  -0.0392   0.9810   0.0207
  -8.500  -0.7429   0.02420   0.01601  -0.0387   0.9759   0.0217
  -8.250  -0.7174   0.02344   0.01522  -0.0393   0.9724   0.0233
  -8.000  -0.6935   0.02270   0.01443  -0.0395   0.9686   0.0254
  -7.750  -0.6735   0.02201   0.01372  -0.0388   0.9630   0.0277
  -7.500  -0.6471   0.02126   0.01294  -0.0393   0.9594   0.0309
  -7.250  -0.6173   0.02054   0.01221  -0.0405   0.9569   0.0355
  -7.000  -0.6025   0.01994   0.01161  -0.0384   0.9495   0.0409
  -6.750  -0.5759   0.01923   0.01096  -0.0389   0.9456   0.0517
  -6.500  -0.5463   0.01847   0.01030  -0.0399   0.9430   0.0711
  -6.250  -0.5320   0.01778   0.00976  -0.0378   0.9352   0.0955
  -6.000  -0.5078   0.01682   0.00911  -0.0380   0.9308   0.1484
  -5.750  -0.4798   0.01586   0.00850  -0.0390   0.9280   0.2167
  -5.500  -0.4656   0.01519   0.00810  -0.0368   0.9197   0.2710
  -5.250  -0.4383   0.01455   0.00772  -0.0371   0.9155   0.3279
  -5.000  -0.4062   0.01407   0.00741  -0.0382   0.9127   0.3747
  -4.750  -0.3855   0.01377   0.00722  -0.0368   0.9054   0.4088
  -4.500  -0.3568   0.01346   0.00702  -0.0370   0.9005   0.4452
  -4.250  -0.3236   0.01318   0.00682  -0.0379   0.8974   0.4795
  -4.000  -0.2875   0.01293   0.00662  -0.0394   0.8952   0.5025
  -3.500  -0.2341   0.01261   0.00628  -0.0385   0.8816   0.5299
  -3.250  -0.1959   0.01239   0.00606  -0.0403   0.8787   0.5425
  -3.000  -0.1743   0.01230   0.00592  -0.0389   0.8688   0.5540
  -2.750  -0.1384   0.01210   0.00575  -0.0402   0.8640   0.5653
  -2.500  -0.1062   0.01196   0.00558  -0.0408   0.8573   0.5764
  -2.250  -0.0764   0.01182   0.00544  -0.0409   0.8486   0.5876
  -2.000  -0.0371   0.01163   0.00524  -0.0429   0.8432   0.5979
  -1.750  -0.0106   0.01155   0.00513  -0.0424   0.8313   0.6080
  -1.500   0.0246   0.01141   0.00499  -0.0435   0.8223   0.6166
  -1.250   0.0571   0.01130   0.00484  -0.0442   0.8106   0.6262
  -1.000   0.0881   0.01121   0.00475  -0.0445   0.7975   0.6342
  -0.750   0.1209   0.01114   0.00463  -0.0452   0.7835   0.6430
  -0.500   0.1530   0.01108   0.00452  -0.0458   0.7680   0.6511
  -0.250   0.1835   0.01106   0.00445  -0.0460   0.7509   0.6590
   0.000   0.2130   0.01106   0.00437  -0.0461   0.7328   0.6677
   0.250   0.2409   0.01109   0.00436  -0.0458   0.7136   0.6747
   0.500   0.2682   0.01114   0.00434  -0.0454   0.6937   0.6829
   0.750   0.2946   0.01121   0.00434  -0.0449   0.6730   0.6903
   1.000   0.3202   0.01130   0.00437  -0.0442   0.6513   0.6978
   1.250   0.3455   0.01141   0.00438  -0.0435   0.6288   0.7064
   1.500   0.3694   0.01154   0.00445  -0.0425   0.6053   0.7128
   1.750   0.3928   0.01169   0.00450  -0.0414   0.5799   0.7209
   2.000   0.4152   0.01186   0.00456  -0.0402   0.5515   0.7282
   2.250   0.4362   0.01207   0.00466  -0.0387   0.5204   0.7353
   2.500   0.4567   0.01231   0.00474  -0.0372   0.4886   0.7435
   2.750   0.4767   0.01255   0.00487  -0.0355   0.4575   0.7503
   3.000   0.4971   0.01280   0.00502  -0.0340   0.4293   0.7579
   3.250   0.5176   0.01307   0.00515  -0.0326   0.4021   0.7660
   3.500   0.5373   0.01333   0.00535  -0.0309   0.3772   0.7729
   3.750   0.5579   0.01360   0.00552  -0.0296   0.3532   0.7811
   4.000   0.5779   0.01387   0.00572  -0.0281   0.3308   0.7885
   4.250   0.5975   0.01415   0.00593  -0.0265   0.3101   0.7964
   4.500   0.6178   0.01444   0.00615  -0.0252   0.2909   0.8048
   4.750   0.6367   0.01473   0.00639  -0.0235   0.2725   0.8124
   5.000   0.6564   0.01503   0.00662  -0.0220   0.2552   0.8216
   5.250   0.6742   0.01531   0.00688  -0.0201   0.2387   0.8295
   5.500   0.6928   0.01559   0.00713  -0.0185   0.2239   0.8390
   5.750   0.7103   0.01587   0.00740  -0.0165   0.2103   0.8478
   6.000   0.7281   0.01619   0.00768  -0.0148   0.1972   0.8580
   6.250   0.7445   0.01653   0.00800  -0.0127   0.1850   0.8681
   6.500   0.7615   0.01688   0.00833  -0.0108   0.1733   0.8796
   6.750   0.7784   0.01721   0.00866  -0.0089   0.1629   0.8918
   7.000   0.7948   0.01758   0.00903  -0.0069   0.1543   0.9057
   7.250   0.8127   0.01795   0.00940  -0.0053   0.1462   0.9214
   7.500   0.8334   0.01836   0.00983  -0.0044   0.1392   0.9402
   7.750   0.8606   0.01885   0.01032  -0.0049   0.1320   0.9624
   8.000   0.8872   0.01934   0.01080  -0.0055   0.1264   1.0000
   8.250   0.9062   0.01983   0.01128  -0.0045   0.1219   1.0000
   8.500   0.9236   0.02039   0.01181  -0.0033   0.1181   1.0000
   8.750   0.9408   0.02097   0.01238  -0.0021   0.1150   1.0000
   9.000   0.9592   0.02150   0.01295  -0.0011   0.1119   1.0000
   9.250   0.9764   0.02209   0.01355   0.0001   0.1089   1.0000
   9.500   0.9921   0.02276   0.01420   0.0014   0.1064   1.0000
   9.750   1.0067   0.02352   0.01493   0.0028   0.1042   1.0000
  10.000   1.0239   0.02414   0.01562   0.0039   0.1022   1.0000
  10.250   1.0401   0.02483   0.01636   0.0051   0.1002   1.0000
  10.500   1.0556   0.02556   0.01713   0.0063   0.0984   1.0000
  10.750   1.0704   0.02634   0.01793   0.0075   0.0967   1.0000
  11.000   1.0839   0.02721   0.01881   0.0087   0.0952   1.0000
  11.250   1.0965   0.02821   0.01977   0.0100   0.0936   1.0000
  11.500   1.1117   0.02902   0.02068   0.0111   0.0922   1.0000
  11.750   1.1261   0.02990   0.02165   0.0121   0.0908   1.0000
  12.000   1.1398   0.03084   0.02266   0.0131   0.0894   1.0000
  12.250   1.1530   0.03184   0.02372   0.0142   0.0882   1.0000
  12.500   1.1656   0.03289   0.02481   0.0152   0.0871   1.0000
  12.750   1.1776   0.03399   0.02596   0.0161   0.0860   1.0000
  13.000   1.1890   0.03517   0.02717   0.0170   0.0849   1.0000
  13.250   1.2006   0.03644   0.02842   0.0179   0.0838   1.0000
  13.500   1.2117   0.03769   0.02979   0.0187   0.0828   1.0000
  13.750   1.2222   0.03900   0.03123   0.0195   0.0819   1.0000
  14.000   1.2319   0.04041   0.03275   0.0202   0.0808   1.0000
  14.250   1.2411   0.04189   0.03433   0.0208   0.0799   1.0000
  14.500   1.2498   0.04343   0.03597   0.0214   0.0790   1.0000
  14.750   1.2578   0.04506   0.03768   0.0219   0.0782   1.0000
  15.000   1.2651   0.04675   0.03945   0.0223   0.0773   1.0000
  15.250   1.2724   0.04850   0.04126   0.0226   0.0765   1.0000
  15.500   1.2793   0.05031   0.04313   0.0228   0.0757   1.0000
  15.750   1.2879   0.05208   0.04491   0.0230   0.0749   1.0000
  16.000   1.2913   0.05436   0.04733   0.0231   0.0743   1.0000
  16.250   1.2919   0.05697   0.05013   0.0229   0.0736   1.0000
  16.500   1.2917   0.05977   0.05310   0.0225   0.0730   1.0000
  16.750   1.2898   0.06282   0.05632   0.0220   0.0722   1.0000
  17.000   1.2877   0.06602   0.05968   0.0212   0.0715   1.0000
  17.250   1.2842   0.06947   0.06327   0.0201   0.0708   1.0000
  17.500   1.2804   0.07307   0.06701   0.0189   0.0701   1.0000
  17.750   1.2765   0.07680   0.07087   0.0174   0.0694   1.0000
  18.000   1.2728   0.08059   0.07477   0.0158   0.0688   1.0000
  18.250   1.2694   0.08442   0.07871   0.0141   0.0682   1.0000
  18.500   1.2668   0.08821   0.08258   0.0124   0.0677   1.0000
  18.750   1.2675   0.09152   0.08595   0.0109   0.0671   1.0000
  19.000   1.2604   0.09616   0.09070   0.0086   0.0665   1.0000
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