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MH 115 11.06% (mh115-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 115 11.06% (mh115-il)
Reynolds number: 1,000,000
Max Cl/Cd: 158.67 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh115-il-1000000.txt
Download as CSV file: xf-mh115-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 115  11.06%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0644   0.09725   0.09562  -0.0814   0.9839   0.0101
 -10.500  -0.0610   0.09352   0.09190  -0.0826   0.9791   0.0101
 -10.250  -0.0535   0.08932   0.08770  -0.0849   0.9768   0.0102
 -10.000  -0.0446   0.08509   0.08347  -0.0874   0.9748   0.0102
  -9.750  -0.0379   0.08040   0.07879  -0.0897   0.9731   0.0104
  -9.500  -0.0298   0.07740   0.07579  -0.0907   0.9678   0.0105
  -9.250  -0.0195   0.07395   0.07235  -0.0926   0.9631   0.0106
  -9.000  -0.0059   0.07020   0.06859  -0.0956   0.9603   0.0109
  -8.750  -0.0924   0.08169   0.08002  -0.0917   0.9734   0.0105
  -8.500  -0.0815   0.07883   0.07717  -0.0937   0.9671   0.0106
  -8.250  -0.0666   0.07569   0.07403  -0.0969   0.9619   0.0108
  -8.000  -0.0495   0.07220   0.07053  -0.1012   0.9560   0.0110
  -7.750  -0.0286   0.06805   0.06637  -0.1072   0.9494   0.0113
  -7.500  -0.0005   0.06297   0.06126  -0.1163   0.9434   0.0118
  -7.250   0.0238   0.05648   0.05471  -0.1272   0.9297   0.0126
  -7.000   0.0372   0.04708   0.04522  -0.1404   0.9065   0.0131
  -6.750   0.0049   0.01921   0.01576  -0.1635   0.8728   0.0078
  -6.500   0.0246   0.01506   0.01109  -0.1646   0.8627   0.0068
  -6.250   0.0498   0.01267   0.00821  -0.1650   0.8544   0.0063
  -6.000   0.0764   0.01157   0.00687  -0.1650   0.8456   0.0061
  -5.750   0.1037   0.01081   0.00594  -0.1651   0.8376   0.0061
  -5.500   0.1311   0.01019   0.00517  -0.1651   0.8291   0.0062
  -5.250   0.1588   0.00970   0.00457  -0.1652   0.8210   0.0062
  -5.000   0.1865   0.00928   0.00404  -0.1652   0.8128   0.0064
  -4.750   0.2146   0.00892   0.00359  -0.1652   0.8047   0.0067
  -4.500   0.2425   0.00862   0.00318  -0.1652   0.7967   0.0071
  -4.250   0.2707   0.00836   0.00284  -0.1652   0.7887   0.0078
  -4.000   0.2988   0.00805   0.00244  -0.1652   0.7806   0.0107
  -3.750   0.3271   0.00775   0.00219  -0.1653   0.7726   0.0232
  -3.500   0.3548   0.00765   0.00205  -0.1653   0.7648   0.0301
  -3.250   0.3830   0.00753   0.00192  -0.1653   0.7568   0.0377
  -3.000   0.4108   0.00741   0.00180  -0.1653   0.7491   0.0518
  -2.750   0.4391   0.00723   0.00171  -0.1655   0.7413   0.0768
  -2.500   0.4669   0.00712   0.00163  -0.1655   0.7337   0.1059
  -2.250   0.4952   0.00698   0.00157  -0.1656   0.7259   0.1365
  -2.000   0.5230   0.00691   0.00152  -0.1656   0.7183   0.1676
  -1.750   0.5513   0.00680   0.00148  -0.1658   0.7106   0.2034
  -1.500   0.5790   0.00673   0.00146  -0.1658   0.7030   0.2416
  -1.250   0.6073   0.00662   0.00145  -0.1659   0.6953   0.2890
  -1.000   0.6350   0.00656   0.00145  -0.1659   0.6877   0.3395
  -0.750   0.6633   0.00646   0.00146  -0.1661   0.6799   0.3900
  -0.500   0.6909   0.00643   0.00149  -0.1661   0.6721   0.4388
  -0.250   0.7190   0.00636   0.00152  -0.1662   0.6641   0.4902
   0.000   0.7465   0.00634   0.00157  -0.1661   0.6562   0.5418
   0.250   0.7745   0.00629   0.00162  -0.1661   0.6480   0.5950
   0.500   0.8018   0.00628   0.00168  -0.1660   0.6398   0.6465
   0.750   0.8292   0.00625   0.00175  -0.1659   0.6312   0.6981
   1.000   0.8560   0.00624   0.00183  -0.1657   0.6228   0.7505
   1.250   0.8821   0.00622   0.00191  -0.1653   0.6138   0.8048
   1.500   0.9062   0.00617   0.00199  -0.1643   0.6051   0.8694
   1.750   0.9264   0.00607   0.00199  -0.1624   0.5959   1.0000
   2.000   0.9541   0.00616   0.00205  -0.1624   0.5862   1.0000
   2.250   0.9812   0.00629   0.00212  -0.1623   0.5764   1.0000
   2.750   1.0349   0.00655   0.00228  -0.1619   0.5549   1.0000
   3.000   1.0615   0.00669   0.00237  -0.1617   0.5438   1.0000
   3.250   1.0877   0.00686   0.00247  -0.1614   0.5319   1.0000
   3.500   1.1135   0.00703   0.00259  -0.1611   0.5191   1.0000
   3.750   1.1396   0.00720   0.00271  -0.1608   0.5060   1.0000
   4.000   1.1652   0.00739   0.00284  -0.1604   0.4920   1.0000
   4.250   1.1906   0.00759   0.00299  -0.1600   0.4775   1.0000
   4.500   1.2155   0.00781   0.00315  -0.1595   0.4620   1.0000
   4.750   1.2399   0.00806   0.00333  -0.1590   0.4451   1.0000
   5.250   1.2880   0.00860   0.00372  -0.1577   0.4109   1.0000
   5.500   1.3116   0.00889   0.00394  -0.1570   0.3927   1.0000
   5.750   1.3350   0.00919   0.00417  -0.1563   0.3757   1.0000
   6.000   1.3582   0.00948   0.00441  -0.1555   0.3601   1.0000
   6.250   1.3808   0.00981   0.00467  -0.1547   0.3431   1.0000
   6.500   1.4033   0.01014   0.00494  -0.1538   0.3276   1.0000
   6.750   1.4252   0.01048   0.00523  -0.1529   0.3114   1.0000
   7.000   1.4466   0.01085   0.00553  -0.1518   0.2954   1.0000
   7.250   1.4679   0.01120   0.00583  -0.1508   0.2812   1.0000
   7.500   1.4884   0.01159   0.00616  -0.1496   0.2662   1.0000
   7.750   1.5077   0.01199   0.00651  -0.1482   0.2509   1.0000
   8.000   1.5261   0.01238   0.00686  -0.1466   0.2376   1.0000
   8.250   1.5433   0.01280   0.00724  -0.1447   0.2237   1.0000
   8.500   1.5598   0.01326   0.00764  -0.1428   0.2099   1.0000
   8.750   1.5759   0.01374   0.00808  -0.1409   0.1963   1.0000
   9.000   1.5899   0.01431   0.00858  -0.1387   0.1800   1.0000
   9.250   1.6024   0.01499   0.00916  -0.1362   0.1623   1.0000
   9.500   1.6148   0.01567   0.00977  -0.1338   0.1460   1.0000
   9.750   1.6276   0.01634   0.01039  -0.1316   0.1329   1.0000
  10.000   1.6390   0.01710   0.01109  -0.1291   0.1187   1.0000
  10.250   1.6497   0.01791   0.01185  -0.1267   0.1057   1.0000
  10.500   1.6599   0.01878   0.01266  -0.1243   0.0942   1.0000
  10.750   1.6700   0.01968   0.01352  -0.1219   0.0842   1.0000
  11.000   1.6806   0.02057   0.01440  -0.1197   0.0758   1.0000
  11.250   1.6903   0.02155   0.01537  -0.1175   0.0676   1.0000
  11.500   1.6986   0.02266   0.01645  -0.1152   0.0597   1.0000
  11.750   1.7063   0.02384   0.01762  -0.1130   0.0523   1.0000
  12.000   1.7151   0.02500   0.01878  -0.1110   0.0462   1.0000
  12.250   1.7219   0.02634   0.02011  -0.1089   0.0399   1.0000
  12.500   1.7270   0.02786   0.02163  -0.1068   0.0337   1.0000
  12.750   1.7308   0.02954   0.02331  -0.1047   0.0275   1.0000
  13.000   1.7339   0.03137   0.02514  -0.1027   0.0221   1.0000
  13.250   1.7363   0.03332   0.02710  -0.1008   0.0177   1.0000
  13.500   1.7388   0.03534   0.02916  -0.0991   0.0145   1.0000
  13.750   1.7421   0.03737   0.03124  -0.0976   0.0121   1.0000
  14.000   1.7449   0.03953   0.03346  -0.0963   0.0103   1.0000
  14.250   1.7462   0.04192   0.03589  -0.0950   0.0086   1.0000
  14.500   1.7485   0.04429   0.03834  -0.0939   0.0072   1.0000
  14.750   1.7491   0.04695   0.04107  -0.0930   0.0060   1.0000
  15.000   1.7469   0.05002   0.04420  -0.0921   0.0046   1.0000
  15.250   1.7440   0.05327   0.04754  -0.0914   0.0033   1.0000
  15.500   1.7410   0.05669   0.05105  -0.0910   0.0025   1.0000
  15.750   1.7351   0.06062   0.05508  -0.0907   0.0019   1.0000
  16.000   1.7328   0.06418   0.05875  -0.0907   0.0017   1.0000
  16.250   1.7287   0.06810   0.06278  -0.0908   0.0016   1.0000
  16.500   1.7227   0.07242   0.06721  -0.0912   0.0014   1.0000
  16.750   1.7147   0.07720   0.07212  -0.0919   0.0013   1.0000
  17.000   1.7030   0.08270   0.07777  -0.0930   0.0012   1.0000
  17.250   1.6972   0.08739   0.08258  -0.0940   0.0012   1.0000
  17.500   1.6904   0.09237   0.08768  -0.0953   0.0012   1.0000
  17.750   1.6826   0.09765   0.09309  -0.0969   0.0011   1.0000
  18.000   1.6732   0.10327   0.09885  -0.0988   0.0011   1.0000
  18.250   1.6635   0.10906   0.10476  -0.1009   0.0011   1.0000
  18.500   1.6545   0.11480   0.11062  -0.1031   0.0011   1.0000
  18.750   1.6425   0.12122   0.11717  -0.1058   0.0010   1.0000
  19.000   1.6318   0.12745   0.12353  -0.1087   0.0010   1.0000
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