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MH 201 13.08% (mh201-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 201 13.08% (mh201-il)
Reynolds number: 500,000
Max Cl/Cd: 85.1 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh201-il-500000-n5.txt
Download as CSV file: xf-mh201-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.5588   0.06106   0.05858  -0.0651   0.9994   0.0055
 -10.750  -0.5727   0.05105   0.04833  -0.0772   0.9959   0.0053
 -10.500  -0.5897   0.04347   0.04045  -0.0848   0.9902   0.0052
 -10.250  -0.5957   0.03802   0.03461  -0.0897   0.9840   0.0054
 -10.000  -0.6016   0.03400   0.03027  -0.0908   0.9732   0.0053
  -9.750  -0.5945   0.03116   0.02711  -0.0910   0.9638   0.0054
  -9.500  -0.5800   0.02815   0.02373  -0.0920   0.9583   0.0054
  -9.250  -0.5665   0.02605   0.02137  -0.0915   0.9496   0.0054
  -9.000  -0.5427   0.02385   0.01887  -0.0927   0.9460   0.0054
  -8.750  -0.5210   0.02214   0.01691  -0.0929   0.9392   0.0054
  -8.500  -0.4920   0.02057   0.01512  -0.0944   0.9350   0.0055
  -8.250  -0.4601   0.01911   0.01345  -0.0962   0.9317   0.0055
  -8.000  -0.4322   0.01802   0.01221  -0.0970   0.9256   0.0055
  -7.750  -0.4012   0.01698   0.01104  -0.0984   0.9203   0.0056
  -7.500  -0.3697   0.01601   0.00994  -0.0999   0.9149   0.0056
  -7.250  -0.3418   0.01514   0.00897  -0.1005   0.9070   0.0057
  -7.000  -0.3124   0.01430   0.00803  -0.1015   0.9004   0.0058
  -6.750  -0.2867   0.01361   0.00726  -0.1016   0.8921   0.0060
  -6.500  -0.2582   0.01308   0.00665  -0.1021   0.8851   0.0062
  -6.250  -0.2325   0.01261   0.00611  -0.1021   0.8769   0.0066
  -6.000  -0.2048   0.01220   0.00562  -0.1023   0.8702   0.0068
  -5.750  -0.1790   0.01184   0.00518  -0.1021   0.8624   0.0073
  -5.500  -0.1517   0.01148   0.00472  -0.1022   0.8557   0.0081
  -5.250  -0.1257   0.01116   0.00436  -0.1021   0.8485   0.0089
  -5.000  -0.0986   0.01087   0.00401  -0.1020   0.8418   0.0110
  -4.750  -0.0720   0.01058   0.00371  -0.1020   0.8354   0.0157
  -4.250  -0.0186   0.00990   0.00316  -0.1021   0.8230   0.0564
  -4.000   0.0073   0.00943   0.00292  -0.1021   0.8167   0.1092
  -3.750   0.0337   0.00893   0.00268  -0.1024   0.8108   0.1858
  -3.500   0.0608   0.00854   0.00250  -0.1026   0.8053   0.2495
  -3.250   0.0879   0.00814   0.00233  -0.1029   0.7993   0.3208
  -3.000   0.1157   0.00769   0.00216  -0.1034   0.7938   0.4166
  -2.750   0.1436   0.00740   0.00206  -0.1037   0.7880   0.4770
  -2.500   0.1716   0.00717   0.00198  -0.1039   0.7818   0.5376
  -2.250   0.1997   0.00703   0.00196  -0.1041   0.7760   0.5891
  -2.000   0.2276   0.00698   0.00198  -0.1040   0.7695   0.6244
  -1.750   0.2557   0.00699   0.00199  -0.1040   0.7632   0.6481
  -1.500   0.2838   0.00702   0.00201  -0.1040   0.7568   0.6653
  -1.250   0.3119   0.00706   0.00202  -0.1040   0.7497   0.6782
  -1.000   0.3402   0.00710   0.00202  -0.1040   0.7430   0.6894
  -0.750   0.3680   0.00715   0.00204  -0.1040   0.7354   0.6981
  -0.500   0.3961   0.00720   0.00205  -0.1040   0.7280   0.7061
  -0.250   0.4236   0.00726   0.00209  -0.1039   0.7194   0.7138
   0.000   0.4514   0.00732   0.00211  -0.1038   0.7108   0.7219
   0.250   0.4786   0.00739   0.00216  -0.1036   0.7012   0.7282
   0.500   0.5062   0.00745   0.00218  -0.1035   0.6907   0.7338
   0.750   0.5334   0.00751   0.00221  -0.1034   0.6794   0.7379
   1.000   0.5601   0.00758   0.00225  -0.1031   0.6665   0.7416
   1.250   0.5867   0.00767   0.00229  -0.1028   0.6518   0.7456
   1.500   0.6131   0.00778   0.00233  -0.1025   0.6344   0.7497
   1.750   0.6388   0.00790   0.00238  -0.1021   0.6144   0.7534
   2.250   0.6882   0.00824   0.00257  -0.1008   0.5697   0.7611
   2.500   0.7125   0.00847   0.00268  -0.1001   0.5447   0.7648
   2.750   0.7369   0.00870   0.00280  -0.0995   0.5192   0.7679
   3.000   0.7605   0.00894   0.00295  -0.0987   0.4937   0.7703
   3.250   0.7838   0.00921   0.00313  -0.0979   0.4670   0.7730
   3.500   0.8071   0.00949   0.00330  -0.0971   0.4397   0.7757
   3.750   0.8304   0.00979   0.00349  -0.0964   0.4129   0.7785
   4.000   0.8538   0.01010   0.00369  -0.0957   0.3875   0.7814
   4.250   0.8768   0.01042   0.00391  -0.0949   0.3622   0.7839
   4.500   0.8996   0.01072   0.00413  -0.0941   0.3382   0.7862
   4.750   0.9221   0.01105   0.00438  -0.0932   0.3154   0.7887
   5.000   0.9449   0.01137   0.00463  -0.0925   0.2936   0.7914
   5.250   0.9677   0.01170   0.00489  -0.0917   0.2736   0.7941
   5.750   1.0124   0.01239   0.00545  -0.0900   0.2362   0.7996
   6.000   1.0341   0.01273   0.00574  -0.0891   0.2190   0.8021
   6.250   1.0557   0.01308   0.00605  -0.0881   0.2030   0.8046
   6.500   1.0772   0.01343   0.00637  -0.0871   0.1890   0.8076
   6.750   1.0984   0.01380   0.00671  -0.0861   0.1749   0.8109
   7.000   1.1188   0.01419   0.00705  -0.0850   0.1614   0.8139
   7.250   1.1376   0.01457   0.00741  -0.0835   0.1491   0.8166
   7.500   1.1560   0.01495   0.00779  -0.0820   0.1376   0.8196
   7.750   1.1750   0.01532   0.00817  -0.0806   0.1281   0.8232
   8.000   1.1934   0.01576   0.00859  -0.0791   0.1184   0.8270
   8.250   1.2110   0.01623   0.00904  -0.0776   0.1092   0.8306
   8.500   1.2291   0.01664   0.00949  -0.0761   0.1014   0.8342
   8.750   1.2462   0.01713   0.00999  -0.0745   0.0937   0.8383
   9.000   1.2631   0.01763   0.01050  -0.0729   0.0865   0.8427
   9.250   1.2799   0.01812   0.01103  -0.0714   0.0809   0.8473
   9.500   1.2958   0.01865   0.01160  -0.0697   0.0749   0.8527
   9.750   1.3116   0.01922   0.01220  -0.0680   0.0698   0.8586
  10.000   1.3267   0.01978   0.01281  -0.0663   0.0649   0.8645
  10.250   1.3405   0.02044   0.01350  -0.0645   0.0600   0.8717
  10.500   1.3547   0.02104   0.01417  -0.0627   0.0555   0.8795
  10.750   1.3667   0.02179   0.01496  -0.0607   0.0511   0.8896
  11.000   1.3791   0.02243   0.01569  -0.0587   0.0478   0.9032
  11.250   1.3885   0.02312   0.01647  -0.0563   0.0444   0.9276
  11.500   1.3990   0.02391   0.01733  -0.0543   0.0413   1.0000
  11.750   1.4128   0.02479   0.01826  -0.0531   0.0384   1.0000
  12.000   1.4246   0.02583   0.01933  -0.0517   0.0353   1.0000
  12.250   1.4363   0.02689   0.02045  -0.0503   0.0329   1.0000
  12.500   1.4476   0.02800   0.02161  -0.0490   0.0304   1.0000
  12.750   1.4567   0.02930   0.02295  -0.0476   0.0280   1.0000
  13.000   1.4671   0.03054   0.02425  -0.0464   0.0261   1.0000
  13.250   1.4757   0.03193   0.02570  -0.0452   0.0238   1.0000
  13.500   1.4828   0.03351   0.02732  -0.0440   0.0218   1.0000
  13.750   1.4908   0.03504   0.02892  -0.0429   0.0199   1.0000
  14.000   1.4956   0.03689   0.03080  -0.0418   0.0177   1.0000
  14.250   1.5020   0.03864   0.03265  -0.0409   0.0161   1.0000
  14.500   1.5061   0.04068   0.03475  -0.0400   0.0145   1.0000
  14.750   1.5098   0.04281   0.03696  -0.0392   0.0132   1.0000
  15.000   1.5127   0.04510   0.03932  -0.0386   0.0117   1.0000
  15.250   1.5139   0.04766   0.04196  -0.0381   0.0108   1.0000
  15.500   1.5162   0.05020   0.04460  -0.0378   0.0100   1.0000
  15.750   1.5170   0.05300   0.04751  -0.0377   0.0094   1.0000
  16.000   1.5159   0.05613   0.05074  -0.0378   0.0087   1.0000
  16.250   1.5138   0.05953   0.05424  -0.0381   0.0082   1.0000
  16.500   1.5120   0.06303   0.05786  -0.0387   0.0077   1.0000
  16.750   1.5088   0.06685   0.06182  -0.0395   0.0073   1.0000
  17.000   1.5038   0.07107   0.06616  -0.0406   0.0069   1.0000
  17.250   1.4975   0.07565   0.07087  -0.0421   0.0066   1.0000
  17.500   1.4894   0.08071   0.07605  -0.0439   0.0063   1.0000
  17.750   1.4808   0.08598   0.08146  -0.0459   0.0060   1.0000
  18.000   1.4712   0.09158   0.08721  -0.0483   0.0058   1.0000
  18.250   1.4601   0.09762   0.09340  -0.0511   0.0056   1.0000
  18.500   1.4476   0.10407   0.09999  -0.0542   0.0053   1.0000
  18.750   1.4340   0.11085   0.10692  -0.0577   0.0052   1.0000
  19.000   1.4193   0.11797   0.11419  -0.0614   0.0051   1.0000
  19.250   1.4039   0.12540   0.12177  -0.0656   0.0050   1.0000
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