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MH 201 13.08% (mh201-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 201 13.08% (mh201-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.58 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh201-il-1000000.txt
Download as CSV file: xf-mh201-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 201  13.08%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3041   0.12593   0.12438  -0.0378   1.0000   0.0090
 -12.500  -0.3041   0.12226   0.12072  -0.0389   0.9998   0.0093
 -12.250  -0.4041   0.12407   0.12236  -0.0370   1.0000   0.0087
 -12.000  -0.4051   0.11990   0.11820  -0.0380   1.0000   0.0086
 -11.750  -0.4057   0.11618   0.11451  -0.0388   1.0000   0.0088
  -8.500  -0.4664   0.02201   0.01778  -0.1009   0.9595   0.0080
  -8.250  -0.4460   0.01971   0.01538  -0.1005   0.9518   0.0075
  -8.000  -0.4155   0.01777   0.01322  -0.1021   0.9480   0.0074
  -7.750  -0.3831   0.01654   0.01183  -0.1037   0.9439   0.0075
  -7.500  -0.3538   0.01531   0.01044  -0.1046   0.9366   0.0075
  -7.250  -0.3205   0.01416   0.00916  -0.1062   0.9311   0.0075
  -7.000  -0.2937   0.01319   0.00808  -0.1065   0.9210   0.0074
  -6.750  -0.2666   0.01233   0.00711  -0.1067   0.9117   0.0073
  -6.500  -0.2399   0.01168   0.00636  -0.1069   0.9020   0.0073
  -6.250  -0.2156   0.01109   0.00568  -0.1064   0.8918   0.0074
  -6.000  -0.1900   0.01062   0.00512  -0.1062   0.8830   0.0074
  -5.750  -0.1646   0.01020   0.00462  -0.1059   0.8741   0.0075
  -5.500  -0.1386   0.00983   0.00418  -0.1057   0.8662   0.0077
  -5.250  -0.1124   0.00951   0.00379  -0.1055   0.8585   0.0079
  -5.000  -0.0864   0.00910   0.00330  -0.1053   0.8516   0.0089
  -4.750  -0.0597   0.00882   0.00297  -0.1052   0.8446   0.0112
  -4.500  -0.0331   0.00841   0.00262  -0.1051   0.8383   0.0293
  -4.250  -0.0069   0.00798   0.00238  -0.1051   0.8319   0.0711
  -4.000   0.0199   0.00762   0.00217  -0.1053   0.8258   0.1203
  -3.750   0.0470   0.00726   0.00201  -0.1055   0.8200   0.1772
  -3.500   0.0740   0.00679   0.00184  -0.1058   0.8139   0.2651
  -3.250   0.1013   0.00620   0.00166  -0.1063   0.8081   0.3935
  -3.000   0.1293   0.00585   0.00155  -0.1067   0.8022   0.4709
  -2.750   0.1576   0.00552   0.00146  -0.1071   0.7963   0.5583
  -2.500   0.1861   0.00539   0.00145  -0.1073   0.7908   0.6117
  -2.250   0.2146   0.00534   0.00144  -0.1074   0.7848   0.6417
  -2.000   0.2431   0.00536   0.00145  -0.1075   0.7789   0.6621
  -1.750   0.2717   0.00538   0.00146  -0.1076   0.7731   0.6769
  -1.500   0.3003   0.00542   0.00146  -0.1077   0.7669   0.6886
  -1.250   0.3286   0.00547   0.00149  -0.1077   0.7609   0.6975
  -1.000   0.3571   0.00549   0.00149  -0.1078   0.7544   0.7057
  -0.750   0.3852   0.00555   0.00152  -0.1078   0.7477   0.7123
  -0.500   0.4137   0.00559   0.00154  -0.1079   0.7409   0.7189
  -0.250   0.4417   0.00563   0.00156  -0.1079   0.7336   0.7242
   0.000   0.4698   0.00568   0.00159  -0.1079   0.7264   0.7294
   0.250   0.4979   0.00575   0.00161  -0.1079   0.7182   0.7347
   0.500   0.5257   0.00579   0.00165  -0.1079   0.7100   0.7399
   0.750   0.5530   0.00586   0.00170  -0.1077   0.7006   0.7451
   1.000   0.5810   0.00592   0.00174  -0.1077   0.6905   0.7496
   1.250   0.6085   0.00598   0.00177  -0.1076   0.6796   0.7531
   1.500   0.6353   0.00604   0.00181  -0.1074   0.6669   0.7563
   1.750   0.6620   0.00613   0.00185  -0.1072   0.6514   0.7595
   2.000   0.6886   0.00624   0.00191  -0.1069   0.6338   0.7628
   2.250   0.7146   0.00638   0.00198  -0.1065   0.6128   0.7659
   2.500   0.7398   0.00654   0.00205  -0.1060   0.5891   0.7691
   2.750   0.7644   0.00673   0.00216  -0.1054   0.5641   0.7724
   3.000   0.7891   0.00695   0.00228  -0.1048   0.5381   0.7758
   3.250   0.8135   0.00719   0.00243  -0.1042   0.5112   0.7789
   3.500   0.8379   0.00746   0.00257  -0.1036   0.4835   0.7817
   3.750   0.8621   0.00772   0.00272  -0.1030   0.4548   0.7841
   4.000   0.8860   0.00797   0.00288  -0.1023   0.4268   0.7866
   4.250   0.9097   0.00825   0.00306  -0.1017   0.3995   0.7891
   4.500   0.9334   0.00855   0.00325  -0.1010   0.3739   0.7916
   4.750   0.9569   0.00886   0.00346  -0.1003   0.3470   0.7942
   5.000   0.9808   0.00916   0.00366  -0.0997   0.3235   0.7967
   5.250   1.0039   0.00949   0.00388  -0.0989   0.2993   0.7989
   5.500   1.0272   0.00977   0.00410  -0.0982   0.2778   0.8016
   5.750   1.0502   0.01007   0.00434  -0.0975   0.2577   0.8041
   6.000   1.0728   0.01041   0.00459  -0.0966   0.2380   0.8067
   6.250   1.0956   0.01073   0.00485  -0.0959   0.2196   0.8093
   6.500   1.1181   0.01107   0.00512  -0.0951   0.2017   0.8121
   6.750   1.1405   0.01140   0.00539  -0.0942   0.1861   0.8146
   7.000   1.1623   0.01173   0.00568  -0.0933   0.1716   0.8174
   7.250   1.1836   0.01207   0.00599  -0.0923   0.1574   0.8202
   7.500   1.2048   0.01243   0.00631  -0.0912   0.1443   0.8233
   7.750   1.2255   0.01281   0.00664  -0.0901   0.1318   0.8265
   8.000   1.2451   0.01320   0.00698  -0.0888   0.1206   0.8296
   8.250   1.2631   0.01356   0.00733  -0.0872   0.1107   0.8330
   8.500   1.2819   0.01389   0.00767  -0.0857   0.1029   0.8365
   8.750   1.2997   0.01431   0.00807  -0.0841   0.0945   0.8405
   9.000   1.3175   0.01474   0.00847  -0.0825   0.0870   0.8445
   9.250   1.3352   0.01512   0.00890  -0.0809   0.0805   0.8489
   9.500   1.3512   0.01562   0.00937  -0.0791   0.0731   0.8537
   9.750   1.3694   0.01602   0.00981  -0.0776   0.0683   0.8586
  10.000   1.3842   0.01657   0.01034  -0.0757   0.0617   0.8641
  10.250   1.4012   0.01700   0.01082  -0.0741   0.0576   0.8706
  10.500   1.4152   0.01760   0.01142  -0.0722   0.0519   0.8779
  10.750   1.4307   0.01809   0.01196  -0.0705   0.0477   0.8868
  11.000   1.4430   0.01873   0.01262  -0.0683   0.0430   0.8977
  11.250   1.4564   0.01925   0.01322  -0.0663   0.0402   0.9134
  11.500   1.4643   0.01971   0.01381  -0.0632   0.0373   1.0000
  11.750   1.4779   0.02051   0.01461  -0.0617   0.0336   1.0000
  12.000   1.4923   0.02126   0.01539  -0.0603   0.0309   1.0000
  12.250   1.5035   0.02223   0.01634  -0.0586   0.0275   1.0000
  12.500   1.5170   0.02305   0.01720  -0.0572   0.0252   1.0000
  12.750   1.5269   0.02413   0.01828  -0.0554   0.0225   1.0000
  13.000   1.5390   0.02508   0.01928  -0.0540   0.0209   1.0000
  13.250   1.5491   0.02620   0.02042  -0.0525   0.0190   1.0000
  13.500   1.5580   0.02743   0.02171  -0.0510   0.0174   1.0000
  13.750   1.5681   0.02860   0.02293  -0.0496   0.0162   1.0000
  14.000   1.5759   0.02999   0.02435  -0.0482   0.0148   1.0000
  14.250   1.5830   0.03147   0.02589  -0.0468   0.0137   1.0000
  14.500   1.5913   0.03289   0.02738  -0.0457   0.0129   1.0000
  14.750   1.5974   0.03455   0.02909  -0.0445   0.0118   1.0000
  15.000   1.6014   0.03644   0.03103  -0.0433   0.0108   1.0000
  15.250   1.6078   0.03817   0.03284  -0.0424   0.0102   1.0000
  15.500   1.6123   0.04014   0.03489  -0.0415   0.0094   1.0000
  15.750   1.6147   0.04238   0.03720  -0.0407   0.0088   1.0000
  16.000   1.6163   0.04479   0.03968  -0.0400   0.0081   1.0000
  16.250   1.6193   0.04714   0.04212  -0.0396   0.0076   1.0000
  16.500   1.6198   0.04987   0.04492  -0.0393   0.0069   1.0000
  16.750   1.6178   0.05298   0.04811  -0.0392   0.0064   1.0000
  17.000   1.6165   0.05612   0.05136  -0.0393   0.0059   1.0000
  17.250   1.6147   0.05948   0.05482  -0.0396   0.0055   1.0000
  17.500   1.6105   0.06330   0.05873  -0.0403   0.0050   1.0000
  17.750   1.6022   0.06785   0.06337  -0.0413   0.0044   1.0000
  18.000   1.5968   0.07215   0.06780  -0.0425   0.0042   1.0000
  18.250   1.5872   0.07728   0.07303  -0.0442   0.0035   1.0000
  18.500   1.5721   0.08349   0.07936  -0.0465   0.0030   1.0000
  18.750   1.5610   0.08922   0.08523  -0.0489   0.0028   1.0000
  19.000   1.5471   0.09565   0.09180  -0.0518   0.0026   1.0000
  19.250   1.5304   0.10277   0.09907  -0.0552   0.0024   1.0000
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