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MH 113 14.62% (mh113-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 113 14.62% (mh113-il)
Reynolds number: 1,000,000
Max Cl/Cd: 152.95 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh113-il-1000000.txt
Download as CSV file: xf-mh113-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500   0.1639   0.08598   0.08381  -0.1508   0.9126   0.0172
 -10.250   0.1810   0.08288   0.08062  -0.1546   0.9000   0.0176
 -10.000   0.2010   0.06516   0.06275  -0.1478   0.8424   0.0197
  -9.750   0.2095   0.06331   0.06088  -0.1479   0.8351   0.0199
  -9.500   0.2154   0.06089   0.05842  -0.1482   0.8282   0.0201
  -9.250   0.0863   0.05017   0.04766  -0.1682   0.8430   0.0166
  -9.000  -0.0059   0.03347   0.03073  -0.1784   0.8244   0.0152
  -8.750  -0.0473   0.02252   0.01891  -0.1896   0.8111   0.0145
  -8.500  -0.0302   0.02077   0.01694  -0.1902   0.8054   0.0146
  -8.250  -0.0122   0.01874   0.01459  -0.1907   0.7997   0.0147
  -8.000   0.0093   0.01714   0.01272  -0.1911   0.7944   0.0147
  -7.750   0.0332   0.01599   0.01140  -0.1913   0.7896   0.0148
  -7.500   0.0582   0.01507   0.01032  -0.1914   0.7845   0.0150
  -7.250   0.0840   0.01432   0.00939  -0.1915   0.7794   0.0152
  -7.000   0.1105   0.01363   0.00859  -0.1916   0.7750   0.0155
  -6.750   0.1374   0.01306   0.00793  -0.1917   0.7702   0.0157
  -6.500   0.1645   0.01261   0.00737  -0.1918   0.7653   0.0160
  -6.250   0.1920   0.01224   0.00689  -0.1919   0.7605   0.0162
  -6.000   0.2192   0.01154   0.00612  -0.1920   0.7560   0.0164
  -5.750   0.2466   0.01094   0.00546  -0.1922   0.7511   0.0168
  -5.500   0.2744   0.01058   0.00504  -0.1924   0.7461   0.0172
  -5.250   0.3026   0.01028   0.00470  -0.1925   0.7416   0.0176
  -5.000   0.3309   0.00998   0.00438  -0.1927   0.7367   0.0180
  -4.750   0.3591   0.00975   0.00408  -0.1928   0.7316   0.0185
  -4.500   0.3874   0.00956   0.00382  -0.1929   0.7266   0.0191
  -4.250   0.4161   0.00927   0.00351  -0.1931   0.7219   0.0198
  -4.000   0.4445   0.00904   0.00325  -0.1932   0.7166   0.0210
  -3.750   0.4726   0.00891   0.00306  -0.1933   0.7113   0.0221
  -3.500   0.5013   0.00874   0.00287  -0.1934   0.7064   0.0233
  -3.250   0.5299   0.00856   0.00268  -0.1935   0.7009   0.0253
  -3.000   0.5580   0.00844   0.00252  -0.1935   0.6954   0.0291
  -2.750   0.5868   0.00822   0.00237  -0.1938   0.6902   0.0465
  -2.500   0.6154   0.00805   0.00227  -0.1940   0.6844   0.0712
  -2.250   0.6433   0.00796   0.00221  -0.1940   0.6785   0.0938
  -2.000   0.6717   0.00784   0.00217  -0.1942   0.6731   0.1191
  -1.750   0.7000   0.00775   0.00213  -0.1943   0.6669   0.1464
  -1.500   0.7275   0.00770   0.00212  -0.1942   0.6606   0.1761
  -1.250   0.7560   0.00759   0.00211  -0.1944   0.6547   0.2151
  -1.000   0.7839   0.00752   0.00212  -0.1945   0.6480   0.2582
  -0.750   0.8113   0.00748   0.00214  -0.1944   0.6416   0.2993
  -0.500   0.8394   0.00742   0.00217  -0.1946   0.6348   0.3420
  -0.250   0.8664   0.00742   0.00221  -0.1944   0.6277   0.3785
   0.000   0.8941   0.00740   0.00225  -0.1944   0.6210   0.4164
   0.250   0.9212   0.00741   0.00231  -0.1943   0.6134   0.4555
   0.500   0.9481   0.00743   0.00238  -0.1941   0.6063   0.4906
   0.750   0.9751   0.00746   0.00244  -0.1939   0.5986   0.5254
   1.000   1.0012   0.00752   0.00253  -0.1936   0.5911   0.5591
   1.250   1.0281   0.00755   0.00261  -0.1934   0.5833   0.5910
   1.500   1.0534   0.00764   0.00271  -0.1929   0.5751   0.6228
   1.750   1.0801   0.00768   0.00280  -0.1927   0.5673   0.6556
   2.000   1.1047   0.00779   0.00293  -0.1921   0.5587   0.6885
   2.250   1.1308   0.00783   0.00303  -0.1918   0.5506   0.7240
   2.500   1.1545   0.00794   0.00317  -0.1910   0.5418   0.7625
   2.750   1.1793   0.00797   0.00330  -0.1903   0.5335   0.8082
   3.000   1.1990   0.00803   0.00345  -0.1886   0.5249   0.8732
   3.250   1.2175   0.00796   0.00350  -0.1865   0.5167   1.0000
   3.500   1.2406   0.00817   0.00364  -0.1857   0.5077   1.0000
   3.750   1.2647   0.00832   0.00376  -0.1850   0.4989   1.0000
   4.000   1.2860   0.00853   0.00390  -0.1838   0.4900   1.0000
   4.250   1.3085   0.00871   0.00405  -0.1828   0.4808   1.0000
   4.500   1.3294   0.00893   0.00422  -0.1815   0.4721   1.0000
   4.750   1.3506   0.00915   0.00440  -0.1803   0.4626   1.0000
   5.000   1.3716   0.00938   0.00459  -0.1791   0.4540   1.0000
   5.250   1.3918   0.00964   0.00480  -0.1778   0.4443   1.0000
   5.500   1.4127   0.00987   0.00501  -0.1766   0.4357   1.0000
   5.750   1.4318   0.01017   0.00525  -0.1750   0.4265   1.0000
   6.000   1.4528   0.01042   0.00547  -0.1739   0.4181   1.0000
   6.500   1.4912   0.01102   0.00602  -0.1710   0.4005   1.0000
   6.750   1.5084   0.01141   0.00635  -0.1693   0.3914   1.0000
   7.000   1.5285   0.01169   0.00663  -0.1681   0.3833   1.0000
   7.250   1.5448   0.01211   0.00700  -0.1663   0.3748   1.0000
   7.500   1.5645   0.01242   0.00731  -0.1650   0.3669   1.0000
   7.750   1.5798   0.01290   0.00775  -0.1631   0.3581   1.0000
   8.000   1.5987   0.01326   0.00811  -0.1618   0.3505   1.0000
   8.250   1.6133   0.01380   0.00860  -0.1598   0.3420   1.0000
   8.500   1.6317   0.01419   0.00900  -0.1585   0.3348   1.0000
   9.000   1.6629   0.01525   0.01003  -0.1552   0.3189   1.0000
   9.500   1.6926   0.01644   0.01119  -0.1517   0.3033   1.0000
   9.750   1.7056   0.01716   0.01188  -0.1498   0.2953   1.0000
  10.000   1.7208   0.01777   0.01251  -0.1483   0.2880   1.0000
  10.250   1.7329   0.01858   0.01329  -0.1464   0.2797   1.0000
  10.500   1.7472   0.01929   0.01400  -0.1448   0.2727   1.0000
  10.750   1.7584   0.02019   0.01488  -0.1429   0.2643   1.0000
  11.000   1.7717   0.02099   0.01569  -0.1414   0.2572   1.0000
  11.250   1.7821   0.02200   0.01668  -0.1395   0.2491   1.0000
  11.500   1.7945   0.02291   0.01760  -0.1380   0.2421   1.0000
  11.750   1.8041   0.02402   0.01870  -0.1361   0.2342   1.0000
  12.000   1.8152   0.02506   0.01975  -0.1346   0.2268   1.0000
  12.250   1.8234   0.02633   0.02100  -0.1328   0.2189   1.0000
  12.500   1.8340   0.02747   0.02216  -0.1313   0.2119   1.0000
  12.750   1.8409   0.02892   0.02359  -0.1295   0.2040   1.0000
  13.000   1.8502   0.03022   0.02490  -0.1280   0.1968   1.0000
  13.250   1.8565   0.03180   0.02647  -0.1264   0.1894   1.0000
  13.500   1.8643   0.03330   0.02798  -0.1249   0.1822   1.0000
  13.750   1.8691   0.03508   0.02975  -0.1233   0.1744   1.0000
  14.000   1.8761   0.03673   0.03142  -0.1220   0.1679   1.0000
  14.250   1.8795   0.03874   0.03342  -0.1205   0.1605   1.0000
  14.500   1.8855   0.04058   0.03527  -0.1193   0.1535   1.0000
  14.750   1.8870   0.04288   0.03756  -0.1179   0.1464   1.0000
  15.000   1.8926   0.04483   0.03954  -0.1168   0.1400   1.0000
  15.250   1.8930   0.04736   0.04207  -0.1156   0.1332   1.0000
  15.500   1.8978   0.04950   0.04425  -0.1147   0.1283   1.0000
  15.750   1.8995   0.05203   0.04678  -0.1138   0.1225   1.0000
  16.000   1.9016   0.05455   0.04934  -0.1130   0.1178   1.0000
  16.250   1.9034   0.05718   0.05200  -0.1122   0.1126   1.0000
  16.500   1.9018   0.06025   0.05508  -0.1115   0.1068   1.0000
  16.750   1.9035   0.06300   0.05787  -0.1110   0.1023   1.0000
  17.000   1.8998   0.06646   0.06136  -0.1106   0.0970   1.0000
  17.250   1.9014   0.06933   0.06428  -0.1103   0.0933   1.0000
  17.500   1.8995   0.07268   0.06766  -0.1100   0.0890   1.0000
  17.750   1.8953   0.07643   0.07145  -0.1099   0.0849   1.0000
  18.000   1.8951   0.07970   0.07478  -0.1100   0.0816   1.0000
  18.250   1.8906   0.08358   0.07870  -0.1101   0.0776   1.0000
  18.500   1.8866   0.08746   0.08263  -0.1104   0.0742   1.0000
  18.750   1.8831   0.09132   0.08656  -0.1108   0.0710   1.0000
  19.000   1.8766   0.09567   0.09095  -0.1113   0.0677   1.0000
  19.250   1.8733   0.09959   0.09493  -0.1119   0.0650   1.0000
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