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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 200,000
Max Cl/Cd: 56.27 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh150-il-200000.txt
Download as CSV file: xf-mh150-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.6070   0.12383   0.11922  -0.0636   1.0001   0.0408
 -19.000  -0.6447   0.11323   0.10832  -0.0702   1.0001   0.0410
 -18.750  -0.6686   0.10533   0.10017  -0.0753   1.0001   0.0413
 -18.500  -0.6466   0.10535   0.10034  -0.0750   1.0001   0.0424
 -18.250  -0.6413   0.10247   0.09747  -0.0768   1.0001   0.0432
 -18.000  -0.6433   0.09840   0.09332  -0.0793   1.0001   0.0441
 -17.750  -0.6490   0.09376   0.08855  -0.0823   1.0001   0.0450
 -17.500  -0.6558   0.08900   0.08362  -0.0853   1.0001   0.0459
 -17.250  -0.6393   0.08812   0.08286  -0.0856   1.0001   0.0472
 -17.000  -0.6295   0.08609   0.08088  -0.0869   1.0001   0.0486
 -16.750  -0.6281   0.08280   0.07752  -0.0891   1.0001   0.0500
 -16.500  -0.6271   0.07968   0.07434  -0.0910   1.0001   0.0515
 -16.250  -0.6170   0.07866   0.07346  -0.0913   1.0001   0.0533
 -16.000  -0.6218   0.07684   0.07165  -0.0916   0.9982   0.0549
 -15.750  -0.6071   0.07336   0.06812  -0.0961   0.9925   0.0577
 -15.500  -0.5924   0.07007   0.06483  -0.1004   0.9852   0.0610
 -15.250  -0.5778   0.06678   0.06156  -0.1048   0.9784   0.0647
 -15.000  -0.5722   0.06296   0.05762  -0.1087   0.9669   0.0688
 -14.750  -0.5640   0.06048   0.05523  -0.1107   0.9541   0.0728
 -14.500  -0.5642   0.05766   0.05238  -0.1119   0.9406   0.0770
 -14.250  -0.5676   0.05491   0.04959  -0.1124   0.9271   0.0813
 -14.000  -0.5695   0.05234   0.04702  -0.1130   0.9143   0.0858
 -13.750  -0.5750   0.04940   0.04396  -0.1136   0.9036   0.0910
 -13.500  -0.5758   0.04690   0.04151  -0.1145   0.8920   0.0960
 -13.250  -0.5785   0.04432   0.03886  -0.1152   0.8825   0.1016
 -13.000  -0.5791   0.04159   0.03605  -0.1168   0.8718   0.1079
 -12.750  -0.5801   0.03932   0.03377  -0.1173   0.8634   0.1137
 -12.500  -0.5774   0.03695   0.03136  -0.1189   0.8532   0.1205
 -12.250  -0.5755   0.03476   0.02909  -0.1200   0.8446   0.1273
 -12.000  -0.5705   0.03282   0.02715  -0.1212   0.8362   0.1341
 -11.750  -0.5641   0.03087   0.02510  -0.1226   0.8271   0.1419
 -11.500  -0.5566   0.02920   0.02339  -0.1235   0.8199   0.1495
 -11.250  -0.5464   0.02770   0.02190  -0.1248   0.8111   0.1575
 -11.000  -0.5390   0.02636   0.02043  -0.1255   0.8029   0.1659
 -10.750  -0.5245   0.02524   0.01932  -0.1266   0.7967   0.1745
 -10.500  -0.5063   0.02420   0.01827  -0.1286   0.7883   0.1841
 -10.250  -0.4835   0.02316   0.01709  -0.1313   0.7809   0.1949
 -10.000  -0.4572   0.02248   0.01640  -0.1333   0.7752   0.2052
  -9.750  -0.4296   0.02194   0.01586  -0.1355   0.7678   0.2154
  -9.500  -0.3999   0.02143   0.01519  -0.1379   0.7606   0.2267
  -9.250  -0.3702   0.02122   0.01498  -0.1389   0.7549   0.2364
  -9.000  -0.3403   0.02097   0.01465  -0.1404   0.7486   0.2463
  -8.750  -0.3102   0.02087   0.01451  -0.1416   0.7413   0.2556
  -8.500  -0.2798   0.02062   0.01419  -0.1426   0.7354   0.2642
  -8.250  -0.2485   0.02059   0.01405  -0.1435   0.7302   0.2727
  -8.000  -0.2187   0.02036   0.01377  -0.1446   0.7229   0.2809
  -7.750  -0.1893   0.02036   0.01378  -0.1449   0.7164   0.2879
  -7.500  -0.1552   0.02017   0.01331  -0.1468   0.7110   0.2968
  -7.250  -0.1275   0.02010   0.01334  -0.1466   0.7054   0.3029
  -7.000  -0.0979   0.02009   0.01332  -0.1472   0.6984   0.3100
  -6.750  -0.0648   0.01983   0.01285  -0.1487   0.6924   0.3177
  -6.500  -0.0357   0.01978   0.01280  -0.1486   0.6874   0.3233
  -6.250  -0.0063   0.01978   0.01280  -0.1491   0.6809   0.3297
  -6.000   0.0272   0.01960   0.01242  -0.1508   0.6746   0.3368
  -5.750   0.0555   0.01942   0.01228  -0.1507   0.6693   0.3420
  -5.500   0.0859   0.01944   0.01224  -0.1511   0.6641   0.3477
  -5.250   0.1172   0.01934   0.01205  -0.1522   0.6573   0.3543
  -5.000   0.1481   0.01910   0.01174  -0.1530   0.6515   0.3598
  -4.750   0.1778   0.01905   0.01167  -0.1532   0.6466   0.3648
  -4.500   0.2082   0.01906   0.01163  -0.1538   0.6411   0.3706
  -4.250   0.2408   0.01897   0.01141  -0.1552   0.6346   0.3768
  -4.000   0.2705   0.01876   0.01118  -0.1556   0.6291   0.3818
  -3.750   0.3009   0.01875   0.01112  -0.1559   0.6245   0.3869
  -3.500   0.3310   0.01878   0.01113  -0.1566   0.6189   0.3927
  -3.250   0.3640   0.01873   0.01094  -0.1580   0.6128   0.3989
  -3.000   0.3931   0.01855   0.01079  -0.1582   0.6076   0.4039
  -2.750   0.4240   0.01858   0.01074  -0.1587   0.6031   0.4092
  -2.500   0.4539   0.01862   0.01078  -0.1594   0.5976   0.4153
  -2.250   0.4863   0.01858   0.01065  -0.1606   0.5920   0.4214
  -2.000   0.5155   0.01848   0.01057  -0.1609   0.5872   0.4263
  -1.750   0.5466   0.01854   0.01055  -0.1614   0.5828   0.4322
  -1.500   0.5768   0.01862   0.01062  -0.1622   0.5774   0.4390
  -1.250   0.6074   0.01859   0.01057  -0.1630   0.5719   0.4451
  -1.000   0.6367   0.01860   0.01060  -0.1633   0.5673   0.4506
  -0.750   0.6682   0.01868   0.01059  -0.1640   0.5633   0.4576
  -0.500   0.7003   0.01883   0.01066  -0.1652   0.5587   0.4655
  -0.250   0.7269   0.01890   0.01086  -0.1651   0.5535   0.4715
   0.000   0.7564   0.01897   0.01093  -0.1655   0.5486   0.4786
   0.250   0.7898   0.01903   0.01085  -0.1667   0.5444   0.4871
   0.500   0.8193   0.01920   0.01101  -0.1671   0.5404   0.4939
   0.750   0.8456   0.01941   0.01133  -0.1671   0.5357   0.5018
   1.000   0.8763   0.01956   0.01145  -0.1679   0.5310   0.5111
   1.250   0.9041   0.01966   0.01161  -0.1679   0.5270   0.5181
   1.500   0.9351   0.01982   0.01169  -0.1686   0.5232   0.5268
   1.750   0.9652   0.02007   0.01191  -0.1693   0.5190   0.5357
   2.000   0.9895   0.02031   0.01229  -0.1688   0.5144   0.5431
   2.250   1.0182   0.02052   0.01251  -0.1692   0.5100   0.5530
   2.500   1.0473   0.02068   0.01265  -0.1696   0.5063   0.5613
   2.750   1.0765   0.02091   0.01286  -0.1698   0.5030   0.5696
   3.000   1.1068   0.02129   0.01319  -0.1707   0.4993   0.5798
   3.250   1.1286   0.02158   0.01365  -0.1698   0.4950   0.5865
   3.500   1.1541   0.02185   0.01397  -0.1696   0.4908   0.5952
   3.750   1.1842   0.02204   0.01411  -0.1703   0.4871   0.6052
   4.000   1.2114   0.02228   0.01435  -0.1701   0.4839   0.6123
   4.250   1.2401   0.02272   0.01476  -0.1705   0.4806   0.6216
   4.500   1.2622   0.02313   0.01530  -0.1700   0.4768   0.6299
   4.750   1.2834   0.02352   0.01579  -0.1690   0.4730   0.6369
   5.000   1.3103   0.02381   0.01609  -0.1692   0.4694   0.6467
   5.250   1.3382   0.02402   0.01628  -0.1693   0.4662   0.6543
   5.500   1.3664   0.02435   0.01656  -0.1693   0.4631   0.6618
   5.750   1.3900   0.02492   0.01719  -0.1693   0.4597   0.6718
   6.000   1.4065   0.02543   0.01786  -0.1677   0.4562   0.6780
   6.250   1.4261   0.02589   0.01840  -0.1666   0.4528   0.6852
   6.500   1.4545   0.02623   0.01871  -0.1673   0.4494   0.6957
   6.750   1.4786   0.02645   0.01895  -0.1665   0.4466   0.7013
   7.000   1.5085   0.02681   0.01924  -0.1669   0.4437   0.7092
   7.250   1.5267   0.02753   0.02007  -0.1662   0.4405   0.7185
   7.500   1.5359   0.02822   0.02094  -0.1636   0.4372   0.7238
   7.750   1.5514   0.02879   0.02160  -0.1621   0.4339   0.7313
   8.000   1.5756   0.02918   0.02199  -0.1621   0.4307   0.7403
   8.250   1.5990   0.02941   0.02223  -0.1613   0.4279   0.7463
   8.500   1.6319   0.02970   0.02245  -0.1623   0.4254   0.7548
   8.750   1.6476   0.03053   0.02337  -0.1611   0.4225   0.7622
   9.000   1.6401   0.03157   0.02462  -0.1565   0.4192   0.7681
   9.250   1.6461   0.03256   0.02573  -0.1543   0.4157   0.7765
   9.500   1.6606   0.03318   0.02640  -0.1529   0.4126   0.7833
   9.750   1.6830   0.03349   0.02673  -0.1523   0.4101   0.7906
  10.000   1.7198   0.03356   0.02672  -0.1538   0.4076   0.7996
  10.250   1.7442   0.03408   0.02724  -0.1535   0.4048   0.8060
  10.500   1.7174   0.03639   0.02983  -0.1480   0.4013   0.8133
  10.750   1.7043   0.03851   0.03214  -0.1445   0.3975   0.8199
  11.000   1.7094   0.03970   0.03342  -0.1426   0.3944   0.8270
  11.250   1.7367   0.03987   0.03357  -0.1429   0.3917   0.8356
  11.500   1.7730   0.03939   0.03303  -0.1435   0.3894   0.8435
  11.750   1.8092   0.03950   0.03308  -0.1447   0.3868   0.8524
  12.000   1.7278   0.04585   0.03989  -0.1367   0.3817   0.8563
  12.250   1.6936   0.05037   0.04461  -0.1334   0.3768   0.8622
  12.500   1.7193   0.05034   0.04458  -0.1334   0.3742   0.8705
  12.750   1.7632   0.04900   0.04316  -0.1342   0.3722   0.8808
  13.000   1.8153   0.04714   0.04121  -0.1355   0.3703   0.8912
  13.250   1.5592   0.07354   0.06837  -0.1265   0.3547   0.8815
  13.500   1.6148   0.06971   0.06450  -0.1264   0.3545   0.8934
  13.750   1.6742   0.06577   0.06049  -0.1267   0.3541   0.9060
  14.000   1.7340   0.06207   0.05670  -0.1273   0.3534   0.9198
  14.250   1.7939   0.05867   0.05322  -0.1280   0.3522   0.9358
  14.500   1.5557   0.08766   0.08276  -0.1243   0.3345   0.9199
  14.750   1.6076   0.08364   0.07873  -0.1238   0.3345   0.9371
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