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MH 106 13.07% (mh106-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 106 13.07% (mh106-il)
Reynolds number: 500,000
Max Cl/Cd: 79.7 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh106-il-500000-n5.txt
Download as CSV file: xf-mh106-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8293   0.12026   0.11755   0.0152   1.0000   0.0033
 -15.500  -0.8447   0.11159   0.10875   0.0104   1.0000   0.0032
 -15.250  -0.8684   0.10154   0.09855   0.0047   1.0000   0.0032
 -15.000  -0.8935   0.09186   0.08872  -0.0010   1.0000   0.0033
 -14.750  -0.8969   0.08684   0.08361  -0.0039   1.0000   0.0032
 -14.500  -0.9160   0.07917   0.07581  -0.0084   1.0000   0.0032
 -14.250  -0.9298   0.07261   0.06911  -0.0123   1.0000   0.0032
 -14.000  -0.9469   0.06589   0.06224  -0.0162   1.0000   0.0032
 -13.750  -0.9589   0.06014   0.05635  -0.0196   1.0000   0.0031
 -13.500  -0.9704   0.05467   0.05071  -0.0228   1.0000   0.0032
 -13.250  -0.9806   0.04983   0.04573  -0.0253   1.0000   0.0031
 -13.000  -0.9889   0.04554   0.04126  -0.0273   1.0000   0.0032
 -12.750  -0.9936   0.04210   0.03768  -0.0284   1.0000   0.0032
 -12.500  -1.0081   0.03794   0.03332  -0.0288   1.0000   0.0033
 -12.250  -1.0025   0.03624   0.03152  -0.0285   1.0000   0.0032
 -12.000  -1.0126   0.03324   0.02832  -0.0272   1.0000   0.0032
 -11.750  -1.0193   0.03087   0.02579  -0.0251   1.0000   0.0034
 -11.500  -1.0168   0.02939   0.02420  -0.0230   1.0000   0.0034
 -11.250  -1.0123   0.02815   0.02287  -0.0208   1.0000   0.0035
 -11.000  -1.0073   0.02697   0.02160  -0.0182   1.0000   0.0036
 -10.750  -1.0014   0.02586   0.02039  -0.0154   1.0000   0.0037
 -10.500  -0.9919   0.02480   0.01922  -0.0131   1.0000   0.0037
 -10.250  -0.9791   0.02381   0.01815  -0.0112   1.0000   0.0038
 -10.000  -0.9651   0.02284   0.01709  -0.0094   1.0000   0.0039
  -9.750  -0.9499   0.02191   0.01606  -0.0078   1.0000   0.0040
  -9.500  -0.9337   0.02102   0.01508  -0.0062   1.0000   0.0041
  -9.250  -0.9166   0.02017   0.01413  -0.0047   1.0000   0.0042
  -9.000  -0.8990   0.01934   0.01322  -0.0032   1.0000   0.0044
  -8.750  -0.8804   0.01858   0.01238  -0.0018   1.0000   0.0045
  -8.500  -0.8611   0.01787   0.01160  -0.0005   1.0000   0.0046
  -8.250  -0.8406   0.01726   0.01092   0.0006   1.0000   0.0048
  -8.000  -0.8202   0.01664   0.01024   0.0018   1.0000   0.0049
  -7.750  -0.7998   0.01587   0.00940   0.0029   0.9971   0.0053
  -7.500  -0.7559   0.01519   0.00864  -0.0008   0.9260   0.0059
  -7.250  -0.7296   0.01483   0.00808  -0.0005   0.8605   0.0064
  -7.000  -0.7088   0.01449   0.00752   0.0010   0.8184   0.0069
  -6.750  -0.6866   0.01416   0.00702   0.0022   0.7851   0.0073
  -6.500  -0.6645   0.01373   0.00643   0.0033   0.7561   0.0082
  -6.250  -0.6409   0.01341   0.00597   0.0041   0.7313   0.0094
  -6.000  -0.6169   0.01307   0.00552   0.0049   0.7094   0.0115
  -5.750  -0.5927   0.01274   0.00511   0.0056   0.6894   0.0157
  -5.500  -0.5684   0.01240   0.00473   0.0063   0.6699   0.0253
  -5.250  -0.5447   0.01197   0.00433   0.0070   0.6511   0.0441
  -5.000  -0.5220   0.01140   0.00389   0.0078   0.6341   0.0835
  -4.750  -0.4997   0.01078   0.00349   0.0086   0.6186   0.1421
  -4.500  -0.4764   0.01029   0.00320   0.0093   0.6041   0.1976
  -4.250  -0.4516   0.00997   0.00299   0.0098   0.5900   0.2385
  -4.000  -0.4257   0.00979   0.00281   0.0102   0.5758   0.2634
  -3.750  -0.3999   0.00959   0.00266   0.0106   0.5620   0.2925
  -3.500  -0.3737   0.00944   0.00252   0.0110   0.5492   0.3183
  -3.250  -0.3470   0.00933   0.00240   0.0113   0.5376   0.3343
  -2.750  -0.2931   0.00916   0.00216   0.0118   0.5160   0.3627
  -2.500  -0.2661   0.00908   0.00206   0.0120   0.5058   0.3772
  -2.250  -0.2391   0.00901   0.00197   0.0123   0.4957   0.3914
  -2.000  -0.2121   0.00894   0.00189   0.0125   0.4860   0.4067
  -1.500  -0.1580   0.00880   0.00175   0.0130   0.4697   0.4389
  -1.250  -0.1310   0.00873   0.00170   0.0132   0.4625   0.4563
  -1.000  -0.1040   0.00867   0.00165   0.0135   0.4551   0.4753
  -0.750  -0.0770   0.00860   0.00161   0.0137   0.4481   0.4957
  -0.500  -0.0503   0.00853   0.00158   0.0140   0.4413   0.5174
  -0.250  -0.0236   0.00846   0.00156   0.0143   0.4357   0.5418
   0.000   0.0031   0.00838   0.00156   0.0146   0.4299   0.5669
   0.250   0.0294   0.00833   0.00155   0.0150   0.4243   0.5942
   0.500   0.0559   0.00825   0.00156   0.0153   0.4189   0.6227
   0.750   0.0822   0.00818   0.00158   0.0158   0.4138   0.6519
   1.000   0.1082   0.00813   0.00160   0.0162   0.4091   0.6824
   1.250   0.1344   0.00806   0.00164   0.0167   0.4044   0.7127
   1.500   0.1605   0.00801   0.00169   0.0172   0.3996   0.7433
   1.750   0.1865   0.00798   0.00174   0.0177   0.3951   0.7748
   2.000   0.2130   0.00793   0.00181   0.0182   0.3907   0.8055
   2.250   0.2399   0.00791   0.00189   0.0186   0.3858   0.8353
   2.500   0.2679   0.00793   0.00198   0.0187   0.3810   0.8631
   2.750   0.2983   0.00797   0.00209   0.0184   0.3764   0.8880
   3.000   0.3311   0.00804   0.00220   0.0175   0.3713   0.9089
   3.250   0.3656   0.00816   0.00233   0.0162   0.3661   0.9247
   3.500   0.4021   0.00826   0.00246   0.0144   0.3608   0.9363
   3.750   0.4377   0.00837   0.00257   0.0128   0.3547   0.9454
   4.000   0.4695   0.00850   0.00270   0.0120   0.3490   0.9546
   4.250   0.5061   0.00861   0.00282   0.0102   0.3421   0.9596
   4.500   0.5368   0.00875   0.00295   0.0096   0.3357   0.9671
   4.750   0.5713   0.00886   0.00309   0.0082   0.3281   0.9716
   5.000   0.6055   0.00900   0.00323   0.0068   0.3204   0.9766
   5.250   0.6372   0.00914   0.00338   0.0060   0.3115   0.9823
   5.500   0.6749   0.00928   0.00353   0.0039   0.3008   0.9856
   5.750   0.7108   0.00944   0.00369   0.0020   0.2884   0.9896
   6.000   0.7443   0.00965   0.00386   0.0007   0.2723   0.9933
   6.250   0.7787   0.00990   0.00406  -0.0010   0.2518   0.9958
   6.500   0.8121   0.01019   0.00429  -0.0024   0.2302   0.9984
   6.750   0.8424   0.01057   0.00459  -0.0033   0.2085   1.0000
   7.000   0.8638   0.01094   0.00490  -0.0023   0.1887   1.0000
   7.250   0.8848   0.01135   0.00525  -0.0013   0.1704   1.0000
   7.500   0.9056   0.01179   0.00562  -0.0002   0.1533   1.0000
   7.750   0.9264   0.01221   0.00600   0.0009   0.1382   1.0000
   8.000   0.9467   0.01266   0.00641   0.0020   0.1228   1.0000
   8.250   0.9669   0.01313   0.00684   0.0031   0.1098   1.0000
   8.500   0.9869   0.01360   0.00728   0.0043   0.0986   1.0000
   8.750   1.0065   0.01408   0.00776   0.0055   0.0881   1.0000
   9.000   1.0260   0.01457   0.00823   0.0067   0.0781   1.0000
   9.250   1.0449   0.01509   0.00874   0.0080   0.0687   1.0000
   9.500   1.0631   0.01565   0.00928   0.0093   0.0602   1.0000
   9.750   1.0807   0.01623   0.00985   0.0107   0.0526   1.0000
  10.000   1.0985   0.01678   0.01042   0.0121   0.0464   1.0000
  10.250   1.1145   0.01744   0.01108   0.0136   0.0401   1.0000
  10.500   1.1306   0.01806   0.01172   0.0152   0.0350   1.0000
  10.750   1.1449   0.01876   0.01243   0.0169   0.0302   1.0000
  11.000   1.1579   0.01950   0.01318   0.0187   0.0258   1.0000
  11.250   1.1698   0.02026   0.01397   0.0207   0.0224   1.0000
  11.500   1.1792   0.02111   0.01484   0.0228   0.0192   1.0000
  11.750   1.1841   0.02195   0.01573   0.0257   0.0172   1.0000
  12.000   1.1865   0.02293   0.01676   0.0285   0.0152   1.0000
  12.250   1.1873   0.02427   0.01814   0.0307   0.0134   1.0000
  12.500   1.1909   0.02574   0.01971   0.0319   0.0121   1.0000
  12.750   1.1935   0.02758   0.02162   0.0324   0.0108   1.0000
  13.000   1.1955   0.02975   0.02388   0.0325   0.0100   1.0000
  13.250   1.1968   0.03219   0.02640   0.0322   0.0092   1.0000
  13.500   1.1981   0.03475   0.02906   0.0317   0.0084   1.0000
  13.750   1.1973   0.03765   0.03203   0.0309   0.0076   1.0000
  14.000   1.1955   0.04071   0.03519   0.0301   0.0073   1.0000
  14.250   1.1916   0.04405   0.03861   0.0292   0.0068   1.0000
  14.500   1.1875   0.04747   0.04212   0.0282   0.0065   1.0000
  14.750   1.1842   0.05081   0.04556   0.0272   0.0061   1.0000
  15.000   1.1785   0.05447   0.04933   0.0260   0.0058   1.0000
  15.250   1.1714   0.05836   0.05331   0.0247   0.0055   1.0000
  15.500   1.1646   0.06226   0.05731   0.0234   0.0053   1.0000
  15.750   1.1566   0.06652   0.06165   0.0218   0.0051   1.0000
  16.000   1.1477   0.07101   0.06623   0.0201   0.0049   1.0000
  16.250   1.1404   0.07538   0.07069   0.0184   0.0047   1.0000
  16.500   1.1300   0.08034   0.07575   0.0164   0.0045   1.0000
  16.750   1.1215   0.08507   0.08059   0.0144   0.0043   1.0000
  17.000   1.1112   0.09024   0.08587   0.0123   0.0041   1.0000
  17.250   1.1030   0.09514   0.09087   0.0102   0.0041   1.0000
  17.500   1.0928   0.10046   0.09630   0.0078   0.0038   1.0000
  17.750   1.0837   0.10573   0.10168   0.0055   0.0039   1.0000
  18.000   1.0711   0.11173   0.10778   0.0027   0.0037   1.0000
  18.250   1.0601   0.11755   0.11370   0.0000   0.0038   1.0000
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