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Bambino 6 (bambino6-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: Bambino 6 (bambino6-il)
Reynolds number: 500,000
Max Cl/Cd: 54.59 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-bambino6-il-500000.txt
Download as CSV file: xf-bambino6-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.6082   0.07798   0.07589  -0.0516   1.0000   0.0139
 -11.500  -0.8119   0.04284   0.04032  -0.0684   1.0000   0.0115
 -11.250  -0.8682   0.03859   0.03576  -0.0590   1.0000   0.0111
 -11.000  -0.8885   0.03712   0.03417  -0.0521   1.0000   0.0113
 -10.750  -0.9086   0.03503   0.03188  -0.0454   1.0000   0.0112
 -10.500  -0.9119   0.03406   0.03081  -0.0407   0.9999   0.0118
 -10.250  -0.8971   0.03078   0.02715  -0.0409   0.9963   0.0121
 -10.000  -0.8799   0.02807   0.02406  -0.0407   0.9928   0.0125
  -9.750  -0.8581   0.02636   0.02207  -0.0406   0.9890   0.0129
  -9.500  -0.8368   0.02398   0.01932  -0.0404   0.9854   0.0137
  -9.250  -0.8099   0.02230   0.01745  -0.0411   0.9831   0.0148
  -9.000  -0.7829   0.02190   0.01701  -0.0411   0.9790   0.0159
  -8.750  -0.7547   0.02121   0.01622  -0.0414   0.9753   0.0171
  -8.500  -0.7233   0.02045   0.01527  -0.0422   0.9727   0.0183
  -8.250  -0.6947   0.01888   0.01354  -0.0428   0.9705   0.0204
  -8.000  -0.6634   0.01858   0.01322  -0.0434   0.9671   0.0224
  -7.750  -0.6351   0.01825   0.01279  -0.0433   0.9620   0.0246
  -7.500  -0.6047   0.01743   0.01191  -0.0440   0.9592   0.0279
  -7.250  -0.5690   0.01756   0.01204  -0.0455   0.9572   0.0311
  -7.000  -0.5328   0.01741   0.01179  -0.0470   0.9556   0.0334
  -6.750  -0.5104   0.01640   0.01067  -0.0460   0.9493   0.0363
  -6.500  -0.4781   0.01643   0.01070  -0.0468   0.9457   0.0387
  -6.250  -0.4426   0.01620   0.01040  -0.0482   0.9431   0.0413
  -6.000  -0.4046   0.01602   0.01013  -0.0502   0.9411   0.0434
  -5.750  -0.3781   0.01508   0.00909  -0.0500   0.9341   0.0460
  -5.500  -0.3423   0.01482   0.00883  -0.0516   0.9296   0.0486
  -5.250  -0.3017   0.01437   0.00832  -0.0543   0.9262   0.0510
  -5.000  -0.2727   0.01401   0.00788  -0.0544   0.9171   0.0531
  -4.750  -0.2322   0.01355   0.00733  -0.0569   0.9117   0.0548
  -4.500  -0.2012   0.01286   0.00656  -0.0575   0.9018   0.0566
  -4.250  -0.1672   0.01205   0.00575  -0.0589   0.8927   0.0600
  -4.000  -0.1340   0.01171   0.00535  -0.0600   0.8818   0.0632
  -3.750  -0.1061   0.01143   0.00500  -0.0598   0.8679   0.0662
  -3.500  -0.0802   0.01129   0.00470  -0.0591   0.8391   0.0683
  -3.250  -0.0590   0.01077   0.00405  -0.0575   0.8089   0.0720
  -3.000  -0.0397   0.01052   0.00367  -0.0555   0.7766   0.0754
  -2.750  -0.0211   0.01038   0.00339  -0.0533   0.7405   0.0785
  -2.500  -0.0030   0.01033   0.00315  -0.0511   0.7049   0.0812
  -2.250   0.0141   0.01030   0.00293  -0.0486   0.6731   0.0846
  -2.000   0.0334   0.01022   0.00276  -0.0467   0.6525   0.0900
  -1.750   0.0528   0.01018   0.00263  -0.0448   0.6326   0.0953
  -1.500   0.0733   0.01012   0.00262  -0.0432   0.6176   0.1136
  -1.250   0.0949   0.01013   0.00263  -0.0418   0.6028   0.1404
  -1.000   0.1168   0.01017   0.00260  -0.0404   0.5872   0.1528
  -0.750   0.1387   0.01018   0.00257  -0.0391   0.5726   0.1617
  -0.500   0.1600   0.01018   0.00252  -0.0377   0.5557   0.1683
  -0.250   0.1784   0.01025   0.00247  -0.0356   0.5218   0.1747
   0.000   0.1958   0.01039   0.00242  -0.0334   0.4733   0.1809
   0.250   0.1849   0.01206   0.00288  -0.0259   0.1744   0.1844
   0.500   0.1995   0.01249   0.00303  -0.0233   0.0966   0.1902
   0.750   0.2190   0.01263   0.00308  -0.0217   0.0685   0.1969
   1.000   0.2400   0.01264   0.00312  -0.0202   0.0642   0.2089
   1.250   0.2594   0.01257   0.00316  -0.0185   0.0622   0.2416
   1.500   0.2693   0.01215   0.00322  -0.0149   0.0614   0.3886
   1.750   0.2375   0.01074   0.00307  -0.0019   0.0612   0.7435
   2.000   0.2443   0.01085   0.00339   0.0032   0.0605   0.8528
   2.250   0.2581   0.01099   0.00355   0.0064   0.0599   0.8707
   2.500   0.2743   0.01112   0.00372   0.0091   0.0588   0.8848
   2.750   0.2955   0.01125   0.00389   0.0105   0.0573   0.8939
   3.000   0.3109   0.01149   0.00417   0.0131   0.0534   0.9029
   3.250   0.3359   0.01163   0.00434   0.0136   0.0501   0.9136
   3.500   0.3761   0.01178   0.00449   0.0105   0.0471   0.9227
   3.750   0.4090   0.01210   0.00478   0.0089   0.0418   0.9313
   4.000   0.4703   0.01228   0.00486   0.0011   0.0391   0.9382
   4.250   0.5053   0.01249   0.00503  -0.0009   0.0370   0.9428
   4.500   0.5452   0.01277   0.00521  -0.0040   0.0329   0.9458
   4.750   0.5929   0.01335   0.00568  -0.0089   0.0180   0.9498
   5.000   0.6278   0.01376   0.00609  -0.0107   0.0175   0.9552
   5.250   0.6531   0.01403   0.00635  -0.0105   0.0176   0.9584
   5.500   0.6829   0.01434   0.00665  -0.0114   0.0177   0.9595
   5.750   0.7098   0.01478   0.00717  -0.0118   0.0168   0.9610
   6.000   0.7339   0.01508   0.00748  -0.0115   0.0169   0.9624
   6.250   0.7591   0.01534   0.00774  -0.0114   0.0173   0.9643
   6.500   0.7822   0.01552   0.00791  -0.0110   0.0179   0.9664
   6.750   0.7989   0.01579   0.00820  -0.0092   0.0183   0.9697
   7.000   0.8209   0.01620   0.00864  -0.0086   0.0189   0.9719
   7.250   0.8496   0.01650   0.00897  -0.0095   0.0196   0.9737
   7.500   0.8746   0.01681   0.00922  -0.0096   0.0226   0.9757
   7.750   0.8841   0.01785   0.01024  -0.0070   0.0229   0.9801
   8.000   0.9204   0.01733   0.00972  -0.0090   0.0219   0.9820
   8.250   0.9493   0.01739   0.00983  -0.0098   0.0211   0.9841
   8.500   0.9731   0.01823   0.01086  -0.0102   0.0200   0.9868
   8.750   0.9913   0.01915   0.01194  -0.0095   0.0191   0.9902
   9.000   1.0071   0.01998   0.01287  -0.0084   0.0183   0.9931
   9.250   1.0215   0.02118   0.01424  -0.0074   0.0172   0.9958
   9.500   1.0313   0.02294   0.01604  -0.0063   0.0165   0.9987
   9.750   1.0250   0.02447   0.01759  -0.0023   0.0154   1.0000
  10.000   1.0221   0.02534   0.01850   0.0021   0.0146   1.0000
  10.250   1.0243   0.02632   0.01950   0.0051   0.0146   1.0000
  10.500   1.0192   0.02812   0.02127   0.0089   0.0140   1.0000
  10.750   1.0314   0.03035   0.02318   0.0105   0.0129   1.0000
  11.000   1.0301   0.03110   0.02417   0.0134   0.0124   1.0000
  11.250   1.0390   0.03219   0.02532   0.0151   0.0117   1.0000
  11.500   1.0528   0.03335   0.02643   0.0162   0.0114   1.0000
  11.750   1.2179   0.03653   0.02882  -0.0037   0.0100   1.0000
  12.000   1.2040   0.03683   0.02925   0.0027   0.0100   1.0000
  12.250   1.1828   0.03718   0.02979   0.0096   0.0098   1.0000
  12.500   1.1727   0.03796   0.03073   0.0140   0.0096   1.0000
  12.750   1.1715   0.03900   0.03190   0.0168   0.0094   1.0000
  13.000   1.1810   0.04021   0.03319   0.0182   0.0092   1.0000
  13.250   1.5147   0.05753   0.04916  -0.0339   0.0075   0.9994
  13.500   1.5233   0.05920   0.05097  -0.0316   0.0075   1.0000
  13.750   1.5266   0.06070   0.05264  -0.0283   0.0075   1.0000
  14.000   1.5279   0.06219   0.05431  -0.0248   0.0075   1.0000
  14.250   1.5295   0.06374   0.05603  -0.0216   0.0075   1.0000
  14.500   1.5279   0.06521   0.05771  -0.0179   0.0075   1.0000
  14.750   1.5150   0.06602   0.05878  -0.0127   0.0075   1.0000
  15.000   1.5068   0.06758   0.06055  -0.0084   0.0074   1.0000
  15.250   1.4930   0.06865   0.06184  -0.0035   0.0074   1.0000
  15.500   1.4712   0.06939   0.06281   0.0024   0.0074   1.0000
  15.750   1.4600   0.07101   0.06458   0.0065   0.0074   1.0000
  16.000   1.4352   0.07187   0.06561   0.0128   0.0074   1.0000
  16.250   1.4110   0.07300   0.06690   0.0181   0.0074   1.0000
  16.500   1.3876   0.07444   0.06850   0.0223   0.0073   1.0000
  16.750   1.3709   0.07656   0.07077   0.0251   0.0073   1.0000
  17.000   1.3518   0.07897   0.07333   0.0275   0.0073   1.0000
  17.250   1.3275   0.08119   0.07571   0.0296   0.0073   1.0000
  17.500   1.3107   0.08418   0.07885   0.0306   0.0073   1.0000
  17.750   1.2818   0.08717   0.08202   0.0315   0.0073   1.0000
  18.000   1.2672   0.09085   0.08583   0.0316   0.0073   1.0000
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