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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 50,000
Max Cl/Cd: 7.79 at α=1.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh150-il-50000-n5.txt
Download as CSV file: xf-mh150-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 150  23.89%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.1825   0.12930   0.12208  -0.0808   0.9625   0.1161
 -13.750  -0.1713   0.12564   0.11839  -0.0840   0.9537   0.1216
 -13.500  -0.1739   0.11960   0.11229  -0.0887   0.9468   0.1288
 -13.250  -0.1484   0.11860   0.11125  -0.0903   0.9373   0.1337
 -13.000  -0.1589   0.11207   0.10467  -0.0948   0.9299   0.1414
 -12.750  -0.1288   0.11201   0.10454  -0.0955   0.9205   0.1462
 -12.500  -0.1416   0.10593   0.09841  -0.0992   0.9121   0.1540
 -12.250  -0.1121   0.10586   0.09826  -0.0996   0.9035   0.1589
 -12.000  -0.1308   0.09983   0.09219  -0.1028   0.8941   0.1669
 -11.750  -0.1000   0.10018   0.09246  -0.1024   0.8859   0.1714
 -11.500  -0.1251   0.09376   0.08601  -0.1058   0.8767   0.1803
 -11.250  -0.0932   0.09473   0.08690  -0.1045   0.8674   0.1840
 -11.000  -0.0874   0.09237   0.08446  -0.1052   0.8591   0.1905
 -10.750  -0.0906   0.08921   0.08126  -0.1064   0.8498   0.1972
 -10.500  -0.0728   0.08826   0.08022  -0.1061   0.8425   0.2026
 -10.250  -0.0914   0.08356   0.07549  -0.1083   0.8335   0.2112
 -10.000  -0.0667   0.08381   0.07566  -0.1071   0.8248   0.2154
  -9.750  -0.0925   0.07790   0.06969  -0.1100   0.8189   0.2261
  -9.500  -0.0660   0.07897   0.07071  -0.1082   0.8086   0.2293
  -9.250  -0.0515   0.07803   0.06969  -0.1077   0.8012   0.2352
  -9.000  -0.0676   0.07376   0.06536  -0.1094   0.7947   0.2444
  -8.750  -0.0463   0.07422   0.06579  -0.1080   0.7850   0.2486
  -8.500  -0.0783   0.06872   0.06025  -0.1103   0.7779   0.2604
  -8.250  -0.0458   0.06962   0.06105  -0.1087   0.7716   0.2637
  -7.750  -0.0615   0.06494   0.05630  -0.1085   0.7554   0.2800
  -7.250  -0.0943   0.06087   0.05220  -0.1062   0.7381   0.2962
  -7.000  -0.0625   0.06129   0.05253  -0.1050   0.7331   0.3002
  -6.500  -0.1009   0.05665   0.04783  -0.1041   0.7157   0.3181
  -6.250  -0.0626   0.05760   0.04869  -0.1024   0.7114   0.3215
  -6.000  -0.1032   0.05339   0.04440  -0.1045   0.7015   0.3349
  -5.750  -0.0899   0.05345   0.04444  -0.1027   0.6942   0.3396
  -5.500  -0.0582   0.05385   0.04475  -0.1014   0.6900   0.3441
  -5.250  -0.0722   0.05017   0.04087  -0.1055   0.6819   0.3579
  -5.000  -0.0624   0.05112   0.04186  -0.1020   0.6737   0.3609
  -4.750  -0.0354   0.05113   0.04179  -0.1011   0.6694   0.3661
  -4.500  -0.0064   0.04821   0.03857  -0.1069   0.6661   0.3792
  -4.250  -0.0192   0.04954   0.04000  -0.1024   0.6542   0.3818
  -4.000   0.0046   0.04957   0.03997  -0.1014   0.6494   0.3868
  -3.750   0.0444   0.04723   0.03732  -0.1077   0.6462   0.3999
  -3.500   0.0389   0.04851   0.03869  -0.1040   0.6363   0.4025
  -3.250   0.0544   0.04888   0.03904  -0.1023   0.6300   0.4068
  -3.000   0.0903   0.04797   0.03795  -0.1048   0.6265   0.4156
  -2.750   0.1312   0.04684   0.03664  -0.1078   0.6241   0.4237
  -2.500   0.1095   0.04884   0.03876  -0.1038   0.6111   0.4263
  -2.250   0.1371   0.04870   0.03855  -0.1039   0.6071   0.4324
  -2.000   0.1880   0.04728   0.03686  -0.1097   0.6045   0.4436
  -1.750   0.1728   0.04948   0.03917  -0.1065   0.5930   0.4460
  -1.500   0.1922   0.04988   0.03956  -0.1055   0.5879   0.4506
  -1.250   0.2279   0.04941   0.03897  -0.1071   0.5849   0.4585
  -1.000   0.2720   0.04853   0.03792  -0.1102   0.5829   0.4674
  -0.750   0.2517   0.05200   0.04153  -0.1081   0.5693   0.4700
  -0.500   0.2788   0.05202   0.04150  -0.1080   0.5657   0.4759
  -0.250   0.3267   0.05115   0.04041  -0.1125   0.5634   0.4876
   0.000   0.3475   0.05145   0.04073  -0.1108   0.5603   0.4919
   0.500   0.3619   0.05541   0.04475  -0.1108   0.5442   0.5034
   0.750   0.4015   0.05484   0.04407  -0.1127   0.5422   0.5127
   1.250   0.4006   0.06027   0.04963  -0.1114   0.5255   0.5221
   1.500   0.4412   0.06006   0.04929  -0.1142   0.5232   0.5339
   1.750   0.4668   0.05990   0.04914  -0.1127   0.5213   0.5397
   2.250   0.4674   0.06603   0.05535  -0.1133   0.5047   0.5524
   2.500   0.4970   0.06616   0.05545  -0.1135   0.5026   0.5608
   3.000   0.4919   0.07256   0.06199  -0.1129   0.4872   0.5725
   3.250   0.5214   0.07305   0.06243  -0.1139   0.4844   0.5826
   3.500   0.5458   0.07328   0.06267  -0.1129   0.4825   0.5904
   4.000   0.5410   0.08074   0.07024  -0.1144   0.4678   0.6048
   4.250   0.5598   0.08140   0.07092  -0.1131   0.4650   0.6120
   4.500   0.5905   0.08175   0.07123  -0.1137   0.4630   0.6235
   5.000   0.5739   0.08974   0.07940  -0.1133   0.4494   0.6342
   5.250   0.5961   0.09075   0.08040  -0.1134   0.4464   0.6446
   5.500   0.6218   0.09130   0.08095  -0.1133   0.4442   0.6547
   6.000   0.6092   0.09918   0.08899  -0.1135   0.4319   0.6673
   6.250   0.6270   0.10066   0.09049  -0.1136   0.4285   0.6770
   6.500   0.6479   0.10142   0.09126  -0.1129   0.4261   0.6868
   6.750   0.6763   0.10196   0.09177  -0.1132   0.4243   0.6985
   7.000   0.6441   0.10860   0.09858  -0.1136   0.4152   0.7009
   7.250   0.6551   0.11060   0.10061  -0.1134   0.4115   0.7100
   7.500   0.6758   0.11186   0.10188  -0.1136   0.4086   0.7208
   7.750   0.6980   0.11248   0.10250  -0.1129   0.4065   0.7312
   8.000   0.6842   0.11769   0.10781  -0.1142   0.3995   0.7375
   8.250   0.6868   0.12038   0.11058  -0.1139   0.3951   0.7447
   8.500   0.7023   0.12203   0.11226  -0.1140   0.3917   0.7552
   8.750   0.7230   0.12296   0.11320  -0.1136   0.3892   0.7656
   9.000   0.7494   0.12365   0.11387  -0.1137   0.3873   0.7781
   9.250   0.7228   0.12981   0.12018  -0.1149   0.3793   0.7816
   9.500   0.7317   0.13183   0.12225  -0.1147   0.3754   0.7907
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