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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.56 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh106-il-1000000.txt
Download as CSV file: xf-mh106-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 106  13.07%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7052   0.13312   0.13147   0.0199   1.0000   0.0053
 -14.500  -0.7541   0.11366   0.11188   0.0107   1.0000   0.0046
 -14.250  -0.7862   0.10058   0.09867   0.0032   1.0000   0.0045
 -14.000  -0.8098   0.09062   0.08860  -0.0029   1.0000   0.0045
 -13.750  -0.8294   0.08217   0.08004  -0.0083   1.0000   0.0045
 -13.500  -0.8603   0.07199   0.06969  -0.0150   1.0000   0.0044
 -13.250  -0.8713   0.06608   0.06368  -0.0190   1.0000   0.0044
 -13.000  -0.8986   0.05777   0.05517  -0.0245   1.0000   0.0043
 -12.750  -0.9101   0.05269   0.04995  -0.0276   1.0000   0.0043
 -12.500  -0.9457   0.04495   0.04191  -0.0309   1.0000   0.0041
 -12.250  -0.9619   0.04063   0.03739  -0.0315   1.0000   0.0040
 -12.000  -1.0035   0.03410   0.03036  -0.0296   1.0000   0.0037
 -11.750  -1.0151   0.03123   0.02728  -0.0270   1.0000   0.0037
 -11.500  -1.0168   0.02948   0.02538  -0.0243   1.0000   0.0037
 -11.250  -1.0170   0.02791   0.02369  -0.0213   1.0000   0.0037
 -11.000  -1.0165   0.02643   0.02207  -0.0179   1.0000   0.0038
 -10.750  -1.0126   0.02501   0.02050  -0.0148   1.0000   0.0038
 -10.500  -1.0036   0.02361   0.01897  -0.0124   1.0000   0.0038
 -10.250  -0.9909   0.02249   0.01775  -0.0104   1.0000   0.0039
 -10.000  -0.9770   0.02139   0.01655  -0.0085   1.0000   0.0040
  -9.750  -0.9619   0.02035   0.01541  -0.0067   1.0000   0.0040
  -9.500  -0.9452   0.01944   0.01441  -0.0051   1.0000   0.0042
  -9.250  -0.9279   0.01855   0.01343  -0.0036   1.0000   0.0043
  -9.000  -0.9097   0.01772   0.01253  -0.0021   1.0000   0.0044
  -8.750  -0.8901   0.01703   0.01177  -0.0008   1.0000   0.0047
  -8.500  -0.8694   0.01644   0.01112   0.0004   1.0000   0.0048
  -8.250  -0.8467   0.01604   0.01069   0.0013   1.0000   0.0050
  -8.000  -0.8292   0.01513   0.00970   0.0030   1.0000   0.0050
  -7.750  -0.8138   0.01404   0.00850   0.0052   1.0000   0.0053
  -7.500  -0.7939   0.01341   0.00781   0.0066   1.0000   0.0056
  -7.250  -0.7680   0.01290   0.00728   0.0068   0.9955   0.0058
  -7.000  -0.7267   0.01231   0.00664   0.0037   0.9620   0.0063
  -6.750  -0.6933   0.01194   0.00607   0.0026   0.8872   0.0066
  -6.500  -0.6719   0.01173   0.00565   0.0041   0.8375   0.0070
  -6.250  -0.6484   0.01152   0.00527   0.0051   0.8006   0.0073
  -6.000  -0.6255   0.01110   0.00472   0.0061   0.7711   0.0088
  -5.750  -0.6010   0.01082   0.00432   0.0069   0.7456   0.0110
  -5.500  -0.5777   0.01035   0.00384   0.0078   0.7223   0.0234
  -5.250  -0.5544   0.00987   0.00344   0.0086   0.7010   0.0512
  -5.000  -0.5318   0.00930   0.00304   0.0095   0.6802   0.0991
  -4.750  -0.5091   0.00876   0.00270   0.0103   0.6611   0.1573
  -4.500  -0.4848   0.00838   0.00246   0.0110   0.6432   0.2046
  -4.250  -0.4595   0.00811   0.00229   0.0114   0.6265   0.2409
  -4.000  -0.4335   0.00792   0.00214   0.0118   0.6105   0.2698
  -3.750  -0.4073   0.00775   0.00202   0.0121   0.5953   0.2982
  -3.500  -0.3804   0.00765   0.00191   0.0124   0.5803   0.3183
  -3.250  -0.3538   0.00752   0.00181   0.0127   0.5658   0.3422
  -3.000  -0.3269   0.00742   0.00172   0.0130   0.5518   0.3641
  -2.750  -0.2998   0.00734   0.00163   0.0132   0.5390   0.3809
  -2.250  -0.2454   0.00720   0.00148   0.0136   0.5152   0.4146
  -2.000  -0.2181   0.00713   0.00142   0.0138   0.5044   0.4323
  -1.750  -0.1907   0.00708   0.00136   0.0140   0.4939   0.4507
  -1.500  -0.1637   0.00701   0.00131   0.0142   0.4836   0.4703
  -1.250  -0.1364   0.00693   0.00127   0.0144   0.4744   0.4922
  -1.000  -0.1094   0.00687   0.00124   0.0146   0.4661   0.5152
  -0.750  -0.0823   0.00679   0.00121   0.0149   0.4581   0.5410
  -0.500  -0.0555   0.00672   0.00119   0.0151   0.4507   0.5685
  -0.250  -0.0287   0.00663   0.00117   0.0155   0.4435   0.5985
   0.000  -0.0022   0.00657   0.00117   0.0158   0.4372   0.6292
   0.250   0.0245   0.00648   0.00117   0.0161   0.4311   0.6599
   0.500   0.0506   0.00642   0.00119   0.0166   0.4252   0.6920
   0.750   0.0771   0.00635   0.00121   0.0170   0.4202   0.7229
   1.000   0.1034   0.00628   0.00123   0.0175   0.4148   0.7538
   1.250   0.1293   0.00625   0.00127   0.0180   0.4094   0.7853
   1.500   0.1558   0.00619   0.00131   0.0185   0.4050   0.8149
   1.750   0.1823   0.00615   0.00136   0.0189   0.4001   0.8442
   2.000   0.2090   0.00617   0.00142   0.0193   0.3949   0.8711
   2.250   0.2370   0.00615   0.00149   0.0195   0.3909   0.8963
   2.500   0.2671   0.00618   0.00157   0.0192   0.3863   0.9176
   2.750   0.2990   0.00628   0.00167   0.0185   0.3812   0.9346
   3.000   0.3332   0.00636   0.00177   0.0173   0.3767   0.9465
   3.250   0.3660   0.00645   0.00186   0.0163   0.3716   0.9563
   3.500   0.4007   0.00659   0.00197   0.0149   0.3660   0.9627
   3.750   0.4321   0.00668   0.00207   0.0143   0.3615   0.9696
   4.000   0.4698   0.00678   0.00217   0.0123   0.3557   0.9721
   4.250   0.5057   0.00692   0.00229   0.0105   0.3498   0.9754
   4.500   0.5389   0.00700   0.00239   0.0095   0.3444   0.9798
   4.750   0.5729   0.00713   0.00250   0.0082   0.3381   0.9829
   5.000   0.6104   0.00721   0.00259   0.0061   0.3314   0.9846
   5.250   0.6471   0.00732   0.00269   0.0042   0.3234   0.9867
   5.500   0.6831   0.00741   0.00279   0.0024   0.3153   0.9892
   5.750   0.7179   0.00755   0.00291   0.0009   0.3054   0.9921
   6.000   0.7537   0.00770   0.00303  -0.0009   0.2933   0.9943
   6.250   0.7920   0.00783   0.00314  -0.0032   0.2782   0.9963
   6.500   0.8294   0.00803   0.00328  -0.0055   0.2571   0.9985
   6.750   0.8637   0.00834   0.00349  -0.0071   0.2316   1.0000
   7.000   0.8856   0.00866   0.00372  -0.0062   0.2112   1.0000
   7.250   0.9071   0.00902   0.00400  -0.0052   0.1888   1.0000
   7.500   0.9281   0.00944   0.00432  -0.0041   0.1674   1.0000
   7.750   0.9496   0.00980   0.00462  -0.0031   0.1507   1.0000
   8.000   0.9707   0.01018   0.00494  -0.0020   0.1345   1.0000
   8.250   0.9913   0.01062   0.00530  -0.0009   0.1180   1.0000
   8.500   1.0117   0.01106   0.00568   0.0002   0.1037   1.0000
   8.750   1.0322   0.01147   0.00606   0.0014   0.0920   1.0000
   9.000   1.0525   0.01190   0.00645   0.0025   0.0811   1.0000
   9.250   1.0725   0.01235   0.00686   0.0037   0.0711   1.0000
   9.500   1.0918   0.01283   0.00730   0.0050   0.0615   1.0000
   9.750   1.1104   0.01336   0.00778   0.0064   0.0522   1.0000
  10.000   1.1295   0.01383   0.00825   0.0076   0.0455   1.0000
  10.250   1.1478   0.01435   0.00875   0.0090   0.0386   1.0000
  10.500   1.1648   0.01494   0.00932   0.0105   0.0325   1.0000
  10.750   1.1829   0.01544   0.00983   0.0119   0.0284   1.0000
  11.000   1.1986   0.01608   0.01046   0.0136   0.0238   1.0000
  11.250   1.2146   0.01668   0.01106   0.0152   0.0204   1.0000
  11.500   1.2291   0.01734   0.01173   0.0169   0.0173   1.0000
  11.750   1.2421   0.01805   0.01245   0.0188   0.0145   1.0000
  12.000   1.2542   0.01877   0.01322   0.0208   0.0123   1.0000
  12.250   1.2637   0.01958   0.01404   0.0230   0.0105   1.0000
  12.500   1.2664   0.02039   0.01490   0.0264   0.0091   1.0000
  12.750   1.2700   0.02130   0.01586   0.0292   0.0083   1.0000
  13.000   1.2718   0.02258   0.01719   0.0312   0.0074   1.0000
  13.250   1.2728   0.02430   0.01900   0.0324   0.0065   1.0000
  13.500   1.2778   0.02604   0.02082   0.0327   0.0061   1.0000
  13.750   1.2793   0.02836   0.02321   0.0325   0.0053   1.0000
  14.000   1.2803   0.03096   0.02590   0.0320   0.0050   1.0000
  14.250   1.2758   0.03432   0.02936   0.0310   0.0045   1.0000
  14.500   1.2767   0.03714   0.03228   0.0302   0.0044   1.0000
  14.750   1.2747   0.04031   0.03554   0.0292   0.0041   1.0000
  15.000   1.2728   0.04348   0.03880   0.0282   0.0038   1.0000
  15.250   1.2655   0.04733   0.04276   0.0270   0.0037   1.0000
  15.500   1.2601   0.05097   0.04647   0.0258   0.0035   1.0000
  15.750   1.2494   0.05530   0.05090   0.0243   0.0034   1.0000
  16.000   1.2351   0.06014   0.05585   0.0226   0.0032   1.0000
  16.250   1.2269   0.06437   0.06016   0.0211   0.0031   1.0000
  16.500   1.2017   0.07118   0.06711   0.0183   0.0030   1.0000
  16.750   1.1939   0.07563   0.07165   0.0166   0.0029   1.0000
  17.000   1.1809   0.08095   0.07708   0.0144   0.0029   1.0000
  17.250   1.1727   0.08560   0.08181   0.0126   0.0029   1.0000
  17.500   1.1597   0.09111   0.08743   0.0103   0.0027   1.0000
  17.750   1.1512   0.09599   0.09239   0.0083   0.0028   1.0000
  18.000   1.1334   0.10245   0.09896   0.0055   0.0027   1.0000
  18.250   1.1214   0.10809   0.10469   0.0031   0.0028   1.0000
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