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MH 113 14.62% (mh113-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 113 14.62% (mh113-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.23 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh113-il-1000000-n5.txt
Download as CSV file: xf-mh113-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.1988   0.04324   0.04017  -0.1705   0.8502   0.0099
 -11.500  -0.2431   0.03478   0.03151  -0.1752   0.8346   0.0097
 -11.250  -0.2800   0.02703   0.02351  -0.1816   0.8209   0.0097
 -11.000  -0.2788   0.02369   0.01991  -0.1858   0.8118   0.0098
 -10.750  -0.2676   0.02185   0.01789  -0.1868   0.8049   0.0098
 -10.500  -0.2515   0.02049   0.01636  -0.1872   0.7985   0.0099
 -10.250  -0.2326   0.01932   0.01502  -0.1875   0.7932   0.0100
 -10.000  -0.2116   0.01830   0.01387  -0.1878   0.7876   0.0101
  -9.750  -0.1892   0.01746   0.01289  -0.1880   0.7822   0.0102
  -9.500  -0.1656   0.01675   0.01205  -0.1881   0.7774   0.0103
  -9.250  -0.1408   0.01610   0.01130  -0.1883   0.7725   0.0104
  -9.000  -0.1159   0.01545   0.01054  -0.1884   0.7674   0.0104
  -8.750  -0.0907   0.01489   0.00986  -0.1884   0.7624   0.0105
  -8.500  -0.0651   0.01420   0.00906  -0.1887   0.7580   0.0106
  -8.250  -0.0391   0.01350   0.00827  -0.1889   0.7532   0.0108
  -8.000  -0.0127   0.01301   0.00770  -0.1891   0.7481   0.0110
  -7.750   0.0141   0.01261   0.00722  -0.1892   0.7435   0.0111
  -7.500   0.0418   0.01223   0.00679  -0.1894   0.7391   0.0113
  -7.250   0.0692   0.01189   0.00639  -0.1895   0.7340   0.0115
  -7.000   0.0966   0.01159   0.00601  -0.1895   0.7291   0.0117
  -6.750   0.1245   0.01129   0.00566  -0.1897   0.7247   0.0119
  -6.500   0.1526   0.01100   0.00532  -0.1899   0.7198   0.0121
  -6.250   0.1804   0.01073   0.00499  -0.1900   0.7147   0.0123
  -6.000   0.2081   0.01050   0.00469  -0.1900   0.7098   0.0126
  -5.750   0.2367   0.01026   0.00440  -0.1902   0.7051   0.0128
  -5.500   0.2649   0.01005   0.00415  -0.1903   0.6996   0.0130
  -5.250   0.2926   0.00989   0.00392  -0.1903   0.6944   0.0132
  -5.000   0.3212   0.00963   0.00362  -0.1905   0.6895   0.0136
  -4.750   0.3496   0.00944   0.00340  -0.1907   0.6839   0.0142
  -4.500   0.3774   0.00931   0.00323  -0.1906   0.6782   0.0148
  -4.250   0.4059   0.00918   0.00306  -0.1908   0.6730   0.0154
  -4.000   0.4342   0.00906   0.00291  -0.1908   0.6670   0.0159
  -3.750   0.4619   0.00897   0.00276  -0.1908   0.6607   0.0165
  -3.500   0.4905   0.00884   0.00262  -0.1909   0.6552   0.0175
  -3.250   0.5186   0.00876   0.00251  -0.1909   0.6486   0.0187
  -3.000   0.5461   0.00870   0.00241  -0.1908   0.6423   0.0204
  -2.750   0.5746   0.00861   0.00231  -0.1909   0.6359   0.0242
  -2.500   0.6023   0.00853   0.00224  -0.1909   0.6289   0.0332
  -2.250   0.6302   0.00845   0.00218  -0.1909   0.6225   0.0468
  -2.000   0.6582   0.00838   0.00213  -0.1910   0.6154   0.0603
  -1.750   0.6853   0.00835   0.00211  -0.1908   0.6083   0.0742
  -1.500   0.7134   0.00830   0.00208  -0.1909   0.6011   0.0917
  -1.250   0.7404   0.00827   0.00208  -0.1908   0.5934   0.1157
  -1.000   0.7683   0.00820   0.00209  -0.1909   0.5862   0.1484
  -0.750   0.7954   0.00817   0.00211  -0.1908   0.5781   0.1808
  -0.500   0.8228   0.00815   0.00214  -0.1908   0.5707   0.2149
  -0.250   0.8496   0.00817   0.00218  -0.1906   0.5623   0.2430
   0.000   0.8765   0.00818   0.00223  -0.1904   0.5546   0.2717
   0.250   0.9032   0.00820   0.00230  -0.1903   0.5458   0.3059
   0.500   0.9296   0.00825   0.00236  -0.1900   0.5380   0.3362
   0.750   0.9559   0.00829   0.00244  -0.1898   0.5292   0.3682
   1.000   0.9821   0.00835   0.00253  -0.1895   0.5213   0.3989
   1.250   1.0079   0.00843   0.00263  -0.1892   0.5124   0.4279
   1.500   1.0335   0.00851   0.00273  -0.1888   0.5040   0.4567
   1.750   1.0588   0.00860   0.00285  -0.1883   0.4951   0.4871
   2.000   1.0840   0.00870   0.00297  -0.1879   0.4868   0.5158
   2.250   1.1085   0.00882   0.00310  -0.1873   0.4774   0.5444
   2.500   1.1334   0.00893   0.00323  -0.1867   0.4694   0.5725
   2.750   1.1570   0.00907   0.00339  -0.1860   0.4600   0.6001
   3.000   1.1808   0.00918   0.00353  -0.1853   0.4520   0.6293
   3.250   1.2026   0.00933   0.00370  -0.1841   0.4429   0.6587
   3.500   1.2253   0.00945   0.00385  -0.1832   0.4350   0.6898
   3.750   1.2462   0.00962   0.00405  -0.1819   0.4258   0.7235
   4.000   1.2683   0.00974   0.00424  -0.1808   0.4180   0.7631
   4.250   1.2879   0.00991   0.00447  -0.1793   0.4089   0.8139
   4.500   1.3011   0.00984   0.00465  -0.1762   0.4019   0.9422
   4.750   1.3218   0.01008   0.00485  -0.1750   0.3928   1.0000
   5.000   1.3433   0.01031   0.00505  -0.1739   0.3850   1.0000
   5.500   1.3841   0.01087   0.00552  -0.1714   0.3680   1.0000
   5.750   1.4030   0.01120   0.00580  -0.1699   0.3595   1.0000
   6.000   1.4236   0.01147   0.00605  -0.1688   0.3523   1.0000
   6.250   1.4420   0.01183   0.00636  -0.1672   0.3436   1.0000
   6.500   1.4615   0.01214   0.00666  -0.1659   0.3363   1.0000
   6.750   1.4791   0.01254   0.00702  -0.1644   0.3276   1.0000
   7.000   1.4981   0.01289   0.00735  -0.1630   0.3206   1.0000
   7.250   1.5154   0.01331   0.00774  -0.1614   0.3127   1.0000
   7.500   1.5335   0.01372   0.00813  -0.1600   0.3060   1.0000
   7.750   1.5503   0.01418   0.00856  -0.1584   0.2981   1.0000
   8.000   1.5668   0.01466   0.00903  -0.1568   0.2905   1.0000
   8.250   1.5831   0.01517   0.00952  -0.1552   0.2829   1.0000
   8.500   1.5987   0.01572   0.01005  -0.1536   0.2758   1.0000
   8.750   1.6151   0.01625   0.01057  -0.1521   0.2690   1.0000
   9.000   1.6288   0.01693   0.01122  -0.1502   0.2609   1.0000
   9.250   1.6445   0.01753   0.01181  -0.1487   0.2538   1.0000
   9.500   1.6573   0.01829   0.01255  -0.1469   0.2462   1.0000
   9.750   1.6724   0.01895   0.01321  -0.1454   0.2392   1.0000
  10.000   1.6841   0.01982   0.01405  -0.1435   0.2313   1.0000
  10.250   1.6982   0.02057   0.01480  -0.1420   0.2244   1.0000
  10.500   1.7091   0.02154   0.01575  -0.1401   0.2167   1.0000
  10.750   1.7220   0.02240   0.01662  -0.1386   0.2094   1.0000
  11.000   1.7317   0.02350   0.01769  -0.1367   0.2014   1.0000
  11.250   1.7440   0.02446   0.01865  -0.1353   0.1950   1.0000
  11.500   1.7528   0.02568   0.01986  -0.1334   0.1870   1.0000
  11.750   1.7640   0.02677   0.02096  -0.1320   0.1807   1.0000
  12.000   1.7723   0.02810   0.02227  -0.1303   0.1735   1.0000
  12.250   1.7821   0.02935   0.02353  -0.1288   0.1669   1.0000
  12.500   1.7894   0.03083   0.02500  -0.1271   0.1599   1.0000
  12.750   1.7988   0.03218   0.02636  -0.1258   0.1541   1.0000
  13.000   1.8051   0.03383   0.02801  -0.1242   0.1473   1.0000
  13.250   1.8137   0.03531   0.02951  -0.1229   0.1420   1.0000
  13.500   1.8196   0.03708   0.03128  -0.1215   0.1357   1.0000
  13.750   1.8257   0.03887   0.03308  -0.1202   0.1298   1.0000
  14.000   1.8317   0.04072   0.03495  -0.1190   0.1240   1.0000
  14.250   1.8359   0.04279   0.03703  -0.1178   0.1186   1.0000
  14.500   1.8413   0.04478   0.03903  -0.1167   0.1128   1.0000
  14.750   1.8433   0.04716   0.04142  -0.1156   0.1072   1.0000
  15.000   1.8469   0.04946   0.04373  -0.1146   0.1013   1.0000
  15.250   1.8482   0.05204   0.04632  -0.1137   0.0957   1.0000
  15.500   1.8515   0.05447   0.04879  -0.1129   0.0912   1.0000
  15.750   1.8511   0.05736   0.05169  -0.1121   0.0860   1.0000
  16.000   1.8554   0.05977   0.05415  -0.1116   0.0829   1.0000
  16.250   1.8569   0.06258   0.05700  -0.1111   0.0793   1.0000
  16.500   1.8556   0.06578   0.06022  -0.1106   0.0752   1.0000
  16.750   1.8576   0.06861   0.06311  -0.1103   0.0717   1.0000
  17.000   1.8539   0.07223   0.06675  -0.1101   0.0672   1.0000
  17.250   1.8536   0.07550   0.07007  -0.1100   0.0643   1.0000
  17.500   1.8523   0.07893   0.07355  -0.1100   0.0609   1.0000
  17.750   1.8486   0.08275   0.07741  -0.1101   0.0578   1.0000
  18.000   1.8476   0.08625   0.08098  -0.1104   0.0556   1.0000
  18.250   1.8450   0.09001   0.08480  -0.1107   0.0530   1.0000
  18.500   1.8401   0.09416   0.08899  -0.1112   0.0503   1.0000
  18.750   1.8375   0.09801   0.09292  -0.1118   0.0480   1.0000
  19.000   1.8326   0.10225   0.09722  -0.1126   0.0455   1.0000
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