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MB253515 15.0% smoothed (mb253515sm-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MB253515 15.0% smoothed (mb253515sm-il)
Reynolds number: 500,000
Max Cl/Cd: 83.63 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mb253515sm-il-500000-n5.txt
Download as CSV file: xf-mb253515sm-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MB253515 15.0% smoothed                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.7670   0.07431   0.07166  -0.0596   1.0000   0.0079
 -15.000  -0.8087   0.06289   0.06001  -0.0671   1.0000   0.0078
 -14.750  -0.8373   0.05499   0.05189  -0.0720   1.0000   0.0078
 -14.500  -0.8591   0.04903   0.04573  -0.0749   1.0000   0.0078
 -14.250  -0.8725   0.04473   0.04124  -0.0764   1.0000   0.0078
 -14.000  -0.8843   0.04101   0.03733  -0.0769   1.0000   0.0079
 -13.750  -0.8913   0.03807   0.03421  -0.0766   1.0000   0.0081
 -13.500  -0.9006   0.03519   0.03112  -0.0756   1.0000   0.0082
 -13.250  -0.9025   0.03317   0.02893  -0.0742   1.0000   0.0083
 -13.000  -0.9040   0.03133   0.02694  -0.0724   1.0000   0.0084
 -12.750  -0.9079   0.02956   0.02505  -0.0700   1.0000   0.0087
 -12.500  -0.9062   0.02836   0.02376  -0.0675   1.0000   0.0088
 -12.250  -0.9040   0.02738   0.02271  -0.0647   1.0000   0.0091
 -12.000  -0.8998   0.02639   0.02163  -0.0621   0.9993   0.0092
 -11.500  -0.8504   0.02440   0.01944  -0.0641   0.9718   0.0100
 -11.250  -0.8155   0.02358   0.01852  -0.0669   0.9603   0.0107
 -11.000  -0.7808   0.02220   0.01691  -0.0699   0.9468   0.0113
 -10.750  -0.7445   0.02106   0.01563  -0.0730   0.9315   0.0121
 -10.500  -0.7111   0.02053   0.01501  -0.0751   0.9129   0.0126
 -10.250  -0.6876   0.02002   0.01436  -0.0750   0.8932   0.0131
 -10.000  -0.6687   0.01971   0.01393  -0.0738   0.8759   0.0137
  -9.750  -0.6516   0.01923   0.01331  -0.0722   0.8609   0.0144
  -9.500  -0.6332   0.01880   0.01272  -0.0709   0.8477   0.0152
  -9.250  -0.6152   0.01831   0.01209  -0.0694   0.8361   0.0159
  -9.000  -0.5968   0.01794   0.01164  -0.0680   0.8255   0.0165
  -8.750  -0.5769   0.01766   0.01129  -0.0668   0.8150   0.0171
  -8.500  -0.5557   0.01748   0.01105  -0.0658   0.8059   0.0179
  -8.000  -0.5144   0.01673   0.01008  -0.0636   0.7889   0.0197
  -7.750  -0.4928   0.01644   0.00967  -0.0627   0.7810   0.0206
  -7.500  -0.4702   0.01618   0.00932  -0.0618   0.7734   0.0211
  -7.250  -0.4522   0.01546   0.00853  -0.0604   0.7665   0.0221
  -7.000  -0.4305   0.01512   0.00816  -0.0595   0.7592   0.0231
  -6.500  -0.3860   0.01450   0.00741  -0.0577   0.7459   0.0250
  -6.250  -0.3641   0.01415   0.00699  -0.0568   0.7396   0.0258
  -6.000  -0.3415   0.01383   0.00660  -0.0559   0.7337   0.0267
  -5.750  -0.3183   0.01357   0.00627  -0.0552   0.7272   0.0275
  -5.500  -0.2954   0.01330   0.00592  -0.0544   0.7217   0.0279
  -5.250  -0.2739   0.01286   0.00542  -0.0533   0.7160   0.0286
  -5.000  -0.2527   0.01243   0.00493  -0.0522   0.7102   0.0298
  -4.750  -0.2296   0.01215   0.00460  -0.0514   0.7049   0.0310
  -4.500  -0.2058   0.01190   0.00431  -0.0508   0.6993   0.0320
  -4.250  -0.1817   0.01168   0.00402  -0.0501   0.6941   0.0327
  -4.000  -0.1572   0.01147   0.00377  -0.0496   0.6890   0.0336
  -3.750  -0.1324   0.01129   0.00354  -0.0491   0.6836   0.0345
  -3.500  -0.1075   0.01113   0.00332  -0.0486   0.6785   0.0355
  -3.250  -0.0822   0.01099   0.00313  -0.0482   0.6737   0.0365
  -3.000  -0.0571   0.01082   0.00294  -0.0477   0.6684   0.0398
  -2.750  -0.0319   0.01068   0.00278  -0.0472   0.6634   0.0443
  -2.500  -0.0071   0.01051   0.00262  -0.0467   0.6572   0.0574
  -2.250   0.0074   0.00957   0.00229  -0.0447   0.6494   0.2294
  -2.000   0.0275   0.00910   0.00213  -0.0434   0.6412   0.3212
  -1.750   0.0477   0.00870   0.00199  -0.0421   0.6335   0.4055
  -1.500   0.0686   0.00835   0.00191  -0.0409   0.6275   0.4825
  -1.250   0.0894   0.00806   0.00186  -0.0396   0.6219   0.5553
  -1.000   0.1129   0.00795   0.00183  -0.0388   0.6168   0.5960
  -0.750   0.1370   0.00783   0.00182  -0.0380   0.6113   0.6323
  -0.500   0.1608   0.00774   0.00183  -0.0372   0.6057   0.6696
  -0.250   0.1853   0.00769   0.00184  -0.0365   0.6001   0.6972
   0.000   0.2102   0.00765   0.00186  -0.0359   0.5942   0.7231
   0.250   0.2351   0.00764   0.00188  -0.0353   0.5886   0.7465
   0.500   0.2610   0.00763   0.00189  -0.0349   0.5823   0.7617
   0.750   0.2869   0.00764   0.00191  -0.0346   0.5758   0.7741
   1.000   0.3129   0.00766   0.00194  -0.0342   0.5697   0.7862
   1.250   0.3389   0.00768   0.00197  -0.0339   0.5629   0.7983
   1.500   0.3646   0.00772   0.00201  -0.0335   0.5562   0.8104
   1.750   0.3905   0.00775   0.00206  -0.0332   0.5484   0.8225
   2.000   0.4162   0.00779   0.00211  -0.0328   0.5411   0.8350
   2.250   0.4421   0.00783   0.00218  -0.0324   0.5330   0.8481
   2.500   0.4679   0.00788   0.00225  -0.0321   0.5247   0.8606
   2.750   0.4935   0.00796   0.00232  -0.0317   0.5151   0.8722
   3.000   0.5200   0.00803   0.00241  -0.0315   0.5055   0.8835
   3.250   0.5469   0.00812   0.00251  -0.0314   0.4957   0.8941
   3.750   0.6017   0.00837   0.00274  -0.0316   0.4713   0.9161
   4.000   0.6329   0.00853   0.00289  -0.0325   0.4585   0.9251
   4.250   0.6634   0.00870   0.00305  -0.0334   0.4453   0.9341
   4.500   0.6956   0.00892   0.00323  -0.0346   0.4304   0.9419
   4.750   0.7269   0.00915   0.00343  -0.0357   0.4157   0.9491
   5.000   0.7600   0.00939   0.00365  -0.0372   0.4023   0.9548
   5.250   0.7901   0.00963   0.00386  -0.0380   0.3901   0.9617
   5.500   0.8238   0.00989   0.00411  -0.0397   0.3777   0.9656
   5.750   0.8523   0.01020   0.00437  -0.0403   0.3618   0.9721
   6.000   0.8823   0.01055   0.00466  -0.0413   0.3442   0.9768
   6.250   0.9104   0.01093   0.00498  -0.0419   0.3253   0.9826
   6.500   0.9394   0.01133   0.00531  -0.0428   0.3065   0.9875
   6.750   0.9687   0.01173   0.00564  -0.0437   0.2850   0.9923
   7.000   0.9974   0.01221   0.00602  -0.0447   0.2606   0.9972
   7.250   1.0171   0.01289   0.00651  -0.0440   0.2208   1.0000
   7.500   1.0175   0.01350   0.00694  -0.0392   0.1869   1.0000
   7.750   0.9989   0.01451   0.00762  -0.0309   0.1299   1.0000
   8.000   0.9752   0.01593   0.00866  -0.0222   0.0631   1.0000
   8.250   0.9758   0.01679   0.00942  -0.0181   0.0398   1.0000
   8.500   0.9829   0.01749   0.01009  -0.0151   0.0294   1.0000
   8.750   0.9918   0.01818   0.01078  -0.0126   0.0230   1.0000
   9.000   1.0011   0.01892   0.01152  -0.0103   0.0185   1.0000
   9.250   1.0122   0.01963   0.01228  -0.0084   0.0164   1.0000
   9.500   1.0228   0.02043   0.01311  -0.0066   0.0148   1.0000
   9.750   1.0326   0.02132   0.01404  -0.0047   0.0137   1.0000
  10.000   1.0412   0.02235   0.01512  -0.0029   0.0124   1.0000
  10.250   1.0515   0.02333   0.01616  -0.0014   0.0120   1.0000
  10.500   1.0605   0.02443   0.01733   0.0000   0.0114   1.0000
  10.750   1.0706   0.02551   0.01847   0.0013   0.0107   1.0000
  11.000   1.0784   0.02681   0.01982   0.0026   0.0101   1.0000
  11.250   1.0848   0.02826   0.02134   0.0039   0.0097   1.0000
  11.500   1.0873   0.03008   0.02324   0.0053   0.0092   1.0000
  11.750   1.0905   0.03191   0.02514   0.0064   0.0090   1.0000
  12.000   1.0961   0.03360   0.02691   0.0074   0.0088   1.0000
  12.250   1.1007   0.03543   0.02883   0.0082   0.0085   1.0000
  12.500   1.1050   0.03733   0.03081   0.0090   0.0083   1.0000
  12.750   1.1069   0.03952   0.03309   0.0097   0.0081   1.0000
  13.000   1.1097   0.04170   0.03535   0.0102   0.0080   1.0000
  13.250   1.1129   0.04389   0.03762   0.0106   0.0076   1.0000
  13.500   1.1166   0.04609   0.03990   0.0109   0.0074   1.0000
  13.750   1.1179   0.04861   0.04250   0.0111   0.0071   1.0000
  14.000   1.1220   0.05089   0.04483   0.0112   0.0068   1.0000
  14.250   1.1230   0.05356   0.04757   0.0112   0.0067   1.0000
  14.500   1.1208   0.05664   0.05074   0.0112   0.0066   1.0000
  14.750   1.1180   0.05987   0.05405   0.0110   0.0065   1.0000
  15.000   1.1126   0.06343   0.05768   0.0108   0.0063   1.0000
  15.250   1.1127   0.06643   0.06076   0.0105   0.0062   1.0000
  15.500   1.1095   0.06983   0.06426   0.0102   0.0062   1.0000
  15.750   1.1107   0.07279   0.06731   0.0097   0.0061   1.0000
  16.000   1.1113   0.07584   0.07046   0.0093   0.0060   1.0000
  16.250   1.1121   0.07892   0.07363   0.0087   0.0058   1.0000
  16.500   1.1116   0.08218   0.07700   0.0081   0.0057   1.0000
  16.750   1.1103   0.08550   0.08040   0.0076   0.0058   1.0000
  17.000   1.1103   0.08877   0.08377   0.0068   0.0056   1.0000
  17.250   1.1091   0.09218   0.08727   0.0061   0.0055   1.0000
  17.500   1.1094   0.09554   0.09073   0.0051   0.0053   1.0000
  17.750   1.1076   0.09905   0.09433   0.0043   0.0053   1.0000
  18.000   1.1065   0.10265   0.09802   0.0032   0.0052   1.0000
  18.250   1.1046   0.10636   0.10183   0.0021   0.0051   1.0000
  18.500   1.1037   0.11003   0.10559   0.0007   0.0050   1.0000
  18.750   1.1012   0.11387   0.10952  -0.0006   0.0050   1.0000
  19.000   1.0983   0.11786   0.11361  -0.0021   0.0049   1.0000
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