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MH 114 13.02% (mh114-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 114 13.02% (mh114-il)
Reynolds number: 500,000
Max Cl/Cd: 131.16 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh114-il-500000.txt
Download as CSV file: xf-mh114-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 114  13.02%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.0364   0.11305   0.11060  -0.0975   0.9687   0.0165
 -10.750  -0.0270   0.10851   0.10606  -0.1027   0.9657   0.0169
 -10.500  -0.0147   0.10417   0.10171  -0.1076   0.9637   0.0170
 -10.250   0.0001   0.09984   0.09739  -0.1115   0.9622   0.0171
 -10.000   0.0120   0.09728   0.09483  -0.1115   0.9559   0.0173
  -9.750   0.0297   0.09427   0.09182  -0.1139   0.9530   0.0175
  -9.500   0.0490   0.09110   0.08864  -0.1174   0.9507   0.0180
  -9.250   0.0664   0.08766   0.08518  -0.1214   0.9467   0.0182
  -9.000   0.0842   0.08406   0.08158  -0.1256   0.9415   0.0189
  -8.750   0.1052   0.07866   0.07615  -0.1340   0.9378   0.0204
  -8.500   0.1214   0.07225   0.06971  -0.1435   0.9297   0.0207
  -8.250   0.1426   0.06918   0.06662  -0.1467   0.9239   0.0210
  -8.000   0.1630   0.06655   0.06396  -0.1500   0.9160   0.0213
  -7.750   0.1814   0.06382   0.06117  -0.1534   0.9070   0.0218
  -7.500   0.1908   0.06124   0.05855  -0.1552   0.8958   0.0224
  -7.250   0.1974   0.05828   0.05556  -0.1572   0.8851   0.0231
  -6.750   0.1709   0.03884   0.03580  -0.1797   0.8558   0.0251
  -6.500   0.1539   0.02327   0.01916  -0.1880   0.8442   0.0142
  -6.250   0.1767   0.02057   0.01611  -0.1892   0.8385   0.0132
  -6.000   0.2002   0.01781   0.01289  -0.1901   0.8323   0.0127
  -5.750   0.2280   0.01580   0.01044  -0.1909   0.8274   0.0126
  -5.500   0.2550   0.01460   0.00898  -0.1911   0.8221   0.0128
  -5.250   0.2822   0.01372   0.00789  -0.1911   0.8164   0.0134
  -5.000   0.3109   0.01283   0.00682  -0.1915   0.8115   0.0142
  -4.750   0.3386   0.01231   0.00627  -0.1917   0.8064   0.0152
  -4.500   0.3662   0.01186   0.00574  -0.1917   0.8007   0.0165
  -4.250   0.3954   0.01132   0.00512  -0.1922   0.7957   0.0180
  -4.000   0.4238   0.01106   0.00480  -0.1923   0.7905   0.0210
  -3.750   0.4517   0.01075   0.00447  -0.1924   0.7847   0.0250
  -3.500   0.4813   0.01033   0.00402  -0.1928   0.7796   0.0317
  -3.250   0.5099   0.01006   0.00375  -0.1930   0.7743   0.0440
  -3.000   0.5380   0.00978   0.00351  -0.1932   0.7683   0.0625
  -2.750   0.5675   0.00953   0.00332  -0.1936   0.7631   0.0918
  -2.500   0.5956   0.00932   0.00321  -0.1938   0.7574   0.1322
  -2.250   0.6237   0.00912   0.00313  -0.1940   0.7514   0.1792
  -2.000   0.6531   0.00898   0.00305  -0.1944   0.7460   0.2316
  -1.750   0.6805   0.00883   0.00303  -0.1944   0.7398   0.2826
  -1.500   0.7086   0.00871   0.00300  -0.1945   0.7337   0.3332
  -1.250   0.7373   0.00864   0.00299  -0.1948   0.7281   0.3856
  -1.000   0.7645   0.00854   0.00302  -0.1947   0.7214   0.4388
  -0.750   0.7927   0.00850   0.00302  -0.1948   0.7153   0.4886
  -0.500   0.8201   0.00845   0.00307  -0.1947   0.7089   0.5345
  -0.250   0.8473   0.00843   0.00310  -0.1945   0.7020   0.5765
   0.000   0.8748   0.00843   0.00314  -0.1944   0.6957   0.6176
   0.250   0.9011   0.00841   0.00320  -0.1941   0.6882   0.6574
   0.750   0.9535   0.00841   0.00332  -0.1933   0.6739   0.7369
   1.000   0.9789   0.00843   0.00338  -0.1927   0.6667   0.7791
   1.250   1.0022   0.00840   0.00346  -0.1916   0.6588   0.8266
   1.500   1.0214   0.00836   0.00349  -0.1895   0.6513   0.8880
   1.750   1.0427   0.00827   0.00346  -0.1880   0.6433   1.0000
   2.000   1.0695   0.00841   0.00351  -0.1878   0.6351   1.0000
   2.250   1.0958   0.00853   0.00359  -0.1876   0.6263   1.0000
   2.500   1.1218   0.00870   0.00366  -0.1873   0.6179   1.0000
   2.750   1.1475   0.00882   0.00376  -0.1869   0.6085   1.0000
   3.000   1.1728   0.00899   0.00386  -0.1865   0.5997   1.0000
   3.250   1.1977   0.00915   0.00399  -0.1860   0.5898   1.0000
   3.500   1.2224   0.00932   0.00411  -0.1854   0.5803   1.0000
   4.000   1.2703   0.00970   0.00440  -0.1841   0.5601   1.0000
   4.250   1.2936   0.00991   0.00457  -0.1833   0.5500   1.0000
   4.500   1.3161   0.01015   0.00475  -0.1823   0.5395   1.0000
   4.750   1.3389   0.01036   0.00494  -0.1814   0.5287   1.0000
   5.000   1.3606   0.01060   0.00514  -0.1804   0.5181   1.0000
   5.500   1.4015   0.01111   0.00559  -0.1777   0.4962   1.0000
   5.750   1.4206   0.01139   0.00583  -0.1762   0.4855   1.0000
   6.000   1.4384   0.01173   0.00612  -0.1744   0.4748   1.0000
   6.250   1.4574   0.01201   0.00640  -0.1728   0.4634   1.0000
   6.500   1.4758   0.01234   0.00670  -0.1712   0.4529   1.0000
   6.750   1.4926   0.01273   0.00705  -0.1693   0.4421   1.0000
   7.000   1.5108   0.01308   0.00739  -0.1677   0.4312   1.0000
   7.250   1.5281   0.01346   0.00776  -0.1660   0.4206   1.0000
   7.500   1.5439   0.01392   0.00818  -0.1641   0.4101   1.0000
   7.750   1.5606   0.01434   0.00861  -0.1623   0.3994   1.0000
   8.000   1.5769   0.01480   0.00906  -0.1605   0.3890   1.0000
   8.250   1.5912   0.01536   0.00958  -0.1585   0.3786   1.0000
   8.500   1.6069   0.01587   0.01010  -0.1567   0.3680   1.0000
   8.750   1.6220   0.01642   0.01066  -0.1548   0.3580   1.0000
   9.000   1.6348   0.01710   0.01131  -0.1527   0.3478   1.0000
   9.250   1.6493   0.01771   0.01193  -0.1509   0.3371   1.0000
   9.500   1.6629   0.01839   0.01262  -0.1490   0.3269   1.0000
   9.750   1.6740   0.01922   0.01343  -0.1468   0.3165   1.0000
  10.000   1.6875   0.01995   0.01418  -0.1450   0.3063   1.0000
  10.250   1.6995   0.02080   0.01503  -0.1431   0.2960   1.0000
  10.500   1.7091   0.02180   0.01602  -0.1409   0.2857   1.0000
  10.750   1.7203   0.02276   0.01699  -0.1391   0.2747   1.0000
  11.000   1.7310   0.02377   0.01801  -0.1372   0.2642   1.0000
  11.250   1.7394   0.02496   0.01919  -0.1352   0.2539   1.0000
  11.500   1.7477   0.02620   0.02043  -0.1332   0.2433   1.0000
  11.750   1.7570   0.02741   0.02167  -0.1314   0.2326   1.0000
  12.000   1.7641   0.02882   0.02308  -0.1295   0.2222   1.0000
  12.250   1.7692   0.03044   0.02468  -0.1275   0.2116   1.0000
  12.500   1.7763   0.03195   0.02621  -0.1259   0.2010   1.0000
  12.750   1.7824   0.03358   0.02785  -0.1242   0.1909   1.0000
  13.000   1.7863   0.03546   0.02974  -0.1224   0.1810   1.0000
  13.250   1.7894   0.03748   0.03175  -0.1207   0.1710   1.0000
  13.500   1.7941   0.03940   0.03370  -0.1193   0.1611   1.0000
  13.750   1.7968   0.04157   0.03588  -0.1178   0.1519   1.0000
  14.000   1.7971   0.04406   0.03836  -0.1163   0.1430   1.0000
  14.250   1.8010   0.04625   0.04059  -0.1152   0.1346   1.0000
  14.500   1.8017   0.04884   0.04320  -0.1140   0.1270   1.0000
  14.750   1.8020   0.05154   0.04593  -0.1129   0.1192   1.0000
  15.000   1.8034   0.05420   0.04863  -0.1120   0.1120   1.0000
  15.250   1.8004   0.05745   0.05189  -0.1112   0.1049   1.0000
  15.500   1.8015   0.06029   0.05479  -0.1105   0.0979   1.0000
  15.750   1.7980   0.06376   0.05829  -0.1100   0.0917   1.0000
  16.000   1.7968   0.06704   0.06161  -0.1096   0.0854   1.0000
  16.250   1.7930   0.07073   0.06536  -0.1093   0.0799   1.0000
  16.500   1.7901   0.07438   0.06906  -0.1092   0.0744   1.0000
  16.750   1.7852   0.07839   0.07312  -0.1092   0.0695   1.0000
  17.000   1.7814   0.08231   0.07711  -0.1094   0.0647   1.0000
  17.250   1.7746   0.08676   0.08162  -0.1097   0.0605   1.0000
  17.500   1.7708   0.09084   0.08577  -0.1102   0.0563   1.0000
  18.000   1.7579   0.09996   0.09503  -0.1117   0.0488   1.0000
  18.250   1.7489   0.10502   0.10015  -0.1128   0.0454   1.0000
  18.500   1.7432   0.10961   0.10483  -0.1140   0.0423   1.0000
  18.750   1.7355   0.11456   0.10985  -0.1153   0.0392   1.0000
  19.000   1.7270   0.11971   0.11507  -0.1169   0.0364   1.0000
  19.250   1.7214   0.12436   0.11982  -0.1185   0.0339   1.0000
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