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MH 84 13.69% (mh84-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 84 13.69% (mh84-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.02 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh84-il-1000000-n5.txt
Download as CSV file: xf-mh84-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 84  13.69%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6689   0.06942   0.06659  -0.0288   0.8227   0.0076
 -12.000  -0.7029   0.06116   0.05818  -0.0343   0.8029   0.0076
 -11.750  -0.7642   0.05079   0.04765  -0.0407   0.7835   0.0075
 -11.500  -0.8164   0.03161   0.02796  -0.0636   0.7680   0.0075
 -11.250  -0.8021   0.02842   0.02453  -0.0666   0.7548   0.0075
 -10.750  -0.7611   0.02475   0.02048  -0.0689   0.7290   0.0075
 -10.500  -0.7381   0.02336   0.01892  -0.0695   0.7170   0.0076
 -10.250  -0.7138   0.02217   0.01757  -0.0700   0.7045   0.0076
 -10.000  -0.6887   0.02112   0.01638  -0.0703   0.6934   0.0076
  -9.750  -0.6630   0.02016   0.01527  -0.0706   0.6815   0.0076
  -9.500  -0.6368   0.01929   0.01427  -0.0707   0.6706   0.0076
  -9.250  -0.6103   0.01840   0.01324  -0.0709   0.6594   0.0077
  -9.000  -0.5837   0.01743   0.01213  -0.0711   0.6484   0.0077
  -8.750  -0.5566   0.01662   0.01119  -0.0713   0.6377   0.0078
  -8.500  -0.5290   0.01592   0.01036  -0.0713   0.6267   0.0079
  -8.250  -0.5011   0.01530   0.00963  -0.0714   0.6163   0.0080
  -8.000  -0.4729   0.01473   0.00897  -0.0714   0.6054   0.0080
  -7.750  -0.4445   0.01424   0.00839  -0.0714   0.5954   0.0081
  -7.500  -0.4160   0.01379   0.00785  -0.0713   0.5846   0.0082
  -7.250  -0.3873   0.01339   0.00736  -0.0713   0.5748   0.0083
  -7.000  -0.3585   0.01302   0.00691  -0.0712   0.5638   0.0084
  -6.750  -0.3295   0.01268   0.00650  -0.0712   0.5544   0.0085
  -6.500  -0.3005   0.01238   0.00611  -0.0711   0.5436   0.0087
  -6.250  -0.2714   0.01208   0.00576  -0.0710   0.5344   0.0088
  -6.000  -0.2423   0.01182   0.00542  -0.0710   0.5238   0.0090
  -5.750  -0.2131   0.01156   0.00509  -0.0709   0.5146   0.0092
  -5.500  -0.1839   0.01132   0.00478  -0.0708   0.5045   0.0094
  -5.250  -0.1545   0.01109   0.00449  -0.0707   0.4953   0.0096
  -4.750  -0.0958   0.01067   0.00394  -0.0706   0.4765   0.0100
  -4.250  -0.0370   0.01027   0.00343  -0.0704   0.4577   0.0110
  -3.750   0.0219   0.01000   0.00306  -0.0703   0.4393   0.0122
  -3.500   0.0513   0.00988   0.00288  -0.0702   0.4297   0.0132
  -3.250   0.0807   0.00976   0.00273  -0.0701   0.4212   0.0145
  -3.000   0.1102   0.00966   0.00259  -0.0700   0.4121   0.0165
  -2.750   0.1397   0.00955   0.00247  -0.0700   0.4044   0.0195
  -2.500   0.1691   0.00947   0.00235  -0.0699   0.3950   0.0242
  -2.250   0.1986   0.00937   0.00225  -0.0699   0.3874   0.0311
  -2.000   0.2280   0.00927   0.00215  -0.0698   0.3786   0.0413
  -1.750   0.2574   0.00917   0.00207  -0.0698   0.3707   0.0557
  -1.500   0.2868   0.00907   0.00201  -0.0698   0.3627   0.0734
  -1.250   0.3162   0.00898   0.00196  -0.0698   0.3555   0.0947
  -1.000   0.3456   0.00890   0.00193  -0.0698   0.3478   0.1167
  -0.750   0.3749   0.00886   0.00192  -0.0698   0.3394   0.1412
  -0.500   0.4043   0.00882   0.00192  -0.0698   0.3331   0.1614
  -0.250   0.4336   0.00881   0.00193  -0.0697   0.3260   0.1814
   0.000   0.4629   0.00883   0.00195  -0.0697   0.3196   0.1954
   0.250   0.4922   0.00885   0.00197  -0.0697   0.3120   0.2100
   0.500   0.5214   0.00890   0.00201  -0.0696   0.3050   0.2230
   0.750   0.5507   0.00893   0.00204  -0.0696   0.2995   0.2357
   1.000   0.5799   0.00897   0.00208  -0.0695   0.2929   0.2505
   1.250   0.6090   0.00902   0.00214  -0.0695   0.2867   0.2668
   1.500   0.6381   0.00907   0.00219  -0.0695   0.2803   0.2840
   1.750   0.6671   0.00914   0.00227  -0.0694   0.2739   0.3042
   2.000   0.6962   0.00917   0.00234  -0.0694   0.2693   0.3287
   2.250   0.7251   0.00921   0.00242  -0.0694   0.2633   0.3572
   2.500   0.7539   0.00928   0.00253  -0.0694   0.2569   0.3919
   2.750   0.7828   0.00930   0.00262  -0.0694   0.2525   0.4314
   3.000   0.8116   0.00933   0.00274  -0.0694   0.2473   0.4769
   3.250   0.8401   0.00939   0.00287  -0.0694   0.2414   0.5292
   3.500   0.8687   0.00938   0.00300  -0.0694   0.2372   0.5885
   3.750   0.8970   0.00940   0.00314  -0.0693   0.2324   0.6531
   4.000   0.9247   0.00941   0.00331  -0.0692   0.2274   0.7300
   4.250   0.9498   0.00923   0.00345  -0.0684   0.2237   0.8553
   4.500   0.9784   0.00918   0.00355  -0.0682   0.2192   1.0000
   4.750   1.0068   0.00937   0.00369  -0.0681   0.2148   1.0000
   5.000   1.0350   0.00956   0.00385  -0.0681   0.2110   1.0000
   5.250   1.0634   0.00972   0.00399  -0.0680   0.2080   1.0000
   5.500   1.0915   0.00991   0.00414  -0.0680   0.2040   1.0000
   5.750   1.1193   0.01013   0.00432  -0.0679   0.1997   1.0000
   6.000   1.1472   0.01033   0.00450  -0.0678   0.1964   1.0000
   6.250   1.1752   0.01051   0.00467  -0.0678   0.1938   1.0000
   6.500   1.2029   0.01071   0.00485  -0.0677   0.1907   1.0000
   6.750   1.2303   0.01094   0.00505  -0.0676   0.1871   1.0000
   7.000   1.2575   0.01119   0.00528  -0.0675   0.1835   1.0000
   7.250   1.2850   0.01139   0.00547  -0.0674   0.1810   1.0000
   7.500   1.3122   0.01161   0.00569  -0.0673   0.1783   1.0000
   7.750   1.3392   0.01185   0.00592  -0.0671   0.1754   1.0000
   8.000   1.3657   0.01213   0.00617  -0.0670   0.1724   1.0000
   8.250   1.3924   0.01238   0.00642  -0.0668   0.1698   1.0000
   8.500   1.4190   0.01261   0.00666  -0.0667   0.1675   1.0000
   8.750   1.4453   0.01287   0.00692  -0.0665   0.1647   1.0000
   9.000   1.4712   0.01317   0.00720  -0.0663   0.1619   1.0000
   9.250   1.4967   0.01349   0.00751  -0.0660   0.1592   1.0000
   9.500   1.5223   0.01377   0.00781  -0.0658   0.1572   1.0000
   9.750   1.5479   0.01404   0.00810  -0.0656   0.1553   1.0000
  10.000   1.5730   0.01434   0.00841  -0.0653   0.1530   1.0000
  10.250   1.5974   0.01469   0.00875  -0.0649   0.1502   1.0000
  10.500   1.6211   0.01507   0.00913  -0.0645   0.1475   1.0000
  10.750   1.6449   0.01543   0.00950  -0.0641   0.1455   1.0000
  11.000   1.6688   0.01575   0.00986  -0.0637   0.1439   1.0000
  11.250   1.6919   0.01611   0.01023  -0.0633   0.1421   1.0000
  11.500   1.7142   0.01650   0.01065  -0.0627   0.1400   1.0000
  11.750   1.7354   0.01695   0.01111  -0.0620   0.1379   1.0000
  12.000   1.7553   0.01746   0.01162  -0.0612   0.1355   1.0000
  12.250   1.7754   0.01789   0.01210  -0.0604   0.1338   1.0000
  12.500   1.7947   0.01835   0.01259  -0.0596   0.1324   1.0000
  12.750   1.8120   0.01885   0.01313  -0.0584   0.1308   1.0000
  13.000   1.8237   0.01943   0.01375  -0.0565   0.1293   1.0000
  13.250   1.8326   0.02018   0.01453  -0.0545   0.1277   1.0000
  13.500   1.8409   0.02108   0.01548  -0.0528   0.1262   1.0000
  13.750   1.8484   0.02218   0.01661  -0.0513   0.1244   1.0000
  14.000   1.8586   0.02320   0.01769  -0.0503   0.1234   1.0000
  14.250   1.8688   0.02431   0.01887  -0.0493   0.1221   1.0000
  14.500   1.8777   0.02558   0.02020  -0.0485   0.1209   1.0000
  14.750   1.8856   0.02703   0.02169  -0.0478   0.1196   1.0000
  15.000   1.8919   0.02867   0.02339  -0.0472   0.1182   1.0000
  15.250   1.8964   0.03055   0.02532  -0.0467   0.1168   1.0000
  15.500   1.8988   0.03270   0.02753  -0.0464   0.1153   1.0000
  15.750   1.9000   0.03506   0.02995  -0.0461   0.1138   1.0000
  16.000   1.9047   0.03714   0.03211  -0.0460   0.1130   1.0000
  16.250   1.9073   0.03945   0.03451  -0.0460   0.1120   1.0000
  16.500   1.9086   0.04200   0.03714  -0.0462   0.1109   1.0000
  16.750   1.9071   0.04488   0.04008  -0.0464   0.1096   1.0000
  17.000   1.9034   0.04808   0.04336  -0.0468   0.1082   1.0000
  17.250   1.8971   0.05167   0.04702  -0.0474   0.1068   1.0000
  17.500   1.8896   0.05558   0.05101  -0.0483   0.1056   1.0000
  17.750   1.8807   0.05978   0.05528  -0.0493   0.1042   1.0000
  18.000   1.8774   0.06334   0.05894  -0.0503   0.1034   1.0000
  18.250   1.8727   0.06717   0.06287  -0.0514   0.1022   1.0000
  18.500   1.8665   0.07130   0.06708  -0.0527   0.1010   1.0000
  18.750   1.8583   0.07573   0.07160  -0.0542   0.0998   1.0000
  19.000   1.8473   0.08069   0.07664  -0.0560   0.0983   1.0000
  19.250   1.8333   0.08619   0.08221  -0.0581   0.0969   1.0000
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