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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 500,000
Max Cl/Cd: 61.35 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh94-il-500000-n5.txt
Download as CSV file: xf-mh94-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 94  16.03%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7766   0.14044   0.13685  -0.0362   1.0000   0.0081
 -19.500  -0.7943   0.13272   0.12900  -0.0402   1.0000   0.0081
 -19.250  -0.8115   0.12538   0.12151  -0.0438   1.0000   0.0080
 -19.000  -0.8257   0.11887   0.11489  -0.0470   1.0000   0.0080
 -18.750  -0.8392   0.11266   0.10857  -0.0500   1.0000   0.0080
 -18.500  -0.8507   0.10694   0.10273  -0.0526   1.0000   0.0080
 -18.250  -0.8607   0.10162   0.09732  -0.0550   1.0000   0.0080
 -18.000  -0.8725   0.09615   0.09174  -0.0574   1.0000   0.0080
 -17.750  -0.8810   0.09135   0.08684  -0.0594   1.0000   0.0080
 -17.500  -0.8910   0.08645   0.08185  -0.0614   1.0000   0.0081
 -17.250  -0.8995   0.08189   0.07720  -0.0632   1.0000   0.0081
 -17.000  -0.9061   0.07776   0.07297  -0.0646   1.0000   0.0081
 -16.750  -0.9130   0.07371   0.06882  -0.0659   1.0000   0.0081
 -16.500  -0.9189   0.06990   0.06493  -0.0671   1.0000   0.0082
 -16.250  -0.9258   0.06609   0.06104  -0.0681   1.0000   0.0083
 -16.000  -0.9295   0.06282   0.05769  -0.0688   1.0000   0.0082
 -15.750  -0.9350   0.05947   0.05426  -0.0693   1.0000   0.0083
 -15.500  -0.9379   0.05653   0.05124  -0.0696   1.0000   0.0083
 -15.250  -0.9429   0.05350   0.04813  -0.0697   1.0000   0.0083
 -15.000  -0.9460   0.05081   0.04537  -0.0696   1.0000   0.0083
 -14.750  -0.9483   0.04831   0.04281  -0.0693   1.0000   0.0084
 -14.500  -0.9511   0.04592   0.04035  -0.0687   1.0000   0.0085
 -14.250  -0.9527   0.04376   0.03812  -0.0680   1.0000   0.0085
 -14.000  -0.9552   0.04163   0.03591  -0.0670   1.0000   0.0086
 -13.750  -0.9560   0.03974   0.03397  -0.0658   1.0000   0.0086
 -13.500  -0.9590   0.03777   0.03193  -0.0644   1.0000   0.0086
 -13.250  -0.9592   0.03614   0.03024  -0.0628   1.0000   0.0087
 -13.000  -0.9620   0.03441   0.02844  -0.0610   1.0000   0.0088
 -12.750  -0.9626   0.03295   0.02693  -0.0590   1.0000   0.0089
 -12.500  -0.9605   0.03152   0.02544  -0.0574   0.9998   0.0089
 -12.250  -0.9459   0.02991   0.02375  -0.0582   0.9983   0.0091
 -12.000  -0.9293   0.02847   0.02225  -0.0591   0.9964   0.0092
 -11.750  -0.9121   0.02714   0.02086  -0.0599   0.9946   0.0094
 -11.500  -0.8938   0.02593   0.01958  -0.0607   0.9928   0.0095
 -11.250  -0.8780   0.02480   0.01838  -0.0608   0.9901   0.0097
 -11.000  -0.8590   0.02383   0.01736  -0.0611   0.9876   0.0099
 -10.750  -0.8373   0.02296   0.01643  -0.0618   0.9855   0.0101
 -10.500  -0.8175   0.02181   0.01524  -0.0626   0.9835   0.0105
 -10.250  -0.7997   0.02096   0.01435  -0.0623   0.9804   0.0107
 -10.000  -0.7830   0.02025   0.01361  -0.0615   0.9763   0.0111
  -9.750  -0.7606   0.01958   0.01289  -0.0617   0.9735   0.0113
  -9.500  -0.7353   0.01892   0.01220  -0.0623   0.9716   0.0117
  -9.250  -0.7187   0.01837   0.01160  -0.0609   0.9673   0.0122
  -9.000  -0.6989   0.01781   0.01099  -0.0600   0.9629   0.0126
  -8.750  -0.6729   0.01716   0.01033  -0.0604   0.9604   0.0133
  -8.500  -0.6438   0.01660   0.00976  -0.0613   0.9587   0.0140
  -8.250  -0.6129   0.01609   0.00921  -0.0625   0.9575   0.0151
  -8.000  -0.6006   0.01569   0.00881  -0.0597   0.9508   0.0160
  -7.750  -0.5741   0.01524   0.00835  -0.0598   0.9478   0.0176
  -7.500  -0.5447   0.01476   0.00788  -0.0606   0.9457   0.0200
  -7.250  -0.5144   0.01431   0.00743  -0.0614   0.9440   0.0235
  -7.000  -0.4913   0.01392   0.00705  -0.0607   0.9400   0.0278
  -6.750  -0.4718   0.01357   0.00671  -0.0592   0.9340   0.0324
  -6.500  -0.4449   0.01309   0.00630  -0.0593   0.9308   0.0427
  -6.250  -0.4158   0.01258   0.00587  -0.0599   0.9283   0.0576
  -6.000  -0.3987   0.01216   0.00554  -0.0580   0.9212   0.0765
  -5.750  -0.3757   0.01155   0.00511  -0.0574   0.9160   0.1112
  -5.500  -0.3488   0.01086   0.00465  -0.0577   0.9124   0.1603
  -5.250  -0.3301   0.01035   0.00434  -0.0561   0.9047   0.2037
  -5.000  -0.3051   0.00975   0.00398  -0.0559   0.8989   0.2581
  -4.750  -0.2772   0.00922   0.00366  -0.0562   0.8939   0.3110
  -4.500  -0.2538   0.00890   0.00346  -0.0554   0.8855   0.3459
  -4.250  -0.2234   0.00856   0.00322  -0.0560   0.8794   0.3820
  -4.000  -0.1984   0.00827   0.00308  -0.0554   0.8704   0.4211
  -3.750  -0.1683   0.00805   0.00292  -0.0559   0.8622   0.4500
  -3.500  -0.1408   0.00792   0.00280  -0.0557   0.8518   0.4670
  -3.250  -0.1103   0.00783   0.00267  -0.0561   0.8417   0.4802
  -3.000  -0.0823   0.00774   0.00257  -0.0559   0.8290   0.4920
  -2.750  -0.0541   0.00768   0.00248  -0.0559   0.8156   0.5029
  -2.500  -0.0259   0.00765   0.00240  -0.0557   0.8009   0.5137
  -2.250   0.0014   0.00762   0.00232  -0.0555   0.7845   0.5235
  -2.000   0.0284   0.00763   0.00226  -0.0551   0.7668   0.5338
  -1.750   0.0546   0.00763   0.00222  -0.0546   0.7480   0.5437
  -1.250   0.1059   0.00771   0.00216  -0.0534   0.7079   0.5632
  -1.000   0.1314   0.00778   0.00214  -0.0527   0.6875   0.5720
  -0.750   0.1564   0.00783   0.00214  -0.0520   0.6679   0.5801
  -0.500   0.1814   0.00791   0.00215  -0.0513   0.6469   0.5885
  -0.250   0.2061   0.00799   0.00216  -0.0505   0.6263   0.5961
   0.000   0.2304   0.00810   0.00219  -0.0497   0.6043   0.6042
   0.250   0.2549   0.00821   0.00222  -0.0489   0.5826   0.6118
   0.500   0.2791   0.00832   0.00226  -0.0480   0.5591   0.6193
   0.750   0.3030   0.00846   0.00231  -0.0472   0.5340   0.6272
   1.000   0.3258   0.00864   0.00238  -0.0461   0.5045   0.6342
   1.250   0.3476   0.00887   0.00246  -0.0448   0.4680   0.6421
   1.500   0.3696   0.00912   0.00256  -0.0437   0.4318   0.6493
   1.750   0.3927   0.00932   0.00266  -0.0427   0.4028   0.6567
   2.000   0.4163   0.00953   0.00277  -0.0418   0.3774   0.6645
   2.250   0.4399   0.00973   0.00289  -0.0410   0.3526   0.6715
   2.500   0.4638   0.00993   0.00301  -0.0402   0.3313   0.6793
   2.750   0.4878   0.01014   0.00313  -0.0395   0.3110   0.6865
   3.000   0.5112   0.01035   0.00328  -0.0386   0.2907   0.6936
   3.500   0.5586   0.01079   0.00358  -0.0370   0.2541   0.7078
   3.750   0.5822   0.01099   0.00375  -0.0362   0.2389   0.7149
   4.000   0.6059   0.01120   0.00391  -0.0355   0.2242   0.7223
   4.250   0.6292   0.01142   0.00409  -0.0346   0.2093   0.7290
   4.500   0.6521   0.01165   0.00428  -0.0337   0.1954   0.7363
   4.750   0.6749   0.01190   0.00447  -0.0328   0.1823   0.7437
   5.000   0.6968   0.01213   0.00467  -0.0317   0.1702   0.7504
   5.250   0.7185   0.01236   0.00488  -0.0305   0.1589   0.7580
   5.750   0.7608   0.01285   0.00532  -0.0281   0.1389   0.7724
   6.000   0.7814   0.01313   0.00557  -0.0268   0.1299   0.7805
   6.250   0.8027   0.01338   0.00582  -0.0256   0.1234   0.7877
   6.500   0.8230   0.01366   0.00610  -0.0243   0.1171   0.7958
   7.000   0.8643   0.01419   0.00667  -0.0218   0.1079   0.8121
   7.250   0.8842   0.01451   0.00698  -0.0204   0.1040   0.8209
   7.500   0.9044   0.01476   0.00729  -0.0191   0.1009   0.8293
   7.750   0.9239   0.01506   0.00761  -0.0177   0.0976   0.8391
   8.000   0.9423   0.01539   0.00796  -0.0162   0.0948   0.8486
   8.250   0.9613   0.01569   0.00831  -0.0147   0.0927   0.8594
   8.500   0.9796   0.01597   0.00865  -0.0131   0.0909   0.8708
   8.750   0.9972   0.01627   0.00901  -0.0114   0.0890   0.8834
   9.000   1.0139   0.01660   0.00940  -0.0096   0.0872   0.8983
   9.250   1.0291   0.01694   0.00980  -0.0075   0.0854   0.9175
   9.500   1.0473   0.01734   0.01026  -0.0061   0.0836   0.9458
  10.000   1.0961   0.01814   0.01115  -0.0062   0.0808   1.0000
  10.250   1.1141   0.01861   0.01164  -0.0050   0.0795   1.0000
  10.500   1.1315   0.01911   0.01216  -0.0037   0.0783   1.0000
  10.750   1.1480   0.01965   0.01271  -0.0024   0.0771   1.0000
  11.000   1.1635   0.02026   0.01333  -0.0010   0.0760   1.0000
  11.250   1.1770   0.02097   0.01406   0.0006   0.0748   1.0000
  11.500   1.1934   0.02154   0.01468   0.0018   0.0740   1.0000
  11.750   1.2092   0.02215   0.01534   0.0030   0.0732   1.0000
  12.000   1.2247   0.02278   0.01602   0.0042   0.0722   1.0000
  12.250   1.2391   0.02349   0.01678   0.0055   0.0713   1.0000
  12.500   1.2527   0.02426   0.01760   0.0068   0.0705   1.0000
  12.750   1.2657   0.02508   0.01846   0.0081   0.0697   1.0000
  13.000   1.2779   0.02598   0.01939   0.0093   0.0689   1.0000
  13.250   1.2890   0.02697   0.02042   0.0106   0.0681   1.0000
  13.500   1.2984   0.02810   0.02158   0.0119   0.0674   1.0000
  13.750   1.3064   0.02935   0.02287   0.0132   0.0666   1.0000
  14.000   1.3187   0.03036   0.02396   0.0141   0.0660   1.0000
  14.250   1.3294   0.03150   0.02518   0.0150   0.0654   1.0000
  14.500   1.3394   0.03273   0.02649   0.0159   0.0648   1.0000
  14.750   1.3486   0.03407   0.02790   0.0167   0.0641   1.0000
  15.000   1.3575   0.03547   0.02937   0.0174   0.0635   1.0000
  15.250   1.3656   0.03697   0.03095   0.0180   0.0629   1.0000
  15.500   1.3730   0.03860   0.03264   0.0186   0.0623   1.0000
  15.750   1.3792   0.04037   0.03447   0.0190   0.0617   1.0000
  16.000   1.3847   0.04227   0.03643   0.0193   0.0610   1.0000
  16.250   1.3885   0.04440   0.03862   0.0194   0.0604   1.0000
  16.500   1.3913   0.04671   0.04099   0.0195   0.0599   1.0000
  16.750   1.3925   0.04923   0.04357   0.0194   0.0593   1.0000
  17.000   1.3973   0.05148   0.04593   0.0192   0.0589   1.0000
  17.250   1.4010   0.05391   0.04846   0.0189   0.0585   1.0000
  17.500   1.4042   0.05646   0.05112   0.0184   0.0579   1.0000
  17.750   1.4063   0.05920   0.05396   0.0177   0.0573   1.0000
  18.000   1.4074   0.06212   0.05697   0.0169   0.0568   1.0000
  18.250   1.4077   0.06522   0.06017   0.0160   0.0563   1.0000
  18.500   1.4075   0.06847   0.06352   0.0148   0.0557   1.0000
  18.750   1.4061   0.07195   0.06709   0.0135   0.0552   1.0000
  19.000   1.4035   0.07564   0.07087   0.0120   0.0547   1.0000
  19.250   1.4001   0.07953   0.07484   0.0104   0.0542   1.0000
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