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MH 114 13.02% (mh114-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 114 13.02% (mh114-il)
Reynolds number: 500,000
Max Cl/Cd: 120.96 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh114-il-500000-n5.txt
Download as CSV file: xf-mh114-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.1268   0.14231   0.13973  -0.0805   0.9785   0.0108
 -13.250  -0.1170   0.13822   0.13564  -0.0837   0.9763   0.0109
 -12.750  -0.1001   0.13117   0.12860  -0.0879   0.9684   0.0110
 -12.500  -0.0868   0.12828   0.12571  -0.0892   0.9650   0.0112
 -12.000  -0.0655   0.12215   0.11958  -0.0929   0.9560   0.0114
 -11.750  -0.0528   0.11884   0.11626  -0.0954   0.9524   0.0115
 -11.500  -0.0387   0.11528   0.11270  -0.0985   0.9497   0.0116
 -11.250  -0.0257   0.11181   0.10922  -0.1014   0.9450   0.0116
 -11.000  -0.0103   0.10824   0.10563  -0.1049   0.9410   0.0118
 -10.750   0.0070   0.10436   0.10173  -0.1091   0.9377   0.0119
 -10.500   0.0264   0.10045   0.09781  -0.1139   0.9346   0.0120
 -10.250   0.0453   0.09638   0.09371  -0.1189   0.9298   0.0120
  -9.750   0.0807   0.08516   0.08240  -0.1314   0.9191   0.0082
  -9.500   0.0998   0.08134   0.07854  -0.1363   0.9103   0.0080
  -9.250   0.1186   0.07801   0.07515  -0.1407   0.9016   0.0078
  -9.000   0.1312   0.07411   0.07119  -0.1445   0.8906   0.0076
  -8.750   0.1374   0.07032   0.06735  -0.1471   0.8788   0.0074
  -8.500   0.1407   0.06651   0.06350  -0.1492   0.8674   0.0071
  -8.250  -0.0306   0.02641   0.02269  -0.1790   0.8309   0.0059
  -8.000  -0.0179   0.02212   0.01783  -0.1826   0.8238   0.0059
  -7.750   0.0024   0.01978   0.01510  -0.1839   0.8173   0.0060
  -7.500   0.0262   0.01807   0.01304  -0.1848   0.8116   0.0061
  -7.250   0.0514   0.01682   0.01153  -0.1854   0.8064   0.0062
  -7.000   0.0771   0.01572   0.01022  -0.1859   0.8006   0.0063
  -6.750   0.1038   0.01478   0.00909  -0.1864   0.7955   0.0065
  -6.500   0.1309   0.01416   0.00835  -0.1867   0.7905   0.0068
  -6.250   0.1581   0.01363   0.00771  -0.1869   0.7850   0.0070
  -6.000   0.1858   0.01313   0.00708  -0.1872   0.7798   0.0073
  -5.750   0.2137   0.01266   0.00649  -0.1874   0.7749   0.0078
  -5.500   0.2415   0.01223   0.00596  -0.1876   0.7694   0.0082
  -5.250   0.2696   0.01182   0.00545  -0.1878   0.7641   0.0086
  -5.000   0.2978   0.01148   0.00504  -0.1881   0.7592   0.0092
  -4.750   0.3259   0.01119   0.00469  -0.1882   0.7536   0.0100
  -4.500   0.3541   0.01095   0.00436  -0.1884   0.7482   0.0111
  -4.250   0.3823   0.01072   0.00408  -0.1885   0.7431   0.0128
  -4.000   0.4105   0.01048   0.00381  -0.1887   0.7373   0.0152
  -3.750   0.4387   0.01029   0.00356  -0.1888   0.7317   0.0181
  -3.500   0.4670   0.01011   0.00335  -0.1889   0.7264   0.0224
  -3.250   0.4951   0.00994   0.00318  -0.1890   0.7203   0.0301
  -3.000   0.5232   0.00980   0.00302  -0.1892   0.7146   0.0401
  -2.750   0.5514   0.00965   0.00290  -0.1893   0.7087   0.0530
  -2.250   0.6075   0.00940   0.00269  -0.1895   0.6965   0.0959
  -2.000   0.6356   0.00927   0.00263  -0.1897   0.6899   0.1266
  -1.750   0.6633   0.00917   0.00258  -0.1897   0.6833   0.1605
  -1.500   0.6913   0.00908   0.00255  -0.1899   0.6769   0.1950
  -1.250   0.7190   0.00901   0.00253  -0.1899   0.6698   0.2315
  -1.000   0.7466   0.00894   0.00253  -0.1900   0.6631   0.2755
  -0.750   0.7742   0.00889   0.00254  -0.1900   0.6557   0.3174
  -0.500   0.8014   0.00886   0.00257  -0.1900   0.6486   0.3597
  -0.250   0.8288   0.00884   0.00261  -0.1899   0.6408   0.3995
   0.000   0.8555   0.00886   0.00266  -0.1898   0.6331   0.4379
   0.250   0.8827   0.00886   0.00272  -0.1897   0.6249   0.4774
   0.500   0.9090   0.00890   0.00279  -0.1894   0.6169   0.5147
   0.750   0.9356   0.00893   0.00287  -0.1892   0.6082   0.5515
   1.000   0.9615   0.00899   0.00296  -0.1889   0.5996   0.5865
   1.250   0.9875   0.00905   0.00306  -0.1885   0.5905   0.6207
   1.500   1.0131   0.00912   0.00317  -0.1881   0.5818   0.6548
   1.750   1.0380   0.00921   0.00329  -0.1875   0.5724   0.6897
   2.000   1.0630   0.00928   0.00341  -0.1870   0.5632   0.7263
   2.250   1.0865   0.00938   0.00356  -0.1861   0.5537   0.7659
   2.500   1.1094   0.00944   0.00370  -0.1851   0.5439   0.8124
   2.750   1.1277   0.00947   0.00382  -0.1830   0.5347   0.8762
   3.000   1.1466   0.00948   0.00387  -0.1810   0.5250   1.0000
   3.250   1.1709   0.00968   0.00401  -0.1805   0.5147   1.0000
   3.500   1.1942   0.00991   0.00418  -0.1797   0.5047   1.0000
   3.750   1.2176   0.01013   0.00435  -0.1789   0.4942   1.0000
   4.000   1.2406   0.01035   0.00453  -0.1781   0.4840   1.0000
   4.250   1.2617   0.01061   0.00472  -0.1769   0.4738   1.0000
   4.500   1.2830   0.01085   0.00493  -0.1757   0.4629   1.0000
   4.750   1.3038   0.01111   0.00515  -0.1745   0.4530   1.0000
   5.000   1.3233   0.01142   0.00540  -0.1730   0.4424   1.0000
   5.250   1.3441   0.01169   0.00565  -0.1718   0.4320   1.0000
   5.500   1.3637   0.01200   0.00592  -0.1704   0.4218   1.0000
   5.750   1.3821   0.01236   0.00623  -0.1688   0.4111   1.0000
   6.000   1.4022   0.01267   0.00652  -0.1676   0.4010   1.0000
   6.250   1.4206   0.01304   0.00686  -0.1661   0.3907   1.0000
   6.750   1.4571   0.01382   0.00758  -0.1630   0.3702   1.0000
   7.000   1.4744   0.01425   0.00800  -0.1614   0.3607   1.0000
   7.250   1.4913   0.01471   0.00843  -0.1597   0.3504   1.0000
   7.500   1.5087   0.01517   0.00887  -0.1581   0.3405   1.0000
   7.750   1.5244   0.01570   0.00938  -0.1564   0.3310   1.0000
   8.000   1.5405   0.01623   0.00990  -0.1547   0.3206   1.0000
   8.250   1.5563   0.01678   0.01045  -0.1530   0.3112   1.0000
   8.500   1.5704   0.01744   0.01108  -0.1511   0.3011   1.0000
   8.750   1.5856   0.01806   0.01170  -0.1494   0.2910   1.0000
   9.000   1.5999   0.01874   0.01238  -0.1477   0.2820   1.0000
   9.500   1.6263   0.02028   0.01391  -0.1440   0.2616   1.0000
   9.750   1.6386   0.02114   0.01476  -0.1422   0.2519   1.0000
  10.250   1.6618   0.02302   0.01663  -0.1385   0.2316   1.0000
  10.500   1.6726   0.02405   0.01766  -0.1367   0.2221   1.0000
  10.750   1.6817   0.02523   0.01884  -0.1347   0.2120   1.0000
  11.000   1.6917   0.02638   0.01999  -0.1330   0.2014   1.0000
  11.250   1.7010   0.02762   0.02123  -0.1312   0.1920   1.0000
  11.500   1.7084   0.02903   0.02263  -0.1294   0.1825   1.0000
  11.750   1.7167   0.03042   0.02402  -0.1277   0.1729   1.0000
  12.000   1.7242   0.03191   0.02553  -0.1260   0.1639   1.0000
  12.250   1.7299   0.03359   0.02721  -0.1243   0.1550   1.0000
  12.500   1.7365   0.03526   0.02889  -0.1228   0.1461   1.0000
  12.750   1.7423   0.03704   0.03069  -0.1213   0.1379   1.0000
  13.000   1.7463   0.03903   0.03268  -0.1197   0.1298   1.0000
  13.250   1.7522   0.04090   0.03459  -0.1184   0.1224   1.0000
  13.500   1.7553   0.04309   0.03680  -0.1171   0.1149   1.0000
  13.750   1.7585   0.04535   0.03908  -0.1158   0.1070   1.0000
  14.000   1.7618   0.04765   0.04141  -0.1147   0.1003   1.0000
  14.250   1.7625   0.05030   0.04407  -0.1136   0.0932   1.0000
  14.500   1.7656   0.05274   0.04656  -0.1128   0.0873   1.0000
  15.000   1.7681   0.05827   0.05219  -0.1112   0.0763   1.0000
  15.500   1.7675   0.06443   0.05843  -0.1101   0.0661   1.0000
  15.750   1.7643   0.06800   0.06205  -0.1097   0.0612   1.0000
  16.000   1.7638   0.07130   0.06542  -0.1095   0.0566   1.0000
  16.250   1.7596   0.07518   0.06934  -0.1095   0.0523   1.0000
  16.500   1.7580   0.07875   0.07298  -0.1095   0.0484   1.0000
  16.750   1.7531   0.08288   0.07716  -0.1097   0.0447   1.0000
  17.000   1.7505   0.08674   0.08112  -0.1101   0.0415   1.0000
  17.250   1.7454   0.09104   0.08549  -0.1106   0.0383   1.0000
  17.500   1.7410   0.09529   0.08981  -0.1112   0.0356   1.0000
  17.750   1.7356   0.09974   0.09434  -0.1120   0.0328   1.0000
  18.000   1.7291   0.10443   0.09911  -0.1130   0.0304   1.0000
  18.250   1.7241   0.10895   0.10371  -0.1141   0.0279   1.0000
  18.500   1.7167   0.11387   0.10871  -0.1155   0.0258   1.0000
  18.750   1.7114   0.11849   0.11343  -0.1169   0.0236   1.0000
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