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MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 95 15.86% (mh95-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.28 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh95-il-1000000-n5.txt
Download as CSV file: xf-mh95-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 95  15.86%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8558   0.12243   0.11958  -0.0476   1.0000   0.0089
 -19.500  -0.8831   0.11354   0.11055  -0.0521   1.0000   0.0089
 -19.250  -0.9062   0.10566   0.10255  -0.0560   1.0000   0.0089
 -19.000  -0.9304   0.09785   0.09460  -0.0599   1.0000   0.0089
 -18.750  -0.9483   0.09130   0.08794  -0.0631   1.0000   0.0089
 -18.500  -0.9665   0.08486   0.08137  -0.0662   1.0000   0.0089
 -18.250  -0.9832   0.07885   0.07525  -0.0689   1.0000   0.0089
 -18.000  -0.9951   0.07373   0.07003  -0.0712   1.0000   0.0090
 -17.750  -1.0097   0.06841   0.06459  -0.0733   1.0000   0.0089
 -17.500  -1.0193   0.06396   0.06003  -0.0750   1.0000   0.0089
 -17.250  -1.0278   0.05989   0.05585  -0.0763   1.0000   0.0089
 -17.000  -1.0369   0.05591   0.05177  -0.0773   1.0000   0.0090
 -16.750  -1.0419   0.05264   0.04842  -0.0778   1.0000   0.0090
 -16.500  -1.0492   0.04934   0.04502  -0.0781   1.0000   0.0091
 -16.250  -1.0547   0.04645   0.04205  -0.0779   1.0000   0.0091
 -16.000  -1.0574   0.04404   0.03955  -0.0773   1.0000   0.0091
 -15.750  -1.0614   0.04169   0.03712  -0.0764   1.0000   0.0092
 -15.500  -1.0629   0.03975   0.03512  -0.0753   1.0000   0.0092
 -15.250  -1.0666   0.03777   0.03306  -0.0737   1.0000   0.0092
 -15.000  -1.0603   0.03583   0.03104  -0.0738   0.9996   0.0093
 -14.750  -1.0502   0.03400   0.02913  -0.0743   0.9988   0.0093
 -14.500  -1.0380   0.03236   0.02741  -0.0747   0.9979   0.0095
 -14.250  -1.0253   0.03076   0.02573  -0.0752   0.9968   0.0095
 -14.000  -1.0118   0.02926   0.02417  -0.0756   0.9955   0.0096
 -13.750  -0.9960   0.02803   0.02287  -0.0759   0.9943   0.0097
 -13.500  -0.9790   0.02687   0.02165  -0.0763   0.9933   0.0098
 -13.250  -0.9668   0.02562   0.02033  -0.0758   0.9914   0.0098
 -13.000  -0.9503   0.02464   0.01930  -0.0756   0.9896   0.0098
 -12.750  -0.9329   0.02366   0.01826  -0.0756   0.9879   0.0099
 -12.500  -0.9142   0.02270   0.01725  -0.0757   0.9863   0.0100
 -12.250  -0.8929   0.02191   0.01640  -0.0760   0.9850   0.0101
 -12.000  -0.8708   0.02113   0.01558  -0.0765   0.9839   0.0101
 -11.750  -0.8514   0.02002   0.01442  -0.0768   0.9828   0.0103
 -11.500  -0.8283   0.01922   0.01358  -0.0774   0.9819   0.0105
 -11.250  -0.8141   0.01859   0.01292  -0.0758   0.9780   0.0107
 -11.000  -0.7930   0.01795   0.01226  -0.0756   0.9757   0.0108
 -10.750  -0.7701   0.01728   0.01156  -0.0758   0.9739   0.0110
 -10.500  -0.7439   0.01675   0.01101  -0.0763   0.9725   0.0112
 -10.250  -0.7166   0.01620   0.01043  -0.0771   0.9713   0.0114
 -10.000  -0.6881   0.01563   0.00984  -0.0782   0.9702   0.0115
  -9.750  -0.6582   0.01512   0.00930  -0.0793   0.9692   0.0118
  -9.500  -0.6423   0.01472   0.00888  -0.0775   0.9638   0.0120
  -9.250  -0.6181   0.01426   0.00839  -0.0774   0.9605   0.0122
  -9.000  -0.5916   0.01382   0.00793  -0.0777   0.9579   0.0123
  -8.750  -0.5630   0.01340   0.00748  -0.0784   0.9557   0.0126
  -8.500  -0.5452   0.01310   0.00716  -0.0767   0.9506   0.0127
  -8.250  -0.5277   0.01269   0.00672  -0.0750   0.9453   0.0130
  -8.000  -0.5037   0.01231   0.00633  -0.0746   0.9417   0.0134
  -7.750  -0.4838   0.01202   0.00603  -0.0732   0.9370   0.0137
  -7.500  -0.4665   0.01178   0.00577  -0.0712   0.9310   0.0141
  -7.250  -0.4422   0.01150   0.00547  -0.0707   0.9266   0.0145
  -7.000  -0.4184   0.01125   0.00520  -0.0700   0.9221   0.0149
  -6.750  -0.3982   0.01104   0.00498  -0.0686   0.9157   0.0153
  -6.500  -0.3743   0.01079   0.00471  -0.0679   0.9101   0.0160
  -6.250  -0.3513   0.01055   0.00447  -0.0670   0.9043   0.0169
  -6.000  -0.3289   0.01035   0.00425  -0.0660   0.8971   0.0181
  -5.750  -0.3039   0.01013   0.00402  -0.0655   0.8906   0.0197
  -5.500  -0.2816   0.00994   0.00383  -0.0644   0.8825   0.0218
  -5.250  -0.2575   0.00971   0.00360  -0.0637   0.8740   0.0269
  -5.000  -0.2353   0.00950   0.00341  -0.0626   0.8642   0.0351
  -4.750  -0.2124   0.00927   0.00321  -0.0616   0.8537   0.0477
  -4.500  -0.1903   0.00903   0.00301  -0.0605   0.8416   0.0647
  -4.250  -0.1690   0.00876   0.00282  -0.0593   0.8287   0.0894
  -4.000  -0.1485   0.00847   0.00262  -0.0579   0.8151   0.1239
  -3.750  -0.1288   0.00816   0.00243  -0.0564   0.7997   0.1667
  -3.500  -0.1082   0.00793   0.00228  -0.0550   0.7838   0.2035
  -3.250  -0.0882   0.00767   0.00213  -0.0535   0.7665   0.2467
  -3.000  -0.0689   0.00740   0.00200  -0.0519   0.7482   0.2998
  -2.750  -0.0496   0.00712   0.00187  -0.0503   0.7293   0.3568
  -2.500  -0.0316   0.00678   0.00173  -0.0485   0.7098   0.4297
  -2.250  -0.0129   0.00647   0.00162  -0.0468   0.6902   0.5005
  -2.000   0.0080   0.00631   0.00155  -0.0454   0.6703   0.5492
  -1.750   0.0311   0.00626   0.00152  -0.0444   0.6516   0.5779
  -1.500   0.0548   0.00625   0.00150  -0.0435   0.6333   0.6023
  -1.250   0.0790   0.00627   0.00150  -0.0427   0.6148   0.6214
  -1.000   0.1035   0.00631   0.00150  -0.0419   0.5963   0.6369
  -0.750   0.1282   0.00637   0.00152  -0.0412   0.5774   0.6496
  -0.500   0.1531   0.00646   0.00153  -0.0405   0.5582   0.6616
  -0.250   0.1777   0.00654   0.00156  -0.0398   0.5388   0.6722
   0.000   0.2026   0.00663   0.00160  -0.0391   0.5196   0.6820
   0.250   0.2272   0.00674   0.00164  -0.0384   0.4988   0.6922
   0.500   0.2523   0.00685   0.00169  -0.0378   0.4795   0.7002
   0.750   0.2769   0.00697   0.00174  -0.0372   0.4584   0.7076
   1.000   0.3019   0.00711   0.00180  -0.0365   0.4378   0.7141
   1.250   0.3264   0.00725   0.00187  -0.0359   0.4167   0.7196
   1.500   0.3502   0.00743   0.00195  -0.0351   0.3923   0.7255
   1.750   0.3732   0.00768   0.00204  -0.0341   0.3599   0.7314
   2.000   0.3966   0.00788   0.00214  -0.0333   0.3328   0.7373
   2.250   0.4209   0.00804   0.00224  -0.0326   0.3142   0.7435
   2.500   0.4456   0.00820   0.00233  -0.0320   0.2988   0.7492
   2.750   0.4700   0.00837   0.00243  -0.0313   0.2832   0.7540
   3.000   0.4941   0.00853   0.00255  -0.0306   0.2685   0.7590
   3.250   0.5185   0.00869   0.00266  -0.0299   0.2561   0.7638
   3.500   0.5433   0.00884   0.00276  -0.0293   0.2452   0.7680
   3.750   0.5673   0.00900   0.00288  -0.0286   0.2338   0.7717
   4.000   0.5901   0.00918   0.00300  -0.0277   0.2211   0.7753
   4.250   0.6135   0.00932   0.00312  -0.0268   0.2112   0.7792
   4.500   0.6364   0.00948   0.00325  -0.0259   0.2022   0.7831
   4.750   0.6592   0.00966   0.00337  -0.0249   0.1924   0.7866
   5.000   0.6818   0.00983   0.00352  -0.0239   0.1829   0.7900
   5.250   0.7035   0.01004   0.00369  -0.0228   0.1722   0.7937
   5.500   0.7254   0.01025   0.00386  -0.0217   0.1620   0.7975
   5.750   0.7475   0.01046   0.00404  -0.0207   0.1529   0.8013
   6.000   0.7690   0.01071   0.00423  -0.0196   0.1436   0.8050
   6.250   0.7908   0.01093   0.00444  -0.0185   0.1354   0.8086
   6.500   0.8118   0.01116   0.00465  -0.0174   0.1282   0.8125
   6.750   0.8327   0.01142   0.00488  -0.0162   0.1205   0.8164
   7.000   0.8539   0.01166   0.00511  -0.0151   0.1144   0.8204
   7.250   0.8751   0.01192   0.00534  -0.0140   0.1091   0.8244
   7.500   0.8956   0.01217   0.00558  -0.0127   0.1045   0.8284
   7.750   0.9166   0.01239   0.00583  -0.0116   0.1012   0.8326
   8.000   0.9370   0.01265   0.00609  -0.0104   0.0978   0.8369
   8.250   0.9571   0.01294   0.00636  -0.0092   0.0939   0.8411
   8.500   0.9778   0.01317   0.00662  -0.0081   0.0918   0.8454
   8.750   0.9976   0.01343   0.00690  -0.0068   0.0895   0.8502
   9.000   1.0170   0.01371   0.00720  -0.0055   0.0871   0.8553
   9.250   1.0362   0.01403   0.00752  -0.0042   0.0847   0.8601
   9.500   1.0552   0.01432   0.00784  -0.0029   0.0829   0.8647
   9.750   1.0743   0.01459   0.00816  -0.0016   0.0818   0.8703
  10.000   1.0933   0.01489   0.00849  -0.0003   0.0803   0.8762
  10.250   1.1114   0.01521   0.00885   0.0011   0.0789   0.8819
  10.500   1.1284   0.01556   0.00923   0.0026   0.0774   0.8884
  10.750   1.1454   0.01594   0.00963   0.0041   0.0757   0.8951
  11.000   1.1608   0.01635   0.01009   0.0059   0.0738   0.9023
  11.250   1.1778   0.01669   0.01049   0.0074   0.0732   0.9110
  11.500   1.1940   0.01704   0.01090   0.0090   0.0724   0.9206
  11.750   1.2095   0.01742   0.01135   0.0106   0.0716   0.9326
  12.000   1.2261   0.01783   0.01183   0.0120   0.0705   0.9490
  12.250   1.2523   0.01834   0.01239   0.0112   0.0694   0.9693
  12.500   1.2745   0.01890   0.01298   0.0110   0.0677   1.0000
  12.750   1.2895   0.01949   0.01359   0.0123   0.0667   1.0000
  13.000   1.3029   0.02018   0.01429   0.0138   0.0654   1.0000
  13.250   1.3186   0.02075   0.01491   0.0149   0.0649   1.0000
  13.500   1.3339   0.02135   0.01556   0.0161   0.0642   1.0000
  13.750   1.3485   0.02200   0.01625   0.0172   0.0632   1.0000
  14.000   1.3623   0.02271   0.01699   0.0184   0.0622   1.0000
  14.250   1.3751   0.02350   0.01781   0.0196   0.0612   1.0000
  14.500   1.3871   0.02435   0.01869   0.0208   0.0602   1.0000
  14.750   1.3983   0.02529   0.01966   0.0220   0.0591   1.0000
  15.000   1.4081   0.02634   0.02074   0.0233   0.0580   1.0000
  15.250   1.4184   0.02738   0.02183   0.0244   0.0574   1.0000
  15.500   1.4302   0.02836   0.02287   0.0253   0.0568   1.0000
  15.750   1.4406   0.02947   0.02404   0.0262   0.0562   1.0000
  16.000   1.4502   0.03066   0.02529   0.0271   0.0555   1.0000
  16.250   1.4593   0.03193   0.02661   0.0279   0.0545   1.0000
  16.500   1.4674   0.03333   0.02806   0.0286   0.0538   1.0000
  16.750   1.4743   0.03487   0.02964   0.0293   0.0530   1.0000
  17.000   1.4801   0.03656   0.03138   0.0299   0.0522   1.0000
  17.250   1.4840   0.03847   0.03334   0.0304   0.0512   1.0000
  17.500   1.4892   0.04033   0.03527   0.0307   0.0506   1.0000
  17.750   1.4949   0.04220   0.03721   0.0309   0.0501   1.0000
  18.000   1.5003   0.04415   0.03924   0.0310   0.0491   1.0000
  18.250   1.5040   0.04633   0.04148   0.0310   0.0483   1.0000
  18.500   1.5060   0.04874   0.04396   0.0309   0.0475   1.0000
  18.750   1.5065   0.05138   0.04666   0.0305   0.0465   1.0000
  19.000   1.5045   0.05440   0.04974   0.0300   0.0456   1.0000
  19.250   1.5021   0.05755   0.05296   0.0294   0.0451   1.0000
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