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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 200,000
Max Cl/Cd: 64.97 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh104-il-200000-n5.txt
Download as CSV file: xf-mh104-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 104  15.28%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6743   0.10958   0.10580  -0.0048   1.0000   0.0099
 -14.250  -0.7341   0.09133   0.08721  -0.0163   1.0000   0.0095
 -14.000  -0.7646   0.08121   0.07682  -0.0229   1.0000   0.0093
 -13.750  -0.7863   0.07346   0.06885  -0.0279   1.0000   0.0092
 -13.500  -0.8010   0.06737   0.06259  -0.0318   1.0000   0.0093
 -13.250  -0.8156   0.06155   0.05656  -0.0353   1.0000   0.0092
 -13.000  -0.8266   0.05665   0.05145  -0.0380   1.0000   0.0091
 -12.750  -0.8341   0.05260   0.04727  -0.0399   1.0000   0.0092
 -12.500  -0.8406   0.04888   0.04337  -0.0413   1.0000   0.0092
 -12.250  -0.8455   0.04563   0.03997  -0.0420   1.0000   0.0093
 -12.000  -0.8483   0.04284   0.03704  -0.0422   1.0000   0.0094
 -11.750  -0.8490   0.04042   0.03447  -0.0419   1.0000   0.0094
 -11.500  -0.8488   0.03818   0.03209  -0.0411   1.0000   0.0095
 -11.250  -0.8469   0.03625   0.03003  -0.0399   1.0000   0.0097
 -11.000  -0.8436   0.03447   0.02811  -0.0384   1.0000   0.0098
 -10.750  -0.8391   0.03285   0.02637  -0.0366   1.0000   0.0100
 -10.500  -0.8326   0.03141   0.02482  -0.0346   1.0000   0.0101
 -10.250  -0.8261   0.03000   0.02330  -0.0324   1.0000   0.0104
 -10.000  -0.8183   0.02875   0.02196  -0.0301   1.0000   0.0106
  -9.750  -0.8091   0.02752   0.02062  -0.0279   1.0000   0.0110
  -9.500  -0.7973   0.02638   0.01938  -0.0260   1.0000   0.0112
  -9.250  -0.7844   0.02529   0.01819  -0.0242   1.0000   0.0115
  -9.000  -0.7554   0.02394   0.01673  -0.0258   0.9154   0.0120
  -8.750  -0.7347   0.02304   0.01567  -0.0251   0.8707   0.0127
  -8.500  -0.7181   0.02234   0.01479  -0.0234   0.8396   0.0136
  -8.250  -0.7012   0.02169   0.01393  -0.0216   0.8150   0.0147
  -8.000  -0.6851   0.02092   0.01306  -0.0198   0.7935   0.0157
  -7.750  -0.6664   0.02031   0.01229  -0.0183   0.7749   0.0173
  -7.500  -0.6479   0.01962   0.01143  -0.0168   0.7577   0.0189
  -7.250  -0.6287   0.01895   0.01063  -0.0154   0.7418   0.0212
  -7.000  -0.6083   0.01833   0.00990  -0.0141   0.7271   0.0245
  -6.750  -0.5875   0.01772   0.00920  -0.0129   0.7130   0.0305
  -6.500  -0.5666   0.01708   0.00851  -0.0118   0.6998   0.0401
  -6.250  -0.5458   0.01640   0.00786  -0.0106   0.6874   0.0589
  -6.000  -0.5260   0.01560   0.00722  -0.0095   0.6756   0.0983
  -5.750  -0.5058   0.01484   0.00672  -0.0084   0.6637   0.1552
  -5.500  -0.4833   0.01437   0.00638  -0.0076   0.6522   0.2013
  -5.250  -0.4594   0.01407   0.00609  -0.0069   0.6413   0.2323
  -5.000  -0.4348   0.01382   0.00584  -0.0062   0.6305   0.2584
  -4.750  -0.4102   0.01358   0.00562  -0.0056   0.6205   0.2853
  -4.500  -0.3855   0.01339   0.00541  -0.0050   0.6110   0.3115
  -4.250  -0.3601   0.01321   0.00522  -0.0044   0.6009   0.3326
  -4.000  -0.3344   0.01306   0.00502  -0.0040   0.5915   0.3493
  -3.750  -0.3085   0.01293   0.00482  -0.0035   0.5823   0.3648
  -3.500  -0.2824   0.01279   0.00464  -0.0031   0.5736   0.3799
  -3.250  -0.2564   0.01268   0.00447  -0.0026   0.5657   0.3956
  -3.000  -0.2301   0.01255   0.00433  -0.0022   0.5575   0.4115
  -2.750  -0.2040   0.01245   0.00418  -0.0018   0.5500   0.4282
  -2.500  -0.1777   0.01234   0.00406  -0.0014   0.5419   0.4457
  -2.250  -0.1517   0.01225   0.00394  -0.0009   0.5347   0.4641
  -2.000  -0.1255   0.01214   0.00384  -0.0005   0.5277   0.4833
  -1.750  -0.0996   0.01204   0.00376   0.0000   0.5212   0.5042
  -1.500  -0.0736   0.01195   0.00369   0.0004   0.5153   0.5265
  -1.250  -0.0478   0.01185   0.00364   0.0009   0.5088   0.5507
  -1.000  -0.0222   0.01178   0.00359   0.0015   0.5032   0.5770
  -0.750   0.0036   0.01168   0.00358   0.0020   0.4970   0.6055
  -0.500   0.0293   0.01161   0.00357   0.0026   0.4915   0.6356
   0.000   0.0811   0.01148   0.00361   0.0038   0.4817   0.7003
   0.250   0.1076   0.01144   0.00365   0.0043   0.4766   0.7338
   0.500   0.1349   0.01144   0.00370   0.0046   0.4722   0.7677
   0.750   0.1643   0.01145   0.00380   0.0046   0.4670   0.8001
   1.000   0.1960   0.01150   0.00391   0.0041   0.4622   0.8309
   1.250   0.2308   0.01161   0.00402   0.0029   0.4580   0.8576
   1.500   0.2674   0.01174   0.00415   0.0013   0.4535   0.8799
   1.750   0.3052   0.01188   0.00430  -0.0005   0.4484   0.8978
   2.000   0.3420   0.01204   0.00443  -0.0023   0.4441   0.9127
   2.250   0.3774   0.01221   0.00454  -0.0037   0.4403   0.9260
   2.500   0.4137   0.01236   0.00470  -0.0054   0.4354   0.9373
   2.750   0.4509   0.01251   0.00485  -0.0073   0.4308   0.9460
   3.000   0.4841   0.01269   0.00497  -0.0083   0.4269   0.9559
   3.250   0.5212   0.01285   0.00512  -0.0103   0.4225   0.9633
   3.500   0.5563   0.01299   0.00530  -0.0119   0.4178   0.9712
   3.750   0.5932   0.01313   0.00542  -0.0138   0.4134   0.9781
   4.000   0.6298   0.01329   0.00554  -0.0157   0.4095   0.9844
   4.250   0.6681   0.01340   0.00572  -0.0181   0.4044   0.9902
   4.500   0.7064   0.01351   0.00585  -0.0204   0.3996   0.9956
   4.750   0.7438   0.01364   0.00595  -0.0226   0.3954   1.0000
   5.000   0.7662   0.01378   0.00615  -0.0218   0.3911   1.0000
   5.250   0.7887   0.01392   0.00634  -0.0210   0.3865   1.0000
   5.500   0.8111   0.01407   0.00650  -0.0201   0.3822   1.0000
   5.750   0.8336   0.01425   0.00668  -0.0192   0.3781   1.0000
   6.000   0.8560   0.01442   0.00694  -0.0184   0.3728   1.0000
   6.250   0.8783   0.01458   0.00714  -0.0175   0.3678   1.0000
   6.500   0.9006   0.01478   0.00734  -0.0166   0.3631   1.0000
   6.750   0.9228   0.01496   0.00762  -0.0157   0.3570   1.0000
   7.000   0.9448   0.01515   0.00784  -0.0147   0.3514   1.0000
   7.250   0.9668   0.01536   0.00812  -0.0138   0.3455   1.0000
   7.500   0.9885   0.01557   0.00839  -0.0129   0.3390   1.0000
   7.750   1.0100   0.01579   0.00864  -0.0118   0.3327   1.0000
   8.000   1.0314   0.01602   0.00898  -0.0109   0.3252   1.0000
   8.250   1.0521   0.01627   0.00926  -0.0098   0.3182   1.0000
   8.500   1.0728   0.01653   0.00961  -0.0087   0.3096   1.0000
   8.750   1.0928   0.01682   0.00994  -0.0075   0.3013   1.0000
   9.000   1.1119   0.01713   0.01030  -0.0062   0.2917   1.0000
   9.250   1.1307   0.01747   0.01072  -0.0049   0.2814   1.0000
   9.500   1.1482   0.01786   0.01114  -0.0035   0.2706   1.0000
   9.750   1.1640   0.01832   0.01161  -0.0018   0.2591   1.0000
  10.000   1.1778   0.01885   0.01214   0.0001   0.2472   1.0000
  10.250   1.1905   0.01944   0.01275   0.0021   0.2347   1.0000
  10.500   1.2012   0.02009   0.01342   0.0043   0.2227   1.0000
  10.750   1.2092   0.02083   0.01417   0.0068   0.2109   1.0000
  11.000   1.2123   0.02165   0.01499   0.0099   0.2004   1.0000
  11.500   1.2122   0.02377   0.01713   0.0158   0.1802   1.0000
  11.750   1.2124   0.02518   0.01857   0.0178   0.1706   1.0000
  12.000   1.2106   0.02695   0.02035   0.0194   0.1614   1.0000
  12.250   1.2106   0.02882   0.02226   0.0204   0.1519   1.0000
  12.500   1.2097   0.03092   0.02440   0.0212   0.1436   1.0000
  12.750   1.2058   0.03342   0.02691   0.0216   0.1357   1.0000
  13.000   1.2047   0.03582   0.02936   0.0219   0.1276   1.0000
  13.250   1.1994   0.03869   0.03225   0.0220   0.1208   1.0000
  13.500   1.1967   0.04141   0.03503   0.0219   0.1134   1.0000
  13.750   1.1905   0.04455   0.03820   0.0217   0.1073   1.0000
  14.000   1.1866   0.04753   0.04123   0.0214   0.1008   1.0000
  14.250   1.1793   0.05093   0.04466   0.0210   0.0956   1.0000
  14.500   1.1755   0.05404   0.04783   0.0205   0.0893   1.0000
  14.750   1.1677   0.05773   0.05154   0.0197   0.0843   1.0000
  15.000   1.1648   0.06095   0.05485   0.0191   0.0790   1.0000
  15.250   1.1587   0.06466   0.05860   0.0181   0.0743   1.0000
  15.500   1.1538   0.06827   0.06227   0.0172   0.0699   1.0000
  15.750   1.1489   0.07199   0.06605   0.0161   0.0652   1.0000
  16.000   1.1408   0.07620   0.07029   0.0148   0.0613   1.0000
  16.250   1.1373   0.07986   0.07402   0.0137   0.0567   1.0000
  16.500   1.1308   0.08403   0.07825   0.0123   0.0533   1.0000
  16.750   1.1242   0.08827   0.08254   0.0109   0.0499   1.0000
  17.000   1.1187   0.09243   0.08676   0.0094   0.0462   1.0000
  17.250   1.1110   0.09700   0.09138   0.0077   0.0436   1.0000
  17.500   1.1050   0.10140   0.09586   0.0061   0.0409   1.0000
  17.750   1.0993   0.10577   0.10031   0.0043   0.0382   1.0000
  18.000   1.0918   0.11054   0.10513   0.0024   0.0360   1.0000
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