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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.98 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh93-il-1000000.txt
Download as CSV file: xf-mh93-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 93  15.98%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.9440   0.10248   0.09990   0.0052   1.0000   0.0077
 -16.500  -0.9744   0.09188   0.08911  -0.0015   1.0000   0.0076
 -16.250  -0.9995   0.08291   0.07996  -0.0071   1.0000   0.0076
 -16.000  -1.0197   0.07540   0.07228  -0.0115   1.0000   0.0075
 -15.750  -1.0398   0.06836   0.06505  -0.0153   1.0000   0.0075
 -15.500  -1.0517   0.06306   0.05961  -0.0178   1.0000   0.0075
 -15.250  -1.0610   0.05843   0.05485  -0.0197   1.0000   0.0075
 -15.000  -1.0722   0.05384   0.05009  -0.0212   1.0000   0.0075
 -14.750  -1.0807   0.04989   0.04600  -0.0220   1.0000   0.0075
 -14.500  -1.0878   0.04631   0.04226  -0.0224   1.0000   0.0074
 -14.250  -1.0922   0.04323   0.03905  -0.0222   1.0000   0.0074
 -14.000  -1.0934   0.04062   0.03633  -0.0218   1.0000   0.0074
 -13.750  -1.0943   0.03814   0.03372  -0.0210   1.0000   0.0074
 -13.500  -1.0932   0.03595   0.03142  -0.0200   1.0000   0.0074
 -13.250  -1.0898   0.03405   0.02942  -0.0189   1.0000   0.0074
 -13.000  -1.0864   0.03218   0.02744  -0.0175   1.0000   0.0075
 -12.750  -1.0807   0.03060   0.02574  -0.0160   1.0000   0.0076
 -12.500  -1.0733   0.02919   0.02425  -0.0145   1.0000   0.0076
 -12.250  -1.0653   0.02785   0.02283  -0.0130   1.0000   0.0076
 -12.000  -1.0567   0.02655   0.02145  -0.0113   1.0000   0.0076
 -11.750  -1.0457   0.02552   0.02035  -0.0097   1.0000   0.0077
 -11.500  -1.0347   0.02448   0.01925  -0.0079   1.0000   0.0077
 -11.250  -1.0226   0.02353   0.01824  -0.0063   1.0000   0.0078
 -11.000  -1.0156   0.02214   0.01676  -0.0039   1.0000   0.0079
 -10.750  -1.0066   0.02099   0.01554  -0.0016   1.0000   0.0080
 -10.500  -0.9988   0.01982   0.01432   0.0009   1.0000   0.0082
 -10.250  -0.9785   0.01906   0.01346   0.0014   0.9315   0.0083
 -10.000  -0.9698   0.01862   0.01287   0.0048   0.8877   0.0085
  -9.750  -0.9586   0.01810   0.01222   0.0076   0.8620   0.0086
  -9.500  -0.9453   0.01761   0.01163   0.0101   0.8420   0.0087
  -9.250  -0.9297   0.01719   0.01113   0.0122   0.8249   0.0089
  -9.000  -0.9112   0.01676   0.01062   0.0138   0.8093   0.0092
  -8.750  -0.8926   0.01626   0.01004   0.0154   0.7951   0.0094
  -8.500  -0.8723   0.01583   0.00953   0.0167   0.7816   0.0097
  -8.250  -0.8517   0.01541   0.00902   0.0180   0.7689   0.0098
  -8.000  -0.8294   0.01507   0.00862   0.0190   0.7562   0.0100
  -7.750  -0.8099   0.01446   0.00794   0.0205   0.7443   0.0103
  -7.500  -0.7884   0.01401   0.00743   0.0216   0.7326   0.0107
  -7.250  -0.7653   0.01364   0.00701   0.0225   0.7209   0.0111
  -7.000  -0.7416   0.01331   0.00663   0.0233   0.7098   0.0116
  -6.500  -0.6930   0.01270   0.00591   0.0247   0.6873   0.0127
  -6.250  -0.6693   0.01233   0.00550   0.0255   0.6766   0.0139
  -6.000  -0.6439   0.01208   0.00521   0.0261   0.6656   0.0150
  -5.750  -0.6192   0.01176   0.00487   0.0268   0.6550   0.0174
  -5.500  -0.5942   0.01147   0.00455   0.0274   0.6441   0.0214
  -5.250  -0.5693   0.01114   0.00426   0.0280   0.6337   0.0292
  -5.000  -0.5450   0.01080   0.00396   0.0286   0.6230   0.0450
  -4.750  -0.5208   0.01039   0.00367   0.0293   0.6129   0.0691
  -4.500  -0.4975   0.00994   0.00337   0.0301   0.6031   0.1072
  -4.250  -0.4745   0.00943   0.00308   0.0309   0.5929   0.1581
  -4.000  -0.4515   0.00894   0.00282   0.0317   0.5831   0.2153
  -3.750  -0.4283   0.00847   0.00259   0.0324   0.5730   0.2767
  -3.500  -0.4040   0.00810   0.00241   0.0331   0.5637   0.3305
  -3.250  -0.3792   0.00778   0.00224   0.0336   0.5533   0.3791
  -3.000  -0.3542   0.00748   0.00210   0.0342   0.5435   0.4287
  -2.750  -0.3293   0.00720   0.00198   0.0347   0.5335   0.4811
  -2.500  -0.3039   0.00693   0.00188   0.0353   0.5242   0.5281
  -2.250  -0.2780   0.00676   0.00179   0.0357   0.5137   0.5698
  -2.000  -0.2522   0.00655   0.00171   0.0362   0.5042   0.6106
  -1.750  -0.2254   0.00644   0.00166   0.0365   0.4946   0.6427
  -1.500  -0.1982   0.00634   0.00162   0.0368   0.4847   0.6691
  -1.250  -0.1705   0.00630   0.00160   0.0370   0.4748   0.6928
  -1.000  -0.1425   0.00628   0.00159   0.0371   0.4648   0.7131
  -0.750  -0.1143   0.00627   0.00159   0.0372   0.4556   0.7311
  -0.500  -0.0860   0.00630   0.00160   0.0373   0.4452   0.7472
  -0.250  -0.0576   0.00631   0.00161   0.0373   0.4358   0.7606
   0.000  -0.0291   0.00636   0.00163   0.0373   0.4260   0.7712
   0.250  -0.0001   0.00640   0.00165   0.0372   0.4171   0.7812
   0.500   0.0284   0.00647   0.00168   0.0372   0.4069   0.7895
   0.750   0.0574   0.00652   0.00171   0.0371   0.3982   0.7978
   1.000   0.0861   0.00659   0.00175   0.0370   0.3889   0.8049
   1.250   0.1149   0.00665   0.00179   0.0370   0.3801   0.8120
   1.500   0.1437   0.00676   0.00183   0.0368   0.3713   0.8185
   1.750   0.1724   0.00681   0.00189   0.0368   0.3631   0.8244
   2.000   0.2010   0.00691   0.00196   0.0367   0.3545   0.8305
   2.250   0.2299   0.00700   0.00200   0.0366   0.3466   0.8362
   2.500   0.2582   0.00710   0.00208   0.0366   0.3385   0.8418
   2.750   0.2868   0.00717   0.00216   0.0365   0.3321   0.8478
   3.000   0.3151   0.00731   0.00225   0.0364   0.3241   0.8539
   3.250   0.3434   0.00738   0.00233   0.0364   0.3176   0.8593
   3.500   0.3717   0.00749   0.00242   0.0364   0.3106   0.8641
   3.750   0.3999   0.00762   0.00252   0.0363   0.3041   0.8689
   4.000   0.4285   0.00771   0.00260   0.0362   0.2985   0.8729
   4.250   0.4564   0.00783   0.00271   0.0362   0.2918   0.8772
   4.500   0.4844   0.00794   0.00282   0.0362   0.2860   0.8813
   4.750   0.5125   0.00805   0.00292   0.0361   0.2803   0.8855
   5.000   0.5402   0.00821   0.00305   0.0361   0.2740   0.8896
   5.250   0.5682   0.00831   0.00315   0.0360   0.2694   0.8934
   5.500   0.5957   0.00842   0.00327   0.0361   0.2639   0.8973
   5.750   0.6226   0.00860   0.00343   0.0362   0.2575   0.9015
   6.000   0.6502   0.00872   0.00356   0.0362   0.2534   0.9059
   6.250   0.6775   0.00884   0.00369   0.0362   0.2484   0.9102
   6.500   0.7034   0.00902   0.00386   0.0366   0.2424   0.9147
   6.750   0.7300   0.00916   0.00401   0.0367   0.2381   0.9191
   7.000   0.7569   0.00930   0.00416   0.0368   0.2332   0.9233
   7.250   0.7828   0.00949   0.00432   0.0370   0.2276   0.9271
   7.500   0.8086   0.00963   0.00449   0.0373   0.2230   0.9310
   7.750   0.8344   0.00978   0.00465   0.0376   0.2180   0.9351
   8.000   0.8594   0.01001   0.00485   0.0379   0.2120   0.9395
   8.250   0.8848   0.01016   0.00502   0.0382   0.2079   0.9435
   8.500   0.9095   0.01031   0.00520   0.0387   0.2038   0.9478
   8.750   0.9333   0.01053   0.00541   0.0393   0.1987   0.9527
   9.000   0.9571   0.01074   0.00563   0.0398   0.1942   0.9576
   9.250   0.9820   0.01090   0.00582   0.0402   0.1906   0.9622
   9.500   1.0056   0.01112   0.00605   0.0407   0.1862   0.9679
   9.750   1.0311   0.01143   0.00635   0.0407   0.1807   0.9725
  10.000   1.0606   0.01162   0.00658   0.0400   0.1776   0.9761
  10.250   1.0889   0.01189   0.00685   0.0395   0.1732   0.9805
  10.500   1.1188   0.01229   0.00723   0.0383   0.1675   0.9836
  10.750   1.1523   0.01255   0.00753   0.0367   0.1641   0.9853
  11.000   1.1847   0.01288   0.00787   0.0351   0.1594   0.9871
  11.250   1.2154   0.01336   0.00833   0.0337   0.1536   0.9894
  11.500   1.2469   0.01364   0.00865   0.0324   0.1502   0.9919
  11.750   1.2777   0.01404   0.00906   0.0309   0.1451   0.9944
  12.000   1.3086   0.01455   0.00956   0.0293   0.1397   0.9971
  12.250   1.3403   0.01494   0.00998   0.0277   0.1354   0.9994
  12.500   1.3432   0.01530   0.01034   0.0314   0.1317   1.0000
  12.750   1.3389   0.01578   0.01082   0.0362   0.1279   1.0000
  13.000   1.3483   0.01622   0.01130   0.0385   0.1248   1.0000
  13.250   1.3563   0.01691   0.01199   0.0405   0.1203   1.0000
  13.500   1.3631   0.01780   0.01289   0.0423   0.1155   1.0000
  13.750   1.3738   0.01861   0.01372   0.0435   0.1113   1.0000
  14.000   1.3800   0.01977   0.01488   0.0447   0.1066   1.0000
  14.250   1.3883   0.02089   0.01604   0.0456   0.1026   1.0000
  14.500   1.3956   0.02217   0.01733   0.0464   0.0989   1.0000
  15.000   1.4058   0.02528   0.02051   0.0476   0.0918   1.0000
  15.250   1.4091   0.02710   0.02235   0.0480   0.0882   1.0000
  15.500   1.4082   0.02936   0.02464   0.0482   0.0847   1.0000
  15.750   1.4124   0.03126   0.02660   0.0482   0.0822   1.0000
  16.000   1.4137   0.03347   0.02886   0.0482   0.0800   1.0000
  16.250   1.4098   0.03623   0.03165   0.0479   0.0772   1.0000
  16.500   1.4042   0.03926   0.03475   0.0475   0.0749   1.0000
  16.750   1.4046   0.04174   0.03730   0.0471   0.0734   1.0000
  17.000   1.4007   0.04478   0.04041   0.0464   0.0713   1.0000
  17.250   1.3939   0.04821   0.04389   0.0455   0.0698   1.0000
  17.500   1.3820   0.05235   0.04809   0.0443   0.0675   1.0000
  17.750   1.3728   0.05627   0.05210   0.0431   0.0663   1.0000
  18.000   1.3691   0.05962   0.05552   0.0420   0.0649   1.0000
  18.250   1.3609   0.06357   0.05955   0.0406   0.0635   1.0000
  18.500   1.3494   0.06800   0.06405   0.0390   0.0620   1.0000
  18.750   1.3347   0.07294   0.06905   0.0371   0.0604   1.0000
  19.000   1.3184   0.07821   0.07440   0.0350   0.0591   1.0000
  19.250   1.3115   0.08229   0.07856   0.0333   0.0579   1.0000
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