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MH 92 15.49% (mh92-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 92 15.49% (mh92-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.09 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh92-il-1000000-n5.txt
Download as CSV file: xf-mh92-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 92  15.49%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.0057   0.13140   0.12879   0.0240   1.0000   0.0045
 -18.500  -1.0391   0.11941   0.11663   0.0167   1.0000   0.0045
 -18.250  -1.0673   0.10891   0.10596   0.0103   1.0000   0.0045
 -18.000  -1.0962   0.09870   0.09557   0.0041   1.0000   0.0045
 -17.750  -1.1196   0.08990   0.08663  -0.0012   1.0000   0.0045
 -17.500  -1.1415   0.08173   0.07829  -0.0060   1.0000   0.0045
 -17.250  -1.1587   0.07469   0.07112  -0.0100   1.0000   0.0045
 -17.000  -1.1708   0.06879   0.06509  -0.0132   1.0000   0.0045
 -16.750  -1.1863   0.06268   0.05881  -0.0164   1.0000   0.0044
 -16.500  -1.1948   0.05790   0.05392  -0.0186   1.0000   0.0044
 -16.250  -1.2030   0.05344   0.04934  -0.0204   1.0000   0.0044
 -16.000  -1.2051   0.04998   0.04579  -0.0216   1.0000   0.0045
 -15.750  -1.2120   0.04617   0.04185  -0.0225   1.0000   0.0045
 -15.500  -1.2145   0.04311   0.03869  -0.0229   1.0000   0.0045
 -15.250  -1.2156   0.04037   0.03585  -0.0230   1.0000   0.0045
 -15.000  -1.2132   0.03812   0.03353  -0.0227   1.0000   0.0046
 -14.750  -1.2127   0.03583   0.03114  -0.0222   1.0000   0.0046
 -14.500  -1.2104   0.03381   0.02904  -0.0214   1.0000   0.0046
 -14.250  -1.2058   0.03209   0.02724  -0.0204   1.0000   0.0047
 -14.000  -1.2014   0.03042   0.02549  -0.0192   1.0000   0.0046
 -13.750  -1.1923   0.02919   0.02420  -0.0180   1.0000   0.0048
 -13.500  -1.1865   0.02775   0.02269  -0.0165   1.0000   0.0048
 -13.250  -1.1786   0.02652   0.02139  -0.0149   1.0000   0.0048
 -13.000  -1.1689   0.02545   0.02026  -0.0134   1.0000   0.0049
 -12.750  -1.1591   0.02443   0.01918  -0.0117   1.0000   0.0049
 -12.500  -1.1484   0.02348   0.01817  -0.0100   1.0000   0.0049
 -12.250  -1.1373   0.02259   0.01721  -0.0082   1.0000   0.0050
 -12.000  -1.1247   0.02180   0.01638  -0.0064   1.0000   0.0051
 -11.750  -1.1110   0.02109   0.01562  -0.0047   1.0000   0.0052
 -11.500  -1.0930   0.02031   0.01478  -0.0039   0.9504   0.0052
 -11.250  -1.0817   0.01988   0.01415  -0.0012   0.8886   0.0053
 -11.000  -1.0702   0.01938   0.01351   0.0014   0.8609   0.0054
 -10.750  -1.0577   0.01883   0.01285   0.0039   0.8393   0.0054
 -10.500  -1.0430   0.01838   0.01230   0.0061   0.8209   0.0055
 -10.250  -1.0276   0.01791   0.01174   0.0081   0.8049   0.0056
 -10.000  -1.0088   0.01748   0.01121   0.0096   0.7900   0.0056
  -9.750  -0.9890   0.01704   0.01070   0.0109   0.7754   0.0057
  -9.500  -0.9681   0.01665   0.01024   0.0121   0.7622   0.0058
  -9.250  -0.9474   0.01621   0.00972   0.0133   0.7498   0.0058
  -9.000  -0.9272   0.01570   0.00913   0.0145   0.7372   0.0060
  -8.750  -0.9053   0.01527   0.00865   0.0156   0.7252   0.0062
  -8.500  -0.8828   0.01489   0.00821   0.0165   0.7133   0.0064
  -8.250  -0.8595   0.01455   0.00781   0.0173   0.7013   0.0064
  -8.000  -0.8358   0.01422   0.00744   0.0181   0.6900   0.0067
  -7.750  -0.8118   0.01391   0.00707   0.0188   0.6788   0.0069
  -7.500  -0.7874   0.01361   0.00672   0.0194   0.6668   0.0071
  -7.250  -0.7627   0.01333   0.00639   0.0200   0.6557   0.0073
  -7.000  -0.7377   0.01306   0.00606   0.0206   0.6446   0.0076
  -6.750  -0.7122   0.01281   0.00577   0.0211   0.6335   0.0078
  -6.500  -0.6872   0.01253   0.00544   0.0217   0.6225   0.0083
  -6.250  -0.6617   0.01228   0.00516   0.0222   0.6110   0.0088
  -6.000  -0.6357   0.01206   0.00490   0.0226   0.6000   0.0095
  -5.750  -0.6096   0.01186   0.00465   0.0230   0.5888   0.0101
  -5.500  -0.5835   0.01163   0.00440   0.0234   0.5776   0.0114
  -5.250  -0.5571   0.01143   0.00417   0.0237   0.5670   0.0130
  -5.000  -0.5307   0.01124   0.00395   0.0241   0.5558   0.0156
  -4.750  -0.5043   0.01103   0.00374   0.0244   0.5455   0.0197
  -4.500  -0.4778   0.01084   0.00353   0.0248   0.5348   0.0253
  -4.000  -0.4251   0.01039   0.00314   0.0254   0.5148   0.0468
  -3.750  -0.3990   0.01014   0.00294   0.0258   0.5039   0.0658
  -3.500  -0.3736   0.00981   0.00273   0.0262   0.4938   0.0974
  -3.250  -0.3492   0.00940   0.00250   0.0268   0.4838   0.1481
  -3.000  -0.3247   0.00898   0.00229   0.0273   0.4745   0.2050
  -2.750  -0.3006   0.00855   0.00211   0.0279   0.4644   0.2714
  -2.500  -0.2756   0.00820   0.00196   0.0284   0.4544   0.3293
  -2.000  -0.2246   0.00763   0.00173   0.0292   0.4359   0.4350
  -1.750  -0.1982   0.00744   0.00165   0.0295   0.4262   0.4788
  -1.500  -0.1709   0.00733   0.00159   0.0297   0.4161   0.5070
  -1.250  -0.1433   0.00724   0.00155   0.0298   0.4075   0.5322
  -1.000  -0.1156   0.00719   0.00151   0.0299   0.3973   0.5555
  -0.750  -0.0879   0.00711   0.00148   0.0300   0.3884   0.5794
  -0.250  -0.0328   0.00697   0.00144   0.0303   0.3710   0.6316
   0.000  -0.0051   0.00695   0.00144   0.0304   0.3614   0.6546
   0.250   0.0230   0.00693   0.00144   0.0304   0.3540   0.6755
   0.750   0.0794   0.00695   0.00149   0.0305   0.3375   0.7111
   1.000   0.1076   0.00698   0.00152   0.0305   0.3292   0.7255
   1.250   0.1361   0.00701   0.00156   0.0305   0.3225   0.7386
   1.500   0.1646   0.00708   0.00160   0.0304   0.3142   0.7502
   1.750   0.1931   0.00713   0.00166   0.0304   0.3078   0.7615
   2.000   0.2217   0.00718   0.00171   0.0303   0.3015   0.7707
   2.250   0.2502   0.00727   0.00177   0.0302   0.2947   0.7803
   2.500   0.2788   0.00732   0.00184   0.0302   0.2888   0.7887
   2.750   0.3072   0.00741   0.00191   0.0301   0.2819   0.7981
   3.000   0.3355   0.00749   0.00199   0.0301   0.2767   0.8072
   3.250   0.3640   0.00757   0.00207   0.0300   0.2717   0.8162
   3.500   0.3923   0.00767   0.00216   0.0299   0.2656   0.8229
   3.750   0.4206   0.00777   0.00226   0.0299   0.2603   0.8291
   4.000   0.4491   0.00786   0.00235   0.0297   0.2548   0.8348
   4.250   0.4774   0.00798   0.00244   0.0297   0.2496   0.8397
   4.500   0.5055   0.00809   0.00256   0.0296   0.2449   0.8448
   4.750   0.5337   0.00819   0.00266   0.0295   0.2400   0.8501
   5.000   0.5619   0.00833   0.00277   0.0294   0.2342   0.8548
   5.250   0.5896   0.00846   0.00290   0.0294   0.2295   0.8594
   5.500   0.6176   0.00856   0.00303   0.0294   0.2255   0.8643
   5.750   0.6452   0.00871   0.00316   0.0293   0.2200   0.8695
   6.000   0.6728   0.00887   0.00331   0.0293   0.2147   0.8743
   6.250   0.7001   0.00899   0.00346   0.0293   0.2109   0.8797
   6.500   0.7272   0.00914   0.00361   0.0294   0.2057   0.8856
   6.750   0.7542   0.00934   0.00378   0.0294   0.2004   0.8908
   7.000   0.7813   0.00947   0.00395   0.0295   0.1962   0.8950
   7.250   0.8077   0.00966   0.00413   0.0296   0.1902   0.8995
   7.500   0.8340   0.00986   0.00432   0.0297   0.1847   0.9041
   7.750   0.8609   0.01003   0.00450   0.0298   0.1806   0.9082
   8.000   0.8868   0.01023   0.00470   0.0300   0.1759   0.9122
   8.250   0.9122   0.01044   0.00493   0.0302   0.1713   0.9167
   8.500   0.9382   0.01062   0.00513   0.0304   0.1677   0.9213
   8.750   0.9638   0.01085   0.00535   0.0306   0.1632   0.9255
   9.250   1.0129   0.01129   0.00583   0.0313   0.1552   0.9352
   9.500   1.0375   0.01152   0.00607   0.0317   0.1513   0.9403
   9.750   1.0608   0.01181   0.00636   0.0322   0.1463   0.9453
  10.000   1.0845   0.01204   0.00663   0.0327   0.1429   0.9513
  10.250   1.1081   0.01230   0.00690   0.0331   0.1390   0.9575
  10.500   1.1322   0.01263   0.00724   0.0334   0.1342   0.9637
  11.000   1.1852   0.01329   0.00793   0.0327   0.1252   0.9754
  11.250   1.2126   0.01374   0.00837   0.0320   0.1199   0.9816
  11.500   1.2427   0.01413   0.00878   0.0308   0.1151   0.9858
  11.750   1.2711   0.01467   0.00929   0.0296   0.1092   0.9909
  12.000   1.2991   0.01513   0.00978   0.0287   0.1048   0.9981
  12.250   1.3146   0.01566   0.01029   0.0300   0.0997   1.0000
  12.500   1.3237   0.01614   0.01079   0.0325   0.0962   1.0000
  12.750   1.3313   0.01670   0.01137   0.0350   0.0926   1.0000
  13.000   1.3376   0.01749   0.01216   0.0372   0.0883   1.0000
  13.250   1.3462   0.01832   0.01300   0.0388   0.0841   1.0000
  13.500   1.3540   0.01930   0.01399   0.0402   0.0806   1.0000
  13.750   1.3610   0.02044   0.01515   0.0414   0.0769   1.0000
  14.000   1.3706   0.02150   0.01625   0.0423   0.0748   1.0000
  14.250   1.3774   0.02282   0.01761   0.0431   0.0720   1.0000
  14.500   1.3828   0.02435   0.01916   0.0437   0.0695   1.0000
  14.750   1.3897   0.02584   0.02071   0.0441   0.0675   1.0000
  15.000   1.3954   0.02750   0.02241   0.0444   0.0653   1.0000
  15.250   1.3983   0.02946   0.02441   0.0446   0.0632   1.0000
  15.500   1.3978   0.03181   0.02681   0.0446   0.0604   1.0000
  15.750   1.4012   0.03389   0.02895   0.0445   0.0590   1.0000
  16.000   1.4031   0.03616   0.03129   0.0442   0.0578   1.0000
  16.250   1.4002   0.03897   0.03416   0.0438   0.0558   1.0000
  16.500   1.3957   0.04202   0.03726   0.0432   0.0543   1.0000
  16.750   1.3912   0.04516   0.04047   0.0425   0.0526   1.0000
  17.000   1.3873   0.04834   0.04373   0.0416   0.0514   1.0000
  17.250   1.3815   0.05185   0.04732   0.0405   0.0501   1.0000
  17.500   1.3732   0.05574   0.05128   0.0392   0.0489   1.0000
  17.750   1.3622   0.06004   0.05565   0.0377   0.0475   1.0000
  18.000   1.3512   0.06446   0.06014   0.0361   0.0465   1.0000
  18.250   1.3428   0.06861   0.06438   0.0345   0.0456   1.0000
  18.500   1.3329   0.07305   0.06891   0.0328   0.0446   1.0000
  18.750   1.3210   0.07786   0.07380   0.0308   0.0436   1.0000
  19.000   1.3075   0.08295   0.07897   0.0286   0.0425   1.0000
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