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BE50 (smoothed) (be50sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: BE50 (smoothed) (be50sm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.49 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-be50sm-il-1000000.txt
Download as CSV file: xf-be50sm-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: BE50 (smoothed)                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.2889   0.08906   0.08752  -0.0278   1.0000   0.0108
  -8.750  -0.2872   0.08542   0.08390  -0.0285   1.0000   0.0109
  -8.500  -0.2934   0.08029   0.07879  -0.0287   1.0000   0.0113
  -8.250  -0.2909   0.07766   0.07618  -0.0283   1.0000   0.0115
  -8.000  -0.2905   0.07524   0.07378  -0.0276   1.0000   0.0116
  -7.750  -0.2945   0.07298   0.07155  -0.0261   1.0000   0.0118
  -7.500  -0.2949   0.07028   0.06888  -0.0260   0.9994   0.0120
  -7.250  -0.2847   0.06602   0.06462  -0.0294   0.9973   0.0123
  -6.000  -0.2036   0.01893   0.01592  -0.1018   0.9857   0.0099
  -5.750  -0.1672   0.01554   0.01199  -0.1051   0.9847   0.0104
  -5.500  -0.1320   0.01422   0.01042  -0.1070   0.9837   0.0107
  -5.250  -0.0996   0.01270   0.00861  -0.1083   0.9810   0.0110
  -5.000  -0.0682   0.01058   0.00615  -0.1095   0.9774   0.0114
  -4.750  -0.0363   0.00971   0.00514  -0.1105   0.9735   0.0120
  -4.500  -0.0056   0.00933   0.00473  -0.1109   0.9678   0.0128
  -4.250   0.0215   0.00898   0.00431  -0.1105   0.9581   0.0138
  -4.000   0.0484   0.00861   0.00386  -0.1100   0.9479   0.0149
  -3.750   0.0760   0.00799   0.00312  -0.1097   0.9388   0.0164
  -3.500   0.1034   0.00768   0.00276  -0.1094   0.9293   0.0187
  -3.250   0.1309   0.00750   0.00254  -0.1091   0.9190   0.0209
  -3.000   0.1587   0.00720   0.00215  -0.1089   0.9084   0.0235
  -2.750   0.1864   0.00702   0.00194  -0.1087   0.8970   0.0275
  -2.500   0.2141   0.00695   0.00181  -0.1084   0.8843   0.0300
  -2.250   0.2422   0.00671   0.00153  -0.1083   0.8705   0.0377
  -2.000   0.2702   0.00657   0.00135  -0.1081   0.8556   0.0480
  -1.750   0.2983   0.00646   0.00123  -0.1080   0.8396   0.0645
  -1.500   0.3263   0.00635   0.00113  -0.1079   0.8219   0.0898
  -1.250   0.3542   0.00628   0.00106  -0.1078   0.8029   0.1194
  -1.000   0.3822   0.00621   0.00101  -0.1077   0.7833   0.1545
  -0.750   0.4102   0.00611   0.00098  -0.1077   0.7621   0.2086
  -0.500   0.4383   0.00594   0.00097  -0.1079   0.7407   0.3029
  -0.250   0.4663   0.00584   0.00100  -0.1079   0.7178   0.3889
   0.000   0.4941   0.00582   0.00104  -0.1079   0.6944   0.4536
   0.250   0.5219   0.00583   0.00107  -0.1078   0.6702   0.5061
   0.500   0.5496   0.00581   0.00112  -0.1078   0.6448   0.5739
   0.750   0.5724   0.00513   0.00122  -0.1067   0.6205   0.8906
   1.000   0.5978   0.00514   0.00120  -0.1059   0.5941   1.0000
   1.250   0.6253   0.00533   0.00125  -0.1057   0.5653   1.0000
   1.500   0.6528   0.00554   0.00131  -0.1056   0.5345   1.0000
   1.750   0.6801   0.00578   0.00138  -0.1055   0.5012   1.0000
   2.000   0.7073   0.00602   0.00147  -0.1053   0.4676   1.0000
   2.250   0.7344   0.00628   0.00157  -0.1052   0.4349   1.0000
   2.500   0.7616   0.00652   0.00168  -0.1051   0.4077   1.0000
   2.750   0.7889   0.00675   0.00179  -0.1049   0.3855   1.0000
   3.000   0.8162   0.00696   0.00192  -0.1048   0.3661   1.0000
   3.250   0.8436   0.00715   0.00204  -0.1047   0.3500   1.0000
   3.500   0.8709   0.00735   0.00217  -0.1046   0.3352   1.0000
   3.750   0.8982   0.00753   0.00231  -0.1045   0.3219   1.0000
   4.000   0.9255   0.00772   0.00246  -0.1044   0.3097   1.0000
   4.250   0.9527   0.00791   0.00261  -0.1043   0.2979   1.0000
   4.500   0.9798   0.00811   0.00277  -0.1041   0.2866   1.0000
   4.750   1.0069   0.00831   0.00293  -0.1040   0.2753   1.0000
   5.000   1.0339   0.00851   0.00311  -0.1038   0.2634   1.0000
   5.250   1.0602   0.00879   0.00330  -0.1036   0.2424   1.0000
   5.500   1.0865   0.00907   0.00350  -0.1034   0.2226   1.0000
   5.750   1.1128   0.00934   0.00372  -0.1031   0.2079   1.0000
   6.000   1.1388   0.00966   0.00397  -0.1029   0.1902   1.0000
   6.250   1.1646   0.00998   0.00423  -0.1026   0.1723   1.0000
   6.500   1.1897   0.01040   0.00455  -0.1022   0.1504   1.0000
   6.750   1.2140   0.01091   0.00493  -0.1017   0.1236   1.0000
   7.000   1.2368   0.01165   0.00545  -0.1010   0.0864   1.0000
   7.250   1.2570   0.01276   0.00625  -0.1000   0.0393   1.0000
   7.500   1.2793   0.01356   0.00695  -0.0992   0.0210   1.0000
   7.750   1.3029   0.01413   0.00751  -0.0985   0.0166   1.0000
   8.000   1.3265   0.01469   0.00812  -0.0978   0.0141   1.0000
   8.250   1.3505   0.01515   0.00863  -0.0972   0.0128   1.0000
   8.500   1.3735   0.01573   0.00925  -0.0965   0.0115   1.0000
   8.750   1.3933   0.01676   0.01041  -0.0952   0.0100   1.0000
   9.000   1.4167   0.01720   0.01090  -0.0945   0.0095   1.0000
   9.250   1.4392   0.01774   0.01148  -0.0938   0.0088   1.0000
   9.500   1.4611   0.01830   0.01208  -0.0930   0.0081   1.0000
   9.750   1.4808   0.01911   0.01295  -0.0918   0.0073   1.0000
  10.000   1.4944   0.02058   0.01459  -0.0897   0.0066   1.0000
  10.250   1.5146   0.02121   0.01529  -0.0886   0.0063   1.0000
  10.500   1.5329   0.02200   0.01616  -0.0873   0.0060   1.0000
  10.750   1.5495   0.02289   0.01714  -0.0857   0.0057   1.0000
  11.000   1.5651   0.02382   0.01816  -0.0840   0.0054   1.0000
  11.250   1.5792   0.02480   0.01921  -0.0822   0.0051   1.0000
  11.500   1.5916   0.02583   0.02034  -0.0801   0.0049   1.0000
  11.750   1.5990   0.02700   0.02159  -0.0773   0.0047   1.0000
  12.000   1.5994   0.02849   0.02319  -0.0736   0.0046   1.0000
  12.250   1.5947   0.03048   0.02533  -0.0696   0.0044   1.0000
  12.500   1.5831   0.03324   0.02829  -0.0656   0.0043   1.0000
  13.000   1.5645   0.03933   0.03472  -0.0604   0.0042   1.0000
  13.250   1.5658   0.04165   0.03717  -0.0592   0.0041   1.0000
  13.500   1.5643   0.04444   0.04009  -0.0584   0.0041   1.0000
  13.750   1.5610   0.04767   0.04346  -0.0580   0.0040   1.0000
  14.000   1.5564   0.05127   0.04720  -0.0581   0.0040   1.0000
  14.250   1.5485   0.05557   0.05165  -0.0587   0.0039   1.0000
  14.500   1.5388   0.06034   0.05657  -0.0597   0.0039   1.0000
  14.750   1.5295   0.06533   0.06171  -0.0612   0.0038   1.0000
  15.000   1.5160   0.07117   0.06770  -0.0632   0.0038   1.0000
  15.250   1.5022   0.07728   0.07395  -0.0656   0.0038   1.0000
  15.500   1.4848   0.08421   0.08104  -0.0684   0.0038   1.0000
  15.750   1.4695   0.09105   0.08802  -0.0714   0.0038   1.0000
  16.000   1.4515   0.09844   0.09555  -0.0746   0.0038   1.0000
  16.250   1.4346   0.10585   0.10309  -0.0780   0.0038   1.0000
  16.500   1.4177   0.11342   0.11079  -0.0816   0.0038   1.0000
  16.750   1.3994   0.12135   0.11885  -0.0854   0.0038   1.0000
  17.000   1.3820   0.12936   0.12698  -0.0895   0.0038   1.0000
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