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MH 113 14.62% (mh113-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 113 14.62% (mh113-il)
Reynolds number: 500,000
Max Cl/Cd: 114.18 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh113-il-500000-n5.txt
Download as CSV file: xf-mh113-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 113  14.62%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.1206   0.08605   0.08297  -0.1456   0.8924   0.0131
 -10.500   0.1274   0.08167   0.07853  -0.1489   0.8822   0.0134
 -10.250   0.1325   0.07814   0.07496  -0.1508   0.8714   0.0134
  -9.750  -0.1026   0.03437   0.03064  -0.1727   0.8299   0.0126
  -9.500  -0.1191   0.02744   0.02329  -0.1822   0.8183   0.0127
  -9.250  -0.1109   0.02477   0.02028  -0.1841   0.8116   0.0128
  -9.000  -0.0965   0.02280   0.01804  -0.1850   0.8052   0.0128
  -8.750  -0.0777   0.02121   0.01618  -0.1856   0.7995   0.0130
  -8.500  -0.0558   0.02002   0.01474  -0.1861   0.7946   0.0131
  -8.250  -0.0329   0.01900   0.01353  -0.1863   0.7892   0.0132
  -8.000  -0.0098   0.01787   0.01222  -0.1866   0.7839   0.0134
  -7.750   0.0151   0.01701   0.01123  -0.1869   0.7792   0.0136
  -7.500   0.0405   0.01633   0.01046  -0.1870   0.7745   0.0138
  -7.250   0.0664   0.01573   0.00977  -0.1872   0.7694   0.0140
  -7.000   0.0929   0.01518   0.00912  -0.1873   0.7645   0.0143
  -6.750   0.1198   0.01468   0.00851  -0.1875   0.7601   0.0146
  -6.500   0.1466   0.01418   0.00795  -0.1876   0.7552   0.0149
  -6.250   0.1737   0.01373   0.00740  -0.1877   0.7500   0.0152
  -6.000   0.2012   0.01333   0.00689  -0.1878   0.7454   0.0155
  -5.750   0.2288   0.01297   0.00646  -0.1879   0.7407   0.0160
  -5.500   0.2564   0.01259   0.00602  -0.1881   0.7356   0.0164
  -5.250   0.2841   0.01224   0.00562  -0.1882   0.7305   0.0171
  -5.000   0.3121   0.01196   0.00528  -0.1884   0.7258   0.0176
  -4.750   0.3401   0.01169   0.00496  -0.1885   0.7207   0.0182
  -4.500   0.3681   0.01145   0.00466  -0.1886   0.7153   0.0188
  -4.000   0.4244   0.01100   0.00412  -0.1888   0.7051   0.0205
  -3.750   0.4524   0.01083   0.00390  -0.1888   0.6995   0.0217
  -3.500   0.4804   0.01069   0.00369  -0.1888   0.6941   0.0233
  -3.250   0.5086   0.01053   0.00352  -0.1889   0.6887   0.0262
  -3.000   0.5365   0.01037   0.00337  -0.1890   0.6827   0.0318
  -2.750   0.5643   0.01024   0.00323  -0.1890   0.6771   0.0426
  -2.500   0.5924   0.01010   0.00313  -0.1891   0.6712   0.0564
  -2.250   0.6201   0.01001   0.00305  -0.1891   0.6648   0.0717
  -2.000   0.6477   0.00992   0.00298  -0.1890   0.6589   0.0907
  -1.750   0.6756   0.00981   0.00294  -0.1891   0.6524   0.1156
  -1.500   0.7030   0.00971   0.00291  -0.1891   0.6457   0.1512
  -1.250   0.7306   0.00962   0.00290  -0.1892   0.6394   0.1900
  -1.000   0.7580   0.00956   0.00290  -0.1891   0.6324   0.2248
  -0.750   0.7848   0.00954   0.00291  -0.1890   0.6256   0.2559
  -0.500   0.8122   0.00950   0.00294  -0.1889   0.6184   0.2883
  -0.250   0.8387   0.00951   0.00298  -0.1887   0.6110   0.3244
   0.000   0.8657   0.00950   0.00303  -0.1886   0.6038   0.3612
   0.250   0.8920   0.00952   0.00309  -0.1883   0.5960   0.3972
   0.500   0.9182   0.00956   0.00316  -0.1880   0.5885   0.4320
   0.750   0.9442   0.00960   0.00325  -0.1877   0.5803   0.4660
   1.000   0.9698   0.00966   0.00334  -0.1873   0.5728   0.4988
   1.250   0.9954   0.00973   0.00344  -0.1869   0.5642   0.5317
   1.500   1.0203   0.00982   0.00356  -0.1863   0.5565   0.5640
   1.750   1.0454   0.00990   0.00368  -0.1858   0.5478   0.5962
   2.000   1.0695   0.01001   0.00382  -0.1851   0.5398   0.6273
   2.250   1.0939   0.01010   0.00396  -0.1844   0.5311   0.6597
   2.500   1.1170   0.01023   0.00411  -0.1836   0.5228   0.6930
   2.750   1.1402   0.01033   0.00427  -0.1826   0.5139   0.7298
   3.000   1.1617   0.01045   0.00445  -0.1814   0.5056   0.7719
   3.250   1.1810   0.01052   0.00462  -0.1797   0.4970   0.8237
   3.500   1.1920   0.01044   0.00469  -0.1760   0.4893   0.9959
   3.750   1.2139   0.01065   0.00487  -0.1749   0.4805   1.0000
   4.000   1.2345   0.01091   0.00506  -0.1736   0.4720   1.0000
   4.250   1.2559   0.01115   0.00526  -0.1725   0.4633   1.0000
   4.500   1.2761   0.01142   0.00548  -0.1712   0.4550   1.0000
   4.750   1.2963   0.01170   0.00572  -0.1699   0.4458   1.0000
   5.000   1.3162   0.01200   0.00597  -0.1685   0.4375   1.0000
   5.250   1.3357   0.01231   0.00624  -0.1672   0.4287   1.0000
   5.500   1.3549   0.01264   0.00653  -0.1658   0.4205   1.0000
   5.750   1.3736   0.01299   0.00685  -0.1643   0.4115   1.0000
   6.000   1.3922   0.01335   0.00718  -0.1628   0.4033   1.0000
   6.250   1.4101   0.01374   0.00754  -0.1613   0.3948   1.0000
   6.500   1.4281   0.01414   0.00792  -0.1598   0.3868   1.0000
   6.750   1.4452   0.01458   0.00833  -0.1582   0.3783   1.0000
   7.000   1.4626   0.01503   0.00876  -0.1567   0.3705   1.0000
   7.250   1.4787   0.01553   0.00924  -0.1550   0.3618   1.0000
   7.500   1.4954   0.01603   0.00972  -0.1535   0.3543   1.0000
   7.750   1.5110   0.01658   0.01026  -0.1518   0.3459   1.0000
   8.000   1.5268   0.01715   0.01081  -0.1502   0.3385   1.0000
   8.250   1.5423   0.01775   0.01140  -0.1486   0.3305   1.0000
   8.500   1.5568   0.01840   0.01205  -0.1469   0.3234   1.0000
   8.750   1.5719   0.01905   0.01270  -0.1454   0.3154   1.0000
   9.000   1.5852   0.01982   0.01345  -0.1436   0.3081   1.0000
   9.250   1.6001   0.02051   0.01416  -0.1421   0.3006   1.0000
   9.500   1.6119   0.02140   0.01503  -0.1403   0.2929   1.0000
   9.750   1.6263   0.02217   0.01581  -0.1389   0.2855   1.0000
  10.250   1.6509   0.02401   0.01766  -0.1356   0.2708   1.0000
  10.500   1.6611   0.02511   0.01875  -0.1339   0.2632   1.0000
  10.750   1.6736   0.02608   0.01974  -0.1324   0.2560   1.0000
  11.000   1.6835   0.02726   0.02092  -0.1308   0.2486   1.0000
  11.250   1.6946   0.02838   0.02206  -0.1293   0.2416   1.0000
  11.500   1.7036   0.02969   0.02337  -0.1278   0.2339   1.0000
  11.750   1.7135   0.03096   0.02466  -0.1263   0.2269   1.0000
  12.000   1.7214   0.03243   0.02613  -0.1248   0.2190   1.0000
  12.250   1.7306   0.03383   0.02755  -0.1234   0.2125   1.0000
  12.500   1.7378   0.03543   0.02916  -0.1220   0.2047   1.0000
  12.750   1.7452   0.03705   0.03080  -0.1207   0.1980   1.0000
  13.000   1.7522   0.03875   0.03252  -0.1194   0.1908   1.0000
  13.250   1.7578   0.04063   0.03442  -0.1181   0.1840   1.0000
  13.500   1.7642   0.04247   0.03628  -0.1170   0.1770   1.0000
  13.750   1.7683   0.04457   0.03840  -0.1158   0.1706   1.0000
  14.000   1.7740   0.04657   0.04043  -0.1148   0.1640   1.0000
  14.250   1.7769   0.04891   0.04279  -0.1137   0.1580   1.0000
  14.500   1.7818   0.05109   0.04502  -0.1128   0.1516   1.0000
  14.750   1.7830   0.05373   0.04767  -0.1119   0.1456   1.0000
  15.000   1.7878   0.05600   0.05000  -0.1112   0.1403   1.0000
  15.250   1.7888   0.05877   0.05279  -0.1105   0.1344   1.0000
  15.500   1.7911   0.06145   0.05552  -0.1100   0.1295   1.0000
  15.750   1.7927   0.06426   0.05838  -0.1095   0.1240   1.0000
  16.000   1.7912   0.06751   0.06166  -0.1091   0.1191   1.0000
  16.250   1.7935   0.07033   0.06454  -0.1088   0.1145   1.0000
  16.500   1.7925   0.07363   0.06788  -0.1086   0.1097   1.0000
  16.750   1.7910   0.07705   0.07137  -0.1085   0.1054   1.0000
  17.000   1.7903   0.08044   0.07482  -0.1085   0.1007   1.0000
  17.500   1.7847   0.08790   0.08239  -0.1089   0.0919   1.0000
  17.750   1.7803   0.09195   0.08649  -0.1094   0.0875   1.0000
  18.000   1.7766   0.09595   0.09055  -0.1099   0.0839   1.0000
  18.250   1.7745   0.09974   0.09441  -0.1105   0.0802   1.0000
  18.500   1.7686   0.10414   0.09886  -0.1113   0.0766   1.0000
  18.750   1.7648   0.10824   0.10304  -0.1121   0.0734   1.0000
  19.000   1.7612   0.11233   0.10720  -0.1131   0.0700   1.0000
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