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Bambino 6 (bambino6-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Bambino 6 (bambino6-il)
Reynolds number: 500,000
Max Cl/Cd: 39.38 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-bambino6-il-500000-n5.txt
Download as CSV file: xf-bambino6-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Bambino 6                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6333   0.08350   0.08113  -0.0492   1.0000   0.0049
 -12.250  -0.6937   0.07053   0.06817  -0.0570   1.0000   0.0046
 -12.000  -0.8593   0.04682   0.04404  -0.0651   1.0000   0.0037
 -11.750  -0.8960   0.04034   0.03728  -0.0606   1.0000   0.0036
 -11.500  -0.9211   0.03681   0.03354  -0.0550   0.9991   0.0038
 -11.250  -0.9105   0.03356   0.03004  -0.0551   0.9957   0.0040
 -11.000  -0.9008   0.03067   0.02685  -0.0543   0.9914   0.0039
 -10.750  -0.8839   0.02867   0.02464  -0.0539   0.9879   0.0041
 -10.500  -0.8623   0.02704   0.02283  -0.0540   0.9852   0.0044
 -10.250  -0.8466   0.02540   0.02098  -0.0526   0.9797   0.0046
 -10.000  -0.8235   0.02406   0.01945  -0.0525   0.9764   0.0048
  -9.750  -0.8045   0.02289   0.01811  -0.0513   0.9713   0.0049
  -9.500  -0.7832   0.02169   0.01671  -0.0505   0.9667   0.0053
  -9.000  -0.7381   0.01976   0.01445  -0.0489   0.9565   0.0057
  -8.750  -0.7145   0.01854   0.01304  -0.0484   0.9518   0.0063
  -8.500  -0.6877   0.01763   0.01200  -0.0484   0.9476   0.0068
  -8.250  -0.6627   0.01690   0.01113  -0.0479   0.9412   0.0073
  -8.000  -0.6315   0.01614   0.01024  -0.0487   0.9370   0.0082
  -7.750  -0.5981   0.01539   0.00934  -0.0499   0.9326   0.0095
  -7.500  -0.5658   0.01459   0.00848  -0.0510   0.9264   0.0122
  -7.250  -0.5278   0.01386   0.00778  -0.0533   0.9214   0.0207
  -7.000  -0.4910   0.01351   0.00744  -0.0552   0.9143   0.0279
  -6.750  -0.4526   0.01323   0.00704  -0.0574   0.9066   0.0312
  -6.500  -0.4176   0.01293   0.00671  -0.0590   0.8975   0.0346
  -6.250  -0.3826   0.01274   0.00646  -0.0604   0.8882   0.0373
  -6.000  -0.3523   0.01252   0.00616  -0.0609   0.8772   0.0390
  -5.750  -0.3228   0.01246   0.00601  -0.0611   0.8659   0.0412
  -5.500  -0.2954   0.01220   0.00568  -0.0610   0.8537   0.0438
  -5.250  -0.2692   0.01196   0.00537  -0.0606   0.8411   0.0453
  -5.000  -0.2441   0.01175   0.00508  -0.0599   0.8275   0.0466
  -4.750  -0.2196   0.01158   0.00482  -0.0590   0.8137   0.0481
  -4.500  -0.1961   0.01142   0.00458  -0.0579   0.7974   0.0499
  -4.250  -0.1733   0.01132   0.00437  -0.0567   0.7765   0.0519
  -4.000  -0.1570   0.01138   0.00415  -0.0539   0.7149   0.0531
  -3.750  -0.1406   0.01141   0.00394  -0.0513   0.6690   0.0547
  -3.500  -0.1236   0.01142   0.00375  -0.0489   0.6333   0.0569
  -3.250  -0.1019   0.01137   0.00360  -0.0476   0.6178   0.0592
  -3.000  -0.0807   0.01135   0.00347  -0.0461   0.5979   0.0615
  -2.750  -0.0578   0.01129   0.00334  -0.0450   0.5870   0.0638
  -2.500  -0.0347   0.01124   0.00322  -0.0439   0.5745   0.0655
  -2.250  -0.0122   0.01123   0.00312  -0.0427   0.5582   0.0666
  -2.000   0.0091   0.01115   0.00294  -0.0413   0.5396   0.0690
  -1.750   0.0289   0.01113   0.00279  -0.0395   0.5050   0.0714
  -1.500   0.0450   0.01134   0.00269  -0.0371   0.4341   0.0734
  -1.250   0.0400   0.01291   0.00309  -0.0309   0.1083   0.0745
  -1.000   0.0608   0.01301   0.00305  -0.0294   0.0658   0.0766
  -0.750   0.0832   0.01303   0.00300  -0.0282   0.0604   0.0789
  -0.500   0.1057   0.01301   0.00297  -0.0271   0.0579   0.0829
  -0.250   0.1275   0.01295   0.00295  -0.0258   0.0554   0.0897
   0.000   0.1485   0.01287   0.00302  -0.0245   0.0547   0.1280
   0.250   0.1711   0.01291   0.00307  -0.0234   0.0540   0.1359
   0.500   0.1938   0.01297   0.00313  -0.0223   0.0533   0.1431
   0.750   0.2162   0.01304   0.00320  -0.0212   0.0522   0.1462
   1.000   0.2380   0.01309   0.00328  -0.0200   0.0513   0.1507
   1.250   0.2598   0.01316   0.00337  -0.0187   0.0500   0.1546
   1.500   0.2813   0.01326   0.00349  -0.0175   0.0490   0.1582
   1.750   0.3027   0.01337   0.00360  -0.0162   0.0483   0.1609
   2.000   0.3218   0.01352   0.00381  -0.0145   0.0454   0.1662
   2.250   0.3437   0.01355   0.00382  -0.0134   0.0440   0.1717
   2.750   0.3870   0.01359   0.00385  -0.0112   0.0393   0.1852
   3.000   0.4068   0.01365   0.00392  -0.0097   0.0376   0.1993
   3.250   0.4026   0.01272   0.00390  -0.0033   0.0346   0.5190
   3.500   0.3789   0.01182   0.00397   0.0083   0.0339   0.8295
   3.750   0.3918   0.01205   0.00410   0.0113   0.0171   0.8474
   4.000   0.4081   0.01219   0.00426   0.0137   0.0157   0.8572
   4.250   0.4251   0.01236   0.00444   0.0158   0.0146   0.8624
   4.500   0.4425   0.01255   0.00466   0.0178   0.0131   0.8686
   4.750   0.4601   0.01276   0.00490   0.0198   0.0126   0.8729
   5.000   0.4765   0.01301   0.00518   0.0219   0.0120   0.8766
   5.250   0.4919   0.01335   0.00558   0.0242   0.0107   0.8797
   5.500   0.5080   0.01372   0.00604   0.0263   0.0099   0.8835
   5.750   0.5240   0.01400   0.00636   0.0284   0.0094   0.8890
   6.000   0.5417   0.01429   0.00675   0.0301   0.0092   0.8987
   6.250   0.5590   0.01467   0.00718   0.0317   0.0080   0.9002
   6.500   0.5740   0.01510   0.00768   0.0338   0.0078   0.9058
   6.750   0.5918   0.01552   0.00816   0.0351   0.0068   0.9078
   7.000   0.6130   0.01596   0.00866   0.0357   0.0064   0.9101
   7.250   0.6359   0.01643   0.00919   0.0357   0.0066   0.9132
   7.500   0.6585   0.01694   0.00975   0.0358   0.0067   0.9160
   7.750   0.6855   0.01749   0.01037   0.0348   0.0066   0.9199
   8.000   0.7131   0.01816   0.01112   0.0335   0.0067   0.9232
   8.250   0.7530   0.01912   0.01218   0.0292   0.0069   0.9293
   8.500   0.7648   0.02194   0.01482   0.0283   0.0102   0.9329
   9.000   0.8456   0.02294   0.01612   0.0204   0.0050   0.9405
   9.250   0.8742   0.02351   0.01672   0.0189   0.0062   0.9430
   9.500   0.8916   0.02536   0.01860   0.0181   0.0049   0.9468
   9.750   0.9084   0.02694   0.02012   0.0180   0.0050   0.9490
  10.250   0.9551   0.02886   0.02206   0.0167   0.0063   0.9853
  10.500   0.9708   0.02996   0.02313   0.0176   0.0062   0.9916
  10.750   0.9901   0.03105   0.02418   0.0178   0.0062   0.9939
  11.000   1.0126   0.03223   0.02529   0.0181   0.0058   0.9959
  11.250   1.0382   0.03331   0.02633   0.0177   0.0058   0.9971
  11.500   1.2305   0.04030   0.03212  -0.0082   0.0052   0.9459
  11.750   1.2616   0.04224   0.03407  -0.0100   0.0052   0.9470
  12.000   1.2910   0.04426   0.03614  -0.0114   0.0052   0.9485
  12.250   1.3167   0.04620   0.03819  -0.0124   0.0052   0.9506
  12.500   1.3394   0.04811   0.04023  -0.0130   0.0052   0.9566
  13.000   1.3591   0.05133   0.04377  -0.0092   0.0051   0.9837
  13.250   1.3729   0.05330   0.04584  -0.0081   0.0051   0.9890
  13.500   1.3721   0.05460   0.04739  -0.0049   0.0051   0.9941
  13.750   1.3620   0.05538   0.04847  -0.0008   0.0051   0.9988
  14.000   1.3694   0.05741   0.05069   0.0003   0.0051   1.0000
  14.250   1.3408   0.05748   0.05095   0.0083   0.0050   1.0000
  14.500   1.3098   0.05772   0.05135   0.0159   0.0050   1.0000
  14.750   1.3108   0.05990   0.05367   0.0180   0.0050   1.0000
  15.000   1.2859   0.06103   0.05499   0.0229   0.0050   1.0000
  15.250   1.2565   0.06185   0.05599   0.0271   0.0049   1.0000
  15.500   1.2349   0.06333   0.05764   0.0297   0.0047   1.0000
  15.750   1.2176   0.06581   0.06029   0.0313   0.0046   1.0000
  16.000   1.2075   0.06858   0.06319   0.0321   0.0046   1.0000
  16.250   1.1924   0.07190   0.06668   0.0327   0.0045   1.0000
  16.500   1.1794   0.07516   0.07009   0.0327   0.0045   1.0000
  16.750   1.1645   0.07884   0.07392   0.0325   0.0044   1.0000
  17.000   1.1502   0.08275   0.07797   0.0318   0.0044   1.0000
  17.250   1.1337   0.08706   0.08243   0.0308   0.0044   1.0000
  17.500   1.1176   0.09163   0.08715   0.0293   0.0041   1.0000
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