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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.94 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh93-il-1000000-n5.txt
Download as CSV file: xf-mh93-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.9976   0.14591   0.14338   0.0330   1.0000   0.0047
 -19.250  -1.0252   0.13491   0.13223   0.0262   1.0000   0.0047
 -19.000  -1.0538   0.12406   0.12122   0.0195   1.0000   0.0047
 -18.750  -1.0806   0.11392   0.11091   0.0133   1.0000   0.0046
 -18.500  -1.1029   0.10493   0.10179   0.0079   1.0000   0.0047
 -18.250  -1.1272   0.09595   0.09264   0.0026   1.0000   0.0046
 -18.000  -1.1488   0.08776   0.08429  -0.0022   1.0000   0.0045
 -17.750  -1.1659   0.08067   0.07706  -0.0062   1.0000   0.0046
 -17.500  -1.1778   0.07463   0.07090  -0.0095   1.0000   0.0046
 -17.250  -1.1919   0.06855   0.06469  -0.0127   1.0000   0.0046
 -17.000  -1.2016   0.06339   0.05941  -0.0152   1.0000   0.0046
 -16.750  -1.2098   0.05870   0.05460  -0.0172   1.0000   0.0046
 -16.500  -1.2160   0.05451   0.05030  -0.0188   1.0000   0.0047
 -16.250  -1.2212   0.05069   0.04637  -0.0200   1.0000   0.0047
 -16.000  -1.2246   0.04728   0.04286  -0.0208   1.0000   0.0047
 -15.750  -1.2251   0.04439   0.03988  -0.0211   1.0000   0.0048
 -15.500  -1.2255   0.04169   0.03708  -0.0212   1.0000   0.0048
 -15.250  -1.2238   0.03933   0.03464  -0.0210   1.0000   0.0048
 -15.000  -1.2223   0.03708   0.03230  -0.0205   1.0000   0.0048
 -14.750  -1.2189   0.03510   0.03024  -0.0198   1.0000   0.0049
 -14.500  -1.2151   0.03324   0.02831  -0.0189   1.0000   0.0049
 -14.250  -1.2102   0.03157   0.02655  -0.0178   1.0000   0.0050
 -14.000  -1.2032   0.03011   0.02504  -0.0166   1.0000   0.0050
 -13.750  -1.1969   0.02866   0.02351  -0.0153   1.0000   0.0050
 -13.500  -1.1886   0.02742   0.02220  -0.0139   1.0000   0.0050
 -13.250  -1.1799   0.02623   0.02095  -0.0123   1.0000   0.0050
 -13.000  -1.1702   0.02516   0.01982  -0.0108   1.0000   0.0051
 -12.750  -1.1587   0.02422   0.01883  -0.0092   1.0000   0.0053
 -12.500  -1.1467   0.02333   0.01789  -0.0077   1.0000   0.0054
 -12.250  -1.1345   0.02249   0.01700  -0.0060   1.0000   0.0054
 -11.750  -1.1028   0.02098   0.01531  -0.0037   0.9157   0.0055
 -11.500  -1.0934   0.02047   0.01462  -0.0009   0.8722   0.0055
 -11.250  -1.0813   0.01991   0.01393   0.0014   0.8461   0.0056
 -11.000  -1.0674   0.01939   0.01329   0.0034   0.8257   0.0057
 -10.500  -1.0379   0.01836   0.01208   0.0074   0.7920   0.0058
 -10.250  -1.0222   0.01789   0.01154   0.0094   0.7774   0.0058
 -10.000  -1.0083   0.01733   0.01089   0.0117   0.7644   0.0059
  -9.750  -0.9925   0.01688   0.01036   0.0137   0.7510   0.0060
  -9.500  -0.9738   0.01646   0.00987   0.0153   0.7383   0.0061
  -9.250  -0.9537   0.01604   0.00940   0.0165   0.7270   0.0063
  -9.000  -0.9326   0.01567   0.00898   0.0177   0.7150   0.0065
  -8.750  -0.9110   0.01529   0.00854   0.0188   0.7038   0.0066
  -8.500  -0.8888   0.01495   0.00815   0.0198   0.6926   0.0068
  -8.250  -0.8660   0.01462   0.00776   0.0207   0.6814   0.0069
  -8.000  -0.8427   0.01431   0.00740   0.0215   0.6708   0.0071
  -7.750  -0.8191   0.01401   0.00704   0.0223   0.6599   0.0074
  -7.500  -0.7951   0.01372   0.00671   0.0230   0.6492   0.0076
  -7.250  -0.7707   0.01345   0.00639   0.0237   0.6390   0.0078
  -7.000  -0.7466   0.01314   0.00604   0.0244   0.6281   0.0083
  -6.750  -0.7219   0.01288   0.00574   0.0250   0.6179   0.0087
  -6.500  -0.6968   0.01264   0.00546   0.0256   0.6070   0.0093
  -6.250  -0.6713   0.01241   0.00519   0.0261   0.5970   0.0100
  -5.750  -0.6201   0.01196   0.00468   0.0270   0.5761   0.0120
  -5.500  -0.5943   0.01175   0.00444   0.0275   0.5661   0.0139
  -5.250  -0.5683   0.01154   0.00422   0.0279   0.5553   0.0164
  -5.000  -0.5424   0.01133   0.00400   0.0283   0.5456   0.0207
  -4.750  -0.5163   0.01112   0.00379   0.0287   0.5350   0.0261
  -4.500  -0.4903   0.01089   0.00358   0.0291   0.5261   0.0346
  -4.250  -0.4643   0.01067   0.00338   0.0294   0.5156   0.0459
  -4.000  -0.4385   0.01042   0.00318   0.0299   0.5063   0.0626
  -3.750  -0.4135   0.01010   0.00296   0.0304   0.4966   0.0906
  -3.500  -0.3893   0.00969   0.00273   0.0310   0.4881   0.1354
  -3.000  -0.3418   0.00883   0.00230   0.0323   0.4691   0.2500
  -2.750  -0.3178   0.00844   0.00213   0.0329   0.4602   0.3116
  -2.500  -0.2927   0.00813   0.00199   0.0334   0.4516   0.3611
  -2.250  -0.2676   0.00786   0.00187   0.0339   0.4418   0.4119
  -2.000  -0.2421   0.00759   0.00177   0.0343   0.4330   0.4630
  -1.750  -0.2155   0.00744   0.00170   0.0346   0.4245   0.4969
  -1.500  -0.1882   0.00733   0.00164   0.0348   0.4154   0.5221
  -1.250  -0.1608   0.00725   0.00159   0.0349   0.4061   0.5464
  -1.000  -0.1331   0.00717   0.00155   0.0351   0.3976   0.5698
  -0.750  -0.1058   0.00710   0.00152   0.0352   0.3893   0.5939
  -0.500  -0.0784   0.00702   0.00149   0.0354   0.3804   0.6204
  -0.250  -0.0509   0.00698   0.00148   0.0355   0.3717   0.6445
   0.000  -0.0231   0.00693   0.00148   0.0356   0.3643   0.6660
   0.250   0.0048   0.00693   0.00149   0.0357   0.3557   0.6853
   0.500   0.0331   0.00693   0.00151   0.0357   0.3477   0.7024
   0.750   0.0613   0.00696   0.00154   0.0357   0.3398   0.7175
   1.000   0.0899   0.00699   0.00156   0.0357   0.3329   0.7308
   1.250   0.1183   0.00704   0.00161   0.0356   0.3248   0.7431
   1.500   0.1469   0.00708   0.00165   0.0356   0.3183   0.7533
   1.750   0.1756   0.00714   0.00170   0.0355   0.3114   0.7631
   2.000   0.2040   0.00722   0.00176   0.0354   0.3043   0.7717
   2.250   0.2328   0.00728   0.00181   0.0353   0.2980   0.7803
   2.500   0.2612   0.00736   0.00188   0.0352   0.2918   0.7882
   2.750   0.2898   0.00744   0.00195   0.0351   0.2867   0.7974
   3.000   0.3182   0.00751   0.00203   0.0351   0.2810   0.8055
   3.250   0.3465   0.00762   0.00212   0.0350   0.2743   0.8133
   3.500   0.3752   0.00771   0.00220   0.0348   0.2693   0.8189
   3.750   0.4036   0.00779   0.00229   0.0347   0.2645   0.8241
   4.000   0.4319   0.00790   0.00238   0.0346   0.2592   0.8294
   4.250   0.4604   0.00801   0.00248   0.0345   0.2544   0.8343
   4.500   0.4888   0.00812   0.00258   0.0344   0.2490   0.8386
   4.750   0.5168   0.00824   0.00269   0.0343   0.2436   0.8431
   5.000   0.5449   0.00836   0.00282   0.0342   0.2393   0.8478
   5.250   0.5732   0.00847   0.00292   0.0341   0.2350   0.8522
   5.500   0.6011   0.00861   0.00305   0.0340   0.2296   0.8563
   5.750   0.6285   0.00875   0.00320   0.0340   0.2245   0.8607
   6.000   0.6563   0.00887   0.00333   0.0340   0.2209   0.8657
   6.250   0.6839   0.00902   0.00347   0.0339   0.2161   0.8709
   6.500   0.7109   0.00920   0.00364   0.0339   0.2105   0.8756
   6.750   0.7381   0.00932   0.00379   0.0340   0.2069   0.8801
   7.000   0.7653   0.00948   0.00396   0.0340   0.2023   0.8843
   7.250   0.7920   0.00968   0.00414   0.0340   0.1971   0.8883
   7.500   0.8190   0.00985   0.00431   0.0340   0.1927   0.8918
   7.750   0.8452   0.01003   0.00450   0.0341   0.1873   0.8954
   8.000   0.8708   0.01026   0.00472   0.0343   0.1814   0.8993
   8.250   0.8972   0.01043   0.00491   0.0344   0.1780   0.9034
   8.500   0.9234   0.01063   0.00512   0.0345   0.1740   0.9073
   8.750   0.9483   0.01088   0.00536   0.0347   0.1689   0.9108
   9.000   0.9733   0.01108   0.00559   0.0350   0.1653   0.9149
   9.250   0.9983   0.01129   0.00582   0.0353   0.1615   0.9194
   9.500   1.0227   0.01154   0.00607   0.0356   0.1573   0.9238
   9.750   1.0462   0.01181   0.00635   0.0361   0.1529   0.9279
  10.000   1.0700   0.01203   0.00661   0.0366   0.1499   0.9326
  10.250   1.0928   0.01229   0.00689   0.0371   0.1457   0.9381
  10.500   1.1142   0.01263   0.00722   0.0379   0.1409   0.9435
  10.750   1.1366   0.01287   0.00751   0.0385   0.1379   0.9492
  11.000   1.1580   0.01317   0.00783   0.0392   0.1338   0.9559
  11.250   1.1795   0.01357   0.00823   0.0397   0.1289   0.9630
  11.500   1.2032   0.01391   0.00861   0.0399   0.1251   0.9706
  11.750   1.2304   0.01435   0.00906   0.0391   0.1201   0.9765
  12.000   1.2571   0.01488   0.00958   0.0382   0.1151   0.9830
  12.250   1.2856   0.01539   0.01011   0.0369   0.1101   0.9886
  12.500   1.3098   0.01607   0.01078   0.0361   0.1048   1.0000
  12.750   1.3154   0.01660   0.01134   0.0389   0.1016   1.0000
  13.000   1.3223   0.01735   0.01209   0.0410   0.0975   1.0000
  13.250   1.3294   0.01825   0.01301   0.0427   0.0936   1.0000
  13.500   1.3377   0.01921   0.01398   0.0439   0.0893   1.0000
  13.750   1.3432   0.02045   0.01522   0.0452   0.0850   1.0000
  14.000   1.3515   0.02161   0.01642   0.0460   0.0817   1.0000
  14.250   1.3576   0.02301   0.01784   0.0468   0.0783   1.0000
  14.500   1.3620   0.02463   0.01948   0.0474   0.0753   1.0000
  14.750   1.3688   0.02613   0.02103   0.0478   0.0730   1.0000
  15.000   1.3742   0.02783   0.02278   0.0480   0.0709   1.0000
  15.250   1.3755   0.02993   0.02491   0.0482   0.0683   1.0000
  15.500   1.3770   0.03209   0.02712   0.0482   0.0661   1.0000
  15.750   1.3793   0.03425   0.02934   0.0480   0.0641   1.0000
  16.000   1.3788   0.03674   0.03189   0.0478   0.0622   1.0000
  16.250   1.3753   0.03958   0.03478   0.0473   0.0603   1.0000
  16.500   1.3709   0.04258   0.03783   0.0468   0.0587   1.0000
  16.750   1.3695   0.04539   0.04072   0.0461   0.0574   1.0000
  17.000   1.3643   0.04870   0.04410   0.0453   0.0555   1.0000
  17.250   1.3584   0.05217   0.04764   0.0442   0.0545   1.0000
  17.500   1.3458   0.05651   0.05203   0.0429   0.0523   1.0000
  17.750   1.3385   0.06033   0.05594   0.0416   0.0517   1.0000
  18.000   1.3315   0.06419   0.05987   0.0402   0.0504   1.0000
  18.250   1.3224   0.06836   0.06412   0.0387   0.0492   1.0000
  18.500   1.3117   0.07282   0.06867   0.0370   0.0481   1.0000
  18.750   1.2976   0.07783   0.07374   0.0350   0.0466   1.0000
  19.000   1.2843   0.08282   0.07881   0.0329   0.0457   1.0000
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