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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 100,000
Max Cl/Cd: 43.74 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh104-il-100000-n5.txt
Download as CSV file: xf-mh104-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6160   0.11137   0.10630  -0.0073   1.0000   0.0185
 -13.500  -0.6357   0.10216   0.09704  -0.0127   1.0000   0.0183
 -13.250  -0.6521   0.09428   0.08910  -0.0176   1.0000   0.0179
 -13.000  -0.6734   0.08585   0.08055  -0.0232   1.0000   0.0175
 -12.750  -0.6984   0.07735   0.07187  -0.0292   1.0000   0.0175
 -12.500  -0.7165   0.07073   0.06508  -0.0337   1.0000   0.0172
 -12.250  -0.7356   0.06460   0.05873  -0.0377   1.0000   0.0172
 -12.000  -0.7509   0.05959   0.05351  -0.0405   1.0000   0.0173
 -11.750  -0.7617   0.05554   0.04926  -0.0420   1.0000   0.0172
 -11.500  -0.7725   0.05189   0.04539  -0.0428   1.0000   0.0174
 -11.250  -0.7808   0.04875   0.04200  -0.0426   1.0000   0.0177
 -11.000  -0.7871   0.04595   0.03893  -0.0415   1.0000   0.0181
 -10.750  -0.7916   0.04347   0.03616  -0.0398   1.0000   0.0186
 -10.500  -0.7868   0.04148   0.03408  -0.0384   1.0000   0.0189
 -10.250  -0.7820   0.03974   0.03229  -0.0366   1.0000   0.0195
 -10.000  -0.7752   0.03813   0.03057  -0.0348   1.0000   0.0201
  -9.750  -0.7658   0.03640   0.02871  -0.0331   1.0000   0.0209
  -9.500  -0.7533   0.03470   0.02685  -0.0317   1.0000   0.0214
  -9.250  -0.7398   0.03307   0.02509  -0.0302   1.0000   0.0222
  -9.000  -0.7258   0.03159   0.02346  -0.0286   1.0000   0.0230
  -8.750  -0.7143   0.03013   0.02202  -0.0269   1.0000   0.0239
  -8.500  -0.7020   0.02895   0.02086  -0.0252   1.0000   0.0253
  -8.250  -0.6888   0.02787   0.01971  -0.0235   1.0000   0.0273
  -8.000  -0.6634   0.02647   0.01825  -0.0244   0.9494   0.0302
  -7.500  -0.6127   0.02402   0.01546  -0.0251   0.8769   0.0387
  -7.250  -0.5956   0.02303   0.01433  -0.0234   0.8500   0.0457
  -7.000  -0.5795   0.02205   0.01328  -0.0215   0.8273   0.0561
  -6.750  -0.5640   0.02098   0.01224  -0.0196   0.8072   0.0771
  -6.500  -0.5495   0.01977   0.01130  -0.0177   0.7893   0.1267
  -6.250  -0.5319   0.01898   0.01074  -0.0161   0.7729   0.1877
  -6.000  -0.5112   0.01856   0.01034  -0.0149   0.7573   0.2312
  -5.750  -0.4899   0.01825   0.01002  -0.0137   0.7425   0.2653
  -5.500  -0.4680   0.01800   0.00974  -0.0125   0.7285   0.2969
  -5.250  -0.4455   0.01781   0.00947  -0.0114   0.7153   0.3250
  -5.000  -0.4225   0.01761   0.00921  -0.0103   0.7030   0.3475
  -4.750  -0.3986   0.01742   0.00890  -0.0094   0.6912   0.3669
  -4.500  -0.3737   0.01721   0.00859  -0.0087   0.6790   0.3842
  -4.250  -0.3486   0.01702   0.00830  -0.0080   0.6677   0.4009
  -4.000  -0.3235   0.01684   0.00801  -0.0073   0.6574   0.4175
  -3.750  -0.2982   0.01665   0.00777  -0.0067   0.6466   0.4344
  -3.500  -0.2727   0.01647   0.00754  -0.0061   0.6366   0.4518
  -3.250  -0.2474   0.01631   0.00731  -0.0054   0.6279   0.4703
  -3.000  -0.2217   0.01615   0.00714  -0.0048   0.6178   0.4897
  -2.750  -0.1962   0.01602   0.00694  -0.0042   0.6094   0.5109
  -2.500  -0.1704   0.01588   0.00680  -0.0036   0.6003   0.5326
  -2.250  -0.1447   0.01576   0.00668  -0.0030   0.5924   0.5568
  -2.000  -0.1187   0.01565   0.00659  -0.0024   0.5844   0.5822
  -1.750  -0.0926   0.01557   0.00651  -0.0018   0.5772   0.6101
  -1.500  -0.0662   0.01549   0.00647  -0.0013   0.5693   0.6397
  -1.250  -0.0392   0.01544   0.00642  -0.0008   0.5626   0.6711
  -1.000  -0.0113   0.01541   0.00646  -0.0005   0.5551   0.7034
  -0.750   0.0177   0.01541   0.00646  -0.0003   0.5495   0.7364
  -0.500   0.0483   0.01547   0.00657  -0.0005   0.5424   0.7689
  -0.250   0.0806   0.01555   0.00664  -0.0009   0.5362   0.7998
   0.000   0.1148   0.01568   0.00675  -0.0018   0.5299   0.8283
   0.250   0.1517   0.01585   0.00690  -0.0032   0.5234   0.8523
   0.500   0.1876   0.01603   0.00698  -0.0044   0.5185   0.8745
   0.750   0.2240   0.01624   0.00718  -0.0060   0.5122   0.8940
   1.000   0.2615   0.01643   0.00731  -0.0077   0.5065   0.9107
   1.250   0.2991   0.01663   0.00740  -0.0094   0.5017   0.9257
   1.500   0.3365   0.01686   0.00764  -0.0114   0.4956   0.9395
   1.750   0.3775   0.01705   0.00776  -0.0140   0.4904   0.9506
   2.000   0.4170   0.01722   0.00784  -0.0164   0.4858   0.9619
   2.250   0.4560   0.01741   0.00806  -0.0189   0.4798   0.9731
   2.500   0.4956   0.01755   0.00816  -0.0214   0.4749   0.9834
   2.750   0.5371   0.01766   0.00821  -0.0244   0.4703   0.9925
   3.000   0.5768   0.01780   0.00842  -0.0273   0.4643   1.0000
   3.250   0.5980   0.01795   0.00855  -0.0264   0.4600   1.0000
   3.500   0.6198   0.01810   0.00863  -0.0255   0.4564   1.0000
   3.750   0.6406   0.01836   0.00898  -0.0246   0.4512   1.0000
   4.000   0.6619   0.01859   0.00923  -0.0237   0.4465   1.0000
   4.250   0.6840   0.01878   0.00938  -0.0227   0.4425   1.0000
   4.500   0.7055   0.01905   0.00969  -0.0218   0.4381   1.0000
   4.750   0.7265   0.01935   0.01008  -0.0209   0.4328   1.0000
   5.000   0.7486   0.01957   0.01030  -0.0200   0.4284   1.0000
   5.250   0.7710   0.01981   0.01052  -0.0191   0.4244   1.0000
   5.500   0.7912   0.02019   0.01105  -0.0181   0.4186   1.0000
   5.750   0.8131   0.02046   0.01134  -0.0172   0.4138   1.0000
   6.000   0.8361   0.02066   0.01151  -0.0163   0.4097   1.0000
   6.250   0.8554   0.02110   0.01214  -0.0152   0.4034   1.0000
   6.500   0.8772   0.02136   0.01243  -0.0142   0.3982   1.0000
   6.750   0.8995   0.02161   0.01270  -0.0133   0.3934   1.0000
   7.000   0.9183   0.02205   0.01329  -0.0121   0.3867   1.0000
   7.250   0.9407   0.02224   0.01351  -0.0112   0.3813   1.0000
   7.500   0.9599   0.02265   0.01405  -0.0100   0.3749   1.0000
   7.750   0.9800   0.02295   0.01443  -0.0089   0.3683   1.0000
   8.000   1.0009   0.02321   0.01476  -0.0078   0.3623   1.0000
   8.250   1.0184   0.02364   0.01534  -0.0064   0.3546   1.0000
   8.500   1.0396   0.02382   0.01554  -0.0053   0.3485   1.0000
   8.750   1.0550   0.02434   0.01626  -0.0037   0.3401   1.0000
   9.000   1.0746   0.02457   0.01652  -0.0024   0.3332   1.0000
   9.250   1.0889   0.02510   0.01724  -0.0007   0.3243   1.0000
   9.500   1.1051   0.02547   0.01770   0.0008   0.3162   1.0000
   9.750   1.1195   0.02591   0.01824   0.0026   0.3073   1.0000
  10.000   1.1313   0.02650   0.01896   0.0045   0.2979   1.0000
  10.250   1.1443   0.02694   0.01944   0.0064   0.2890   1.0000
  10.500   1.1522   0.02766   0.02029   0.0086   0.2791   1.0000
  10.750   1.1578   0.02845   0.02117   0.0111   0.2694   1.0000
  11.000   1.1603   0.02921   0.02193   0.0140   0.2605   1.0000
  11.250   1.1584   0.03041   0.02321   0.0167   0.2511   1.0000
  11.500   1.1570   0.03183   0.02468   0.0187   0.2419   1.0000
  11.750   1.1566   0.03335   0.02617   0.0202   0.2328   1.0000
  12.000   1.1519   0.03551   0.02844   0.0213   0.2232   1.0000
  12.250   1.1484   0.03774   0.03070   0.0221   0.2141   1.0000
  12.500   1.1450   0.04007   0.03305   0.0226   0.2052   1.0000
  12.750   1.1387   0.04296   0.03603   0.0227   0.1964   1.0000
  13.000   1.1342   0.04567   0.03874   0.0228   0.1880   1.0000
  13.250   1.1273   0.04883   0.04195   0.0226   0.1795   1.0000
  13.500   1.1214   0.05196   0.04513   0.0223   0.1715   1.0000
  13.750   1.1157   0.05509   0.04826   0.0219   0.1637   1.0000
  14.000   1.1082   0.05863   0.05189   0.0213   0.1561   1.0000
  14.250   1.1036   0.06174   0.05496   0.0208   0.1489   1.0000
  14.500   1.0958   0.06563   0.05898   0.0198   0.1416   1.0000
  14.750   1.0923   0.06884   0.06213   0.0191   0.1349   1.0000
  15.000   1.0845   0.07300   0.06643   0.0178   0.1280   1.0000
  15.250   1.0812   0.07632   0.06969   0.0170   0.1217   1.0000
  15.500   1.0734   0.08069   0.07422   0.0155   0.1152   1.0000
  15.750   1.0696   0.08430   0.07779   0.0143   0.1092   1.0000
  16.000   1.0622   0.08877   0.08239   0.0127   0.1033   1.0000
  16.250   1.0574   0.09275   0.08641   0.0113   0.0977   1.0000
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