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MH 84 13.69% (mh84-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 84 13.69% (mh84-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.31 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh84-il-1000000.txt
Download as CSV file: xf-mh84-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3089   0.10753   0.10523  -0.0067   0.7664   0.0152
 -10.000  -0.5449   0.05534   0.05294  -0.0364   0.7929   0.0116
  -9.750  -0.6205   0.03156   0.02840  -0.0646   0.7750   0.0111
  -9.250  -0.5868   0.02591   0.02215  -0.0685   0.7481   0.0112
  -9.000  -0.5652   0.02386   0.01983  -0.0695   0.7360   0.0113
  -8.750  -0.5415   0.02227   0.01801  -0.0700   0.7235   0.0114
  -8.500  -0.5164   0.02094   0.01649  -0.0704   0.7119   0.0115
  -8.250  -0.4909   0.01969   0.01502  -0.0706   0.6999   0.0115
  -8.000  -0.4644   0.01860   0.01377  -0.0708   0.6886   0.0116
  -7.750  -0.4375   0.01764   0.01264  -0.0709   0.6772   0.0117
  -7.500  -0.4101   0.01678   0.01163  -0.0709   0.6658   0.0118
  -7.250  -0.3824   0.01601   0.01072  -0.0710   0.6550   0.0118
  -7.000  -0.3544   0.01531   0.00989  -0.0709   0.6435   0.0119
  -6.750  -0.3262   0.01468   0.00915  -0.0709   0.6331   0.0120
  -6.500  -0.2978   0.01411   0.00846  -0.0709   0.6216   0.0121
  -6.250  -0.2692   0.01359   0.00784  -0.0708   0.6115   0.0122
  -5.750  -0.2115   0.01270   0.00677  -0.0707   0.5901   0.0123
  -5.500  -0.1827   0.01215   0.00611  -0.0707   0.5795   0.0125
  -5.250  -0.1538   0.01157   0.00545  -0.0707   0.5693   0.0129
  -5.000  -0.1247   0.01123   0.00504  -0.0706   0.5590   0.0132
  -4.750  -0.0954   0.01094   0.00469  -0.0706   0.5487   0.0136
  -4.500  -0.0661   0.01068   0.00436  -0.0705   0.5386   0.0140
  -4.250  -0.0366   0.01042   0.00404  -0.0704   0.5283   0.0145
  -4.000  -0.0071   0.01022   0.00376  -0.0703   0.5186   0.0149
  -3.750   0.0224   0.00989   0.00337  -0.0703   0.5083   0.0160
  -3.500   0.0519   0.00972   0.00314  -0.0702   0.4988   0.0173
  -3.250   0.0814   0.00951   0.00289  -0.0701   0.4886   0.0194
  -3.000   0.1110   0.00933   0.00268  -0.0701   0.4796   0.0233
  -2.750   0.1405   0.00911   0.00246  -0.0700   0.4698   0.0331
  -2.500   0.1700   0.00889   0.00230  -0.0700   0.4607   0.0524
  -2.250   0.1994   0.00874   0.00218  -0.0700   0.4510   0.0732
  -2.000   0.2289   0.00862   0.00210  -0.0700   0.4423   0.0920
  -1.750   0.2583   0.00853   0.00204  -0.0700   0.4326   0.1106
  -1.500   0.2878   0.00846   0.00199  -0.0700   0.4243   0.1298
  -1.250   0.3172   0.00838   0.00196  -0.0700   0.4154   0.1531
  -1.000   0.3466   0.00834   0.00195  -0.0699   0.4069   0.1755
  -0.750   0.3760   0.00832   0.00195  -0.0699   0.3979   0.1969
  -0.500   0.4054   0.00831   0.00195  -0.0699   0.3899   0.2161
   0.000   0.4641   0.00833   0.00198  -0.0698   0.3735   0.2512
   0.250   0.4935   0.00832   0.00199  -0.0698   0.3656   0.2691
   0.500   0.5227   0.00837   0.00202  -0.0697   0.3569   0.2884
   0.750   0.5521   0.00836   0.00205  -0.0697   0.3504   0.3112
   1.000   0.5812   0.00839   0.00210  -0.0697   0.3424   0.3387
   1.250   0.6104   0.00838   0.00215  -0.0697   0.3354   0.3742
   1.500   0.6395   0.00838   0.00222  -0.0697   0.3276   0.4170
   1.750   0.6684   0.00837   0.00230  -0.0697   0.3207   0.4711
   2.000   0.6974   0.00831   0.00239  -0.0697   0.3142   0.5368
   2.250   0.7258   0.00830   0.00252  -0.0696   0.3064   0.6155
   2.500   0.7541   0.00818   0.00263  -0.0695   0.3006   0.7070
   2.750   0.7792   0.00795   0.00274  -0.0686   0.2942   0.8466
   3.000   0.8082   0.00786   0.00281  -0.0684   0.2877   1.0000
   3.250   0.8372   0.00799   0.00289  -0.0684   0.2819   1.0000
   3.500   0.8659   0.00818   0.00300  -0.0684   0.2750   1.0000
   3.750   0.8947   0.00832   0.00311  -0.0683   0.2699   1.0000
   4.000   0.9235   0.00848   0.00322  -0.0683   0.2643   1.0000
   4.250   0.9518   0.00870   0.00337  -0.0683   0.2576   1.0000
   4.500   0.9805   0.00883   0.00348  -0.0682   0.2533   1.0000
   4.750   1.0090   0.00901   0.00361  -0.0682   0.2482   1.0000
   5.000   1.0371   0.00924   0.00379  -0.0681   0.2424   1.0000
   5.250   1.0655   0.00939   0.00393  -0.0681   0.2386   1.0000
   5.500   1.0937   0.00957   0.00407  -0.0680   0.2340   1.0000
   5.750   1.1215   0.00981   0.00426  -0.0679   0.2287   1.0000
   6.000   1.1494   0.01001   0.00444  -0.0679   0.2248   1.0000
   6.250   1.1775   0.01019   0.00461  -0.0678   0.2213   1.0000
   6.500   1.2051   0.01041   0.00479  -0.0677   0.2172   1.0000
   6.750   1.2322   0.01070   0.00504  -0.0676   0.2123   1.0000
   7.000   1.2600   0.01087   0.00522  -0.0675   0.2095   1.0000
   7.250   1.2875   0.01107   0.00541  -0.0674   0.2061   1.0000
   7.500   1.3145   0.01133   0.00564  -0.0673   0.2024   1.0000
   7.750   1.3409   0.01165   0.00593  -0.0672   0.1981   1.0000
   8.000   1.3681   0.01185   0.00614  -0.0670   0.1958   1.0000
   8.250   1.3951   0.01206   0.00637  -0.0669   0.1930   1.0000
   8.500   1.4216   0.01233   0.00662  -0.0667   0.1897   1.0000
   8.750   1.4473   0.01266   0.00693  -0.0665   0.1859   1.0000
   9.000   1.4731   0.01297   0.00724  -0.0663   0.1830   1.0000
   9.250   1.4995   0.01319   0.00748  -0.0661   0.1810   1.0000
   9.500   1.5253   0.01346   0.00776  -0.0659   0.1783   1.0000
   9.750   1.5504   0.01379   0.00808  -0.0656   0.1754   1.0000
  10.000   1.5744   0.01421   0.00848  -0.0653   0.1719   1.0000
  10.250   1.5992   0.01452   0.00881  -0.0649   0.1696   1.0000
  10.500   1.6243   0.01478   0.00911  -0.0647   0.1675   1.0000
  10.750   1.6485   0.01511   0.00945  -0.0643   0.1651   1.0000
  11.000   1.6717   0.01550   0.00985  -0.0638   0.1626   1.0000
  11.250   1.6933   0.01600   0.01033  -0.0632   0.1596   1.0000
  11.500   1.7152   0.01643   0.01079  -0.0626   0.1574   1.0000
  11.750   1.7382   0.01675   0.01116  -0.0621   0.1558   1.0000
  12.000   1.7598   0.01714   0.01158  -0.0615   0.1537   1.0000
  12.250   1.7798   0.01760   0.01206  -0.0607   0.1514   1.0000
  12.500   1.7974   0.01817   0.01264  -0.0596   0.1491   1.0000
  12.750   1.8095   0.01892   0.01340  -0.0579   0.1465   1.0000
  13.000   1.8222   0.01944   0.01398  -0.0561   0.1454   1.0000
  13.250   1.8343   0.02004   0.01465  -0.0544   0.1441   1.0000
  13.500   1.8453   0.02079   0.01545  -0.0529   0.1426   1.0000
  13.750   1.8553   0.02170   0.01640  -0.0515   0.1409   1.0000
  14.000   1.8637   0.02281   0.01755  -0.0503   0.1392   1.0000
  14.250   1.8697   0.02419   0.01897  -0.0491   0.1374   1.0000
  14.500   1.8714   0.02602   0.02083  -0.0480   0.1353   1.0000
  14.750   1.8804   0.02740   0.02228  -0.0474   0.1342   1.0000
  15.000   1.8907   0.02873   0.02369  -0.0469   0.1331   1.0000
  15.250   1.8992   0.03025   0.02527  -0.0465   0.1318   1.0000
  15.500   1.9055   0.03203   0.02712  -0.0461   0.1304   1.0000
  15.750   1.9095   0.03408   0.02923  -0.0459   0.1289   1.0000
  16.000   1.9102   0.03653   0.03173  -0.0457   0.1274   1.0000
  16.250   1.9061   0.03953   0.03478  -0.0457   0.1257   1.0000
  16.500   1.8999   0.04285   0.03816  -0.0459   0.1240   1.0000
  16.750   1.9041   0.04510   0.04051  -0.0461   0.1232   1.0000
  17.000   1.9066   0.04758   0.04308  -0.0463   0.1221   1.0000
  17.250   1.9071   0.05034   0.04591  -0.0467   0.1209   1.0000
  17.500   1.9054   0.05345   0.04911  -0.0472   0.1197   1.0000
  17.750   1.9013   0.05697   0.05270  -0.0480   0.1183   1.0000
  18.000   1.8936   0.06100   0.05679  -0.0491   0.1169   1.0000
  18.250   1.8817   0.06568   0.06152  -0.0504   0.1152   1.0000
  18.500   1.8730   0.07004   0.06595  -0.0517   0.1137   1.0000
  18.750   1.8712   0.07357   0.06959  -0.0529   0.1129   1.0000
  19.000   1.8693   0.07716   0.07327  -0.0541   0.1118   1.0000
  19.250   1.8642   0.08127   0.07747  -0.0556   0.1105   1.0000
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