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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 100,000
Max Cl/Cd: 36.46 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh94-il-100000-n5.txt
Download as CSV file: xf-mh94-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.5955   0.11377   0.10755  -0.0501   1.0000   0.0246
 -15.000  -0.6279   0.10297   0.09662  -0.0560   1.0000   0.0243
 -14.750  -0.6606   0.09330   0.08676  -0.0615   1.0000   0.0240
 -14.500  -0.6870   0.08576   0.07905  -0.0653   1.0000   0.0239
 -14.250  -0.7105   0.07938   0.07247  -0.0682   1.0000   0.0238
 -14.000  -0.7303   0.07407   0.06697  -0.0701   1.0000   0.0237
 -13.750  -0.7474   0.06946   0.06217  -0.0712   1.0000   0.0237
 -13.500  -0.7620   0.06542   0.05794  -0.0717   1.0000   0.0237
 -13.250  -0.7746   0.06180   0.05412  -0.0717   1.0000   0.0238
 -13.000  -0.7852   0.05855   0.05068  -0.0712   1.0000   0.0240
 -12.750  -0.7930   0.05570   0.04762  -0.0702   1.0000   0.0241
 -12.500  -0.7983   0.05314   0.04488  -0.0689   1.0000   0.0243
 -12.250  -0.8022   0.05079   0.04233  -0.0674   1.0000   0.0245
 -12.000  -0.8030   0.04871   0.04008  -0.0656   1.0000   0.0248
 -11.750  -0.8011   0.04711   0.03848  -0.0639   1.0000   0.0252
 -11.500  -0.7989   0.04558   0.03689  -0.0620   1.0000   0.0255
 -11.250  -0.7983   0.04413   0.03539  -0.0599   1.0000   0.0262
 -11.000  -0.7961   0.04271   0.03388  -0.0576   1.0000   0.0268
 -10.750  -0.7940   0.04135   0.03241  -0.0551   1.0000   0.0275
 -10.500  -0.7922   0.04002   0.03090  -0.0524   1.0000   0.0285
 -10.250  -0.7893   0.03884   0.02974  -0.0498   1.0000   0.0291
 -10.000  -0.7893   0.03777   0.02868  -0.0468   1.0000   0.0298
  -9.750  -0.7884   0.03672   0.02760  -0.0436   1.0000   0.0304
  -9.500  -0.7895   0.03574   0.02657  -0.0400   1.0000   0.0311
  -9.250  -0.7925   0.03480   0.02556  -0.0359   1.0000   0.0318
  -9.000  -0.7956   0.03391   0.02459  -0.0317   1.0000   0.0326
  -8.750  -0.7968   0.03295   0.02365  -0.0279   1.0000   0.0333
  -8.500  -0.7963   0.03203   0.02272  -0.0243   1.0000   0.0342
  -8.250  -0.7940   0.03113   0.02179  -0.0209   1.0000   0.0354
  -8.000  -0.7895   0.03029   0.02084  -0.0177   1.0000   0.0374
  -7.750  -0.7831   0.02937   0.01996  -0.0151   0.9996   0.0391
  -7.500  -0.7575   0.02838   0.01891  -0.0160   0.9950   0.0432
  -7.250  -0.7328   0.02741   0.01788  -0.0166   0.9902   0.0478
  -7.000  -0.7078   0.02645   0.01692  -0.0173   0.9852   0.0546
  -6.750  -0.6828   0.02544   0.01597  -0.0180   0.9804   0.0651
  -6.500  -0.6599   0.02438   0.01504  -0.0182   0.9747   0.0844
  -6.250  -0.6338   0.02315   0.01415  -0.0194   0.9703   0.1283
  -6.000  -0.6165   0.02190   0.01335  -0.0187   0.9633   0.1997
  -5.750  -0.5906   0.02090   0.01281  -0.0196   0.9583   0.2829
  -5.500  -0.5682   0.02027   0.01248  -0.0192   0.9520   0.3453
  -5.250  -0.5405   0.01989   0.01230  -0.0195   0.9462   0.3975
  -5.000  -0.5082   0.01970   0.01221  -0.0206   0.9419   0.4442
  -4.750  -0.4857   0.01954   0.01212  -0.0195   0.9340   0.4791
  -4.500  -0.4530   0.01952   0.01215  -0.0203   0.9292   0.5107
  -4.250  -0.4268   0.01946   0.01205  -0.0199   0.9221   0.5337
  -4.000  -0.3962   0.01940   0.01197  -0.0202   0.9159   0.5507
  -3.750  -0.3595   0.01935   0.01187  -0.0217   0.9119   0.5653
  -3.500  -0.3369   0.01927   0.01175  -0.0206   0.9028   0.5779
  -3.250  -0.3021   0.01916   0.01155  -0.0218   0.8976   0.5921
  -3.000  -0.2741   0.01911   0.01150  -0.0215   0.8903   0.6036
  -2.750  -0.2435   0.01902   0.01137  -0.0218   0.8832   0.6155
  -2.500  -0.2056   0.01886   0.01113  -0.0235   0.8790   0.6288
  -2.250  -0.1830   0.01884   0.01114  -0.0221   0.8688   0.6378
  -2.000  -0.1468   0.01864   0.01087  -0.0235   0.8634   0.6494
  -1.750  -0.1195   0.01856   0.01081  -0.0230   0.8547   0.6582
  -1.500  -0.0865   0.01835   0.01055  -0.0236   0.8476   0.6688
  -1.000  -0.0242   0.01801   0.01018  -0.0241   0.8312   0.6876
  -0.750   0.0165   0.01778   0.00996  -0.0259   0.8259   0.6954
  -0.500   0.0403   0.01765   0.00979  -0.0249   0.8133   0.7056
  -0.250   0.0782   0.01745   0.00960  -0.0261   0.8055   0.7129
   0.000   0.1071   0.01729   0.00943  -0.0259   0.7931   0.7222
   0.250   0.1375   0.01714   0.00929  -0.0259   0.7806   0.7301
   0.500   0.1752   0.01692   0.00904  -0.0272   0.7696   0.7385
   0.750   0.2054   0.01677   0.00887  -0.0272   0.7547   0.7473
   1.000   0.2352   0.01668   0.00879  -0.0270   0.7387   0.7547
   1.250   0.2665   0.01655   0.00861  -0.0273   0.7220   0.7642
   1.500   0.2971   0.01649   0.00854  -0.0273   0.7041   0.7709
   1.750   0.3272   0.01644   0.00845  -0.0272   0.6851   0.7794
   2.000   0.3564   0.01641   0.00836  -0.0271   0.6646   0.7874
   2.250   0.3844   0.01644   0.00834  -0.0266   0.6430   0.7950
   2.500   0.4107   0.01647   0.00828  -0.0261   0.6200   0.8043
   2.750   0.4341   0.01656   0.00833  -0.0247   0.5949   0.8114
   3.000   0.4579   0.01666   0.00832  -0.0237   0.5686   0.8208
   3.250   0.4797   0.01681   0.00838  -0.0222   0.5405   0.8286
   3.500   0.5005   0.01698   0.00842  -0.0206   0.5114   0.8380
   3.750   0.5199   0.01717   0.00852  -0.0188   0.4822   0.8468
   4.250   0.5568   0.01763   0.00875  -0.0150   0.4261   0.8661
   4.500   0.5743   0.01790   0.00889  -0.0130   0.4002   0.8775
   4.750   0.5925   0.01817   0.00909  -0.0111   0.3753   0.8875
   5.000   0.6104   0.01846   0.00929  -0.0093   0.3514   0.8990
   5.250   0.6285   0.01878   0.00952  -0.0076   0.3292   0.9119
   5.500   0.6493   0.01915   0.00981  -0.0065   0.3077   0.9238
   5.750   0.6728   0.01953   0.01013  -0.0060   0.2863   0.9365
   6.000   0.6992   0.01999   0.01052  -0.0063   0.2657   0.9496
   6.250   0.7285   0.02051   0.01098  -0.0072   0.2456   0.9629
   6.500   0.7598   0.02109   0.01148  -0.0087   0.2270   0.9773
   6.750   0.7905   0.02168   0.01200  -0.0102   0.2100   0.9990
   7.000   0.7979   0.02204   0.01229  -0.0072   0.2000   1.0000
   7.250   0.8106   0.02252   0.01269  -0.0052   0.1897   1.0000
   7.500   0.8262   0.02306   0.01319  -0.0037   0.1803   1.0000
   7.750   0.8408   0.02370   0.01373  -0.0021   0.1723   1.0000
   8.000   0.8583   0.02429   0.01433  -0.0009   0.1644   1.0000
   8.250   0.8735   0.02499   0.01496   0.0006   0.1580   1.0000
   8.500   0.8910   0.02567   0.01564   0.0017   0.1520   1.0000
   8.750   0.9077   0.02638   0.01636   0.0029   0.1468   1.0000
   9.000   0.9229   0.02720   0.01709   0.0042   0.1427   1.0000
   9.250   0.9410   0.02794   0.01789   0.0052   0.1382   1.0000
   9.500   0.9578   0.02872   0.01871   0.0063   0.1341   1.0000
   9.750   0.9737   0.02957   0.01952   0.0074   0.1308   1.0000
  10.000   0.9907   0.03048   0.02041   0.0083   0.1279   1.0000
  10.250   1.0084   0.03136   0.02140   0.0092   0.1250   1.0000
  10.500   1.0251   0.03228   0.02237   0.0101   0.1221   1.0000
  10.750   1.0411   0.03322   0.02333   0.0111   0.1196   1.0000
  11.000   1.0572   0.03420   0.02429   0.0120   0.1174   1.0000
  11.250   1.0742   0.03528   0.02541   0.0127   0.1152   1.0000
  11.500   1.0890   0.03640   0.02668   0.0137   0.1130   1.0000
  11.750   1.1040   0.03756   0.02795   0.0146   0.1112   1.0000
  12.000   1.1182   0.03875   0.02923   0.0155   0.1093   1.0000
  12.250   1.1320   0.03994   0.03048   0.0164   0.1076   1.0000
  12.500   1.1469   0.04113   0.03168   0.0171   0.1060   1.0000
  12.750   1.1651   0.04237   0.03286   0.0175   0.1044   1.0000
  13.000   1.1708   0.04403   0.03478   0.0188   0.1030   1.0000
  13.250   1.1766   0.04579   0.03675   0.0200   0.1017   1.0000
  13.500   1.1819   0.04765   0.03880   0.0210   0.1003   1.0000
  13.750   1.1864   0.04959   0.04091   0.0219   0.0991   1.0000
  14.000   1.1899   0.05161   0.04307   0.0227   0.0979   1.0000
  14.250   1.1939   0.05362   0.04521   0.0234   0.0968   1.0000
  14.500   1.1992   0.05560   0.04727   0.0238   0.0957   1.0000
  14.750   1.2082   0.05740   0.04910   0.0241   0.0946   1.0000
  15.000   1.2192   0.05925   0.05096   0.0243   0.0936   1.0000
  15.250   1.2029   0.06310   0.05511   0.0245   0.0929   1.0000
  15.500   1.1829   0.06764   0.05994   0.0241   0.0923   1.0000
  15.750   1.1570   0.07321   0.06582   0.0227   0.0917   1.0000
  16.000   1.1199   0.08076   0.07369   0.0197   0.0912   1.0000
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