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MH 201 13.08% (mh201-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 201 13.08% (mh201-il)
Reynolds number: 200,000
Max Cl/Cd: 67.05 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh201-il-200000-n5.txt
Download as CSV file: xf-mh201-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.4204   0.09388   0.09029  -0.0488   1.0000   0.0122
 -10.250  -0.4985   0.06791   0.06425  -0.0621   1.0000   0.0104
 -10.000  -0.5261   0.06213   0.05842  -0.0645   1.0000   0.0104
  -9.500  -0.5503   0.05186   0.04782  -0.0735   0.9904   0.0102
  -9.250  -0.5538   0.04747   0.04317  -0.0774   0.9808   0.0102
  -9.000  -0.5487   0.04272   0.03804  -0.0806   0.9721   0.0101
  -8.750  -0.5430   0.03898   0.03391  -0.0813   0.9625   0.0100
  -8.500  -0.5300   0.03548   0.03000  -0.0823   0.9558   0.0100
  -8.250  -0.5141   0.03228   0.02636  -0.0827   0.9492   0.0100
  -8.000  -0.4895   0.02952   0.02318  -0.0841   0.9459   0.0100
  -7.750  -0.4708   0.02747   0.02082  -0.0835   0.9386   0.0100
  -7.500  -0.4443   0.02540   0.01840  -0.0841   0.9348   0.0102
  -7.250  -0.4145   0.02369   0.01641  -0.0852   0.9324   0.0103
  -7.000  -0.3895   0.02237   0.01493  -0.0852   0.9272   0.0105
  -6.750  -0.3630   0.02111   0.01361  -0.0856   0.9224   0.0109
  -6.500  -0.3317   0.02003   0.01244  -0.0869   0.9193   0.0112
  -6.250  -0.2990   0.01900   0.01131  -0.0884   0.9169   0.0121
  -6.000  -0.2747   0.01821   0.01043  -0.0882   0.9106   0.0126
  -5.750  -0.2450   0.01739   0.00950  -0.0890   0.9062   0.0136
  -5.500  -0.2123   0.01669   0.00876  -0.0905   0.9030   0.0162
  -5.250  -0.1827   0.01605   0.00806  -0.0913   0.8985   0.0188
  -5.000  -0.1552   0.01542   0.00736  -0.0915   0.8926   0.0230
  -4.750  -0.1234   0.01470   0.00665  -0.0927   0.8886   0.0346
  -4.500  -0.0923   0.01386   0.00603  -0.0940   0.8847   0.0760
  -4.250  -0.0676   0.01308   0.00564  -0.0942   0.8779   0.1581
  -4.000  -0.0373   0.01229   0.00525  -0.0955   0.8733   0.2554
  -3.750  -0.0071   0.01156   0.00491  -0.0967   0.8688   0.3640
  -3.500   0.0184   0.01096   0.00477  -0.0967   0.8623   0.4776
  -3.250   0.0477   0.01067   0.00475  -0.0970   0.8576   0.5603
  -3.000   0.0760   0.01063   0.00481  -0.0968   0.8525   0.6138
  -2.750   0.1026   0.01069   0.00488  -0.0962   0.8462   0.6473
  -2.500   0.1333   0.01074   0.00486  -0.0965   0.8414   0.6722
  -2.250   0.1614   0.01083   0.00487  -0.0964   0.8356   0.6899
  -2.000   0.1895   0.01090   0.00487  -0.0963   0.8294   0.7046
  -1.750   0.2198   0.01096   0.00486  -0.0965   0.8245   0.7159
  -1.500   0.2454   0.01105   0.00491  -0.0959   0.8174   0.7259
  -1.250   0.2750   0.01110   0.00486  -0.0961   0.8112   0.7364
  -1.000   0.3016   0.01118   0.00492  -0.0956   0.8047   0.7443
  -0.750   0.3289   0.01125   0.00493  -0.0953   0.7975   0.7537
  -0.500   0.3568   0.01131   0.00495  -0.0951   0.7913   0.7609
  -0.250   0.3837   0.01135   0.00495  -0.0949   0.7832   0.7682
   0.000   0.4117   0.01138   0.00494  -0.0946   0.7765   0.7727
   0.250   0.4373   0.01142   0.00496  -0.0941   0.7678   0.7782
   0.500   0.4668   0.01144   0.00491  -0.0944   0.7603   0.7837
   0.750   0.4916   0.01147   0.00496  -0.0937   0.7509   0.7877
   1.000   0.5184   0.01150   0.00496  -0.0933   0.7420   0.7925
   1.250   0.5467   0.01153   0.00494  -0.0934   0.7324   0.7980
   1.500   0.5715   0.01156   0.00499  -0.0927   0.7217   0.8018
   1.750   0.5975   0.01159   0.00501  -0.0922   0.7111   0.8057
   2.000   0.6246   0.01162   0.00500  -0.0920   0.6996   0.8100
   2.250   0.6513   0.01166   0.00502  -0.0918   0.6863   0.8143
   2.500   0.6757   0.01169   0.00507  -0.0910   0.6721   0.8172
   2.750   0.7006   0.01174   0.00511  -0.0903   0.6564   0.8205
   3.000   0.7260   0.01181   0.00514  -0.0898   0.6389   0.8242
   3.250   0.7516   0.01190   0.00518  -0.0894   0.6188   0.8280
   3.500   0.7756   0.01202   0.00525  -0.0886   0.5965   0.8311
   3.750   0.7984   0.01217   0.00533  -0.0875   0.5730   0.8342
   4.000   0.8209   0.01238   0.00544  -0.0865   0.5477   0.8376
   4.250   0.8435   0.01262   0.00561  -0.0855   0.5209   0.8415
   4.500   0.8656   0.01291   0.00579  -0.0846   0.4933   0.8452
   4.750   0.8852   0.01321   0.00600  -0.0830   0.4663   0.8483
   5.000   0.9044   0.01356   0.00626  -0.0815   0.4386   0.8521
   5.250   0.9244   0.01392   0.00654  -0.0802   0.4114   0.8563
   5.500   0.9444   0.01431   0.00684  -0.0789   0.3849   0.8602
   5.750   0.9618   0.01470   0.00715  -0.0771   0.3607   0.8638
   6.000   0.9801   0.01510   0.00750  -0.0756   0.3364   0.8682
   6.250   0.9985   0.01554   0.00788  -0.0741   0.3141   0.8731
   6.500   1.0162   0.01596   0.00825  -0.0725   0.2924   0.8773
   6.750   1.0324   0.01639   0.00864  -0.0706   0.2724   0.8821
   7.250   1.0638   0.01729   0.00949  -0.0667   0.2368   0.8938
   7.500   1.0795   0.01776   0.00995  -0.0648   0.2205   0.9005
   7.750   1.0948   0.01826   0.01044  -0.0629   0.2051   0.9076
   8.000   1.1094   0.01876   0.01096  -0.0609   0.1910   0.9167
   8.250   1.1227   0.01927   0.01148  -0.0587   0.1781   0.9290
   8.500   1.1366   0.01979   0.01202  -0.0567   0.1655   0.9490
   8.750   1.1541   0.02035   0.01260  -0.0557   0.1530   1.0000
   9.000   1.1726   0.02107   0.01334  -0.0549   0.1416   1.0000
   9.250   1.1898   0.02183   0.01411  -0.0539   0.1312   1.0000
   9.500   1.2055   0.02268   0.01495  -0.0528   0.1219   1.0000
   9.750   1.2219   0.02349   0.01578  -0.0518   0.1129   1.0000
  10.000   1.2369   0.02437   0.01671  -0.0506   0.1052   1.0000
  10.250   1.2506   0.02534   0.01769  -0.0494   0.0978   1.0000
  10.500   1.2651   0.02626   0.01868  -0.0482   0.0913   1.0000
  10.750   1.2771   0.02736   0.01979  -0.0469   0.0851   1.0000
  11.000   1.2902   0.02840   0.02092  -0.0457   0.0797   1.0000
  11.250   1.3017   0.02957   0.02213  -0.0444   0.0744   1.0000
  11.500   1.3121   0.03085   0.02348  -0.0432   0.0700   1.0000
  11.750   1.3235   0.03207   0.02480  -0.0420   0.0653   1.0000
  12.000   1.3310   0.03361   0.02637  -0.0408   0.0613   1.0000
  12.250   1.3415   0.03497   0.02785  -0.0397   0.0575   1.0000
  12.500   1.3499   0.03651   0.02947  -0.0387   0.0536   1.0000
  12.750   1.3547   0.03841   0.03140  -0.0376   0.0505   1.0000
  13.000   1.3634   0.04001   0.03318  -0.0367   0.0474   1.0000
  13.250   1.3694   0.04191   0.03516  -0.0359   0.0444   1.0000
  13.500   1.3713   0.04423   0.03753  -0.0351   0.0420   1.0000
  13.750   1.3768   0.04628   0.03974  -0.0344   0.0397   1.0000
  14.000   1.3808   0.04855   0.04215  -0.0339   0.0373   1.0000
  14.250   1.3817   0.05121   0.04489  -0.0336   0.0354   1.0000
  14.500   1.3801   0.05424   0.04801  -0.0334   0.0338   1.0000
  14.750   1.3820   0.05702   0.05096  -0.0334   0.0321   1.0000
  15.000   1.3821   0.06010   0.05419  -0.0336   0.0304   1.0000
  15.250   1.3798   0.06361   0.05781  -0.0341   0.0290   1.0000
  15.500   1.3740   0.06770   0.06201  -0.0349   0.0279   1.0000
  15.750   1.3706   0.07166   0.06613  -0.0359   0.0267   1.0000
  16.000   1.3671   0.07578   0.07043  -0.0370   0.0255   1.0000
  16.250   1.3619   0.08029   0.07509  -0.0386   0.0245   1.0000
  16.500   1.3550   0.08521   0.08016  -0.0405   0.0236   1.0000
  16.750   1.3462   0.09062   0.08569  -0.0428   0.0229   1.0000
  17.000   1.3352   0.09654   0.09172  -0.0455   0.0222   1.0000
  17.250   1.3273   0.10210   0.09746  -0.0480   0.0215   1.0000
  17.500   1.3183   0.10797   0.10351  -0.0510   0.0208   1.0000
  17.750   1.3087   0.11412   0.10982  -0.0542   0.0201   1.0000
  18.000   1.2983   0.12052   0.11637  -0.0577   0.0195   1.0000
  18.250   1.2877   0.12708   0.12307  -0.0614   0.0190   1.0000
  18.500   1.2768   0.13381   0.12992  -0.0654   0.0185   1.0000
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