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BE50 (smoothed) (be50sm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: BE50 (smoothed) (be50sm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.87 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-be50sm-il-1000000-n5.txt
Download as CSV file: xf-be50sm-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.4105   0.10635   0.10468  -0.0144   1.0000   0.0054
  -9.250  -0.4049   0.10295   0.10129  -0.0159   1.0000   0.0054
  -8.250  -0.4536   0.02013   0.01721  -0.0988   0.9888   0.0054
  -8.000  -0.4223   0.01817   0.01499  -0.1010   0.9866   0.0056
  -7.750  -0.3907   0.01665   0.01325  -0.1029   0.9846   0.0058
  -7.500  -0.3592   0.01538   0.01177  -0.1044   0.9824   0.0060
  -7.250  -0.3305   0.01433   0.01052  -0.1051   0.9781   0.0062
  -7.000  -0.3006   0.01334   0.00934  -0.1060   0.9744   0.0065
  -6.750  -0.2700   0.01249   0.00833  -0.1069   0.9711   0.0067
  -6.500  -0.2409   0.01175   0.00744  -0.1073   0.9668   0.0069
  -6.250  -0.2123   0.01112   0.00667  -0.1076   0.9614   0.0071
  -6.000  -0.1833   0.01057   0.00600  -0.1079   0.9564   0.0072
  -5.750  -0.1553   0.01009   0.00540  -0.1079   0.9501   0.0074
  -5.500  -0.1272   0.00965   0.00487  -0.1079   0.9436   0.0075
  -5.250  -0.0990   0.00905   0.00415  -0.1080   0.9367   0.0080
  -5.000  -0.0712   0.00875   0.00379  -0.1079   0.9289   0.0087
  -4.750  -0.0434   0.00851   0.00350  -0.1078   0.9194   0.0094
  -4.500  -0.0161   0.00827   0.00318  -0.1075   0.9054   0.0101
  -4.250   0.0108   0.00809   0.00287  -0.1070   0.8854   0.0107
  -4.000   0.0381   0.00786   0.00252  -0.1067   0.8622   0.0120
  -3.750   0.0657   0.00773   0.00230  -0.1065   0.8414   0.0133
  -3.500   0.0936   0.00763   0.00210  -0.1064   0.8226   0.0147
  -3.250   0.1215   0.00753   0.00190  -0.1062   0.8032   0.0160
  -3.000   0.1496   0.00743   0.00172  -0.1062   0.7836   0.0186
  -2.750   0.1777   0.00738   0.00159  -0.1061   0.7637   0.0210
  -2.500   0.2058   0.00733   0.00144  -0.1060   0.7432   0.0242
  -2.250   0.2339   0.00728   0.00133  -0.1060   0.7218   0.0288
  -2.000   0.2620   0.00726   0.00123  -0.1059   0.7007   0.0344
  -1.750   0.2902   0.00725   0.00115  -0.1059   0.6795   0.0410
  -1.500   0.3183   0.00724   0.00108  -0.1059   0.6576   0.0529
  -1.250   0.3464   0.00724   0.00103  -0.1059   0.6347   0.0670
  -1.000   0.3745   0.00725   0.00100  -0.1059   0.6121   0.0837
  -0.750   0.4026   0.00726   0.00097  -0.1059   0.5888   0.1067
  -0.500   0.4307   0.00725   0.00097  -0.1060   0.5651   0.1390
  -0.250   0.4586   0.00728   0.00098  -0.1060   0.5396   0.1716
   0.000   0.4866   0.00729   0.00100  -0.1061   0.5114   0.2195
   0.250   0.5144   0.00730   0.00104  -0.1062   0.4825   0.2804
   0.500   0.5422   0.00731   0.00112  -0.1063   0.4528   0.3539
   0.750   0.5700   0.00738   0.00120  -0.1063   0.4263   0.4082
   1.000   0.5976   0.00748   0.00128  -0.1063   0.4020   0.4472
   1.250   0.6254   0.00756   0.00136  -0.1063   0.3813   0.4857
   1.500   0.6532   0.00761   0.00145  -0.1063   0.3640   0.5311
   1.750   0.6810   0.00762   0.00155  -0.1063   0.3486   0.5961
   2.000   0.7020   0.00688   0.00165  -0.1047   0.3365   1.0000
   2.250   0.7297   0.00704   0.00173  -0.1047   0.3238   1.0000
   2.500   0.7575   0.00719   0.00182  -0.1046   0.3122   1.0000
   2.750   0.7851   0.00735   0.00192  -0.1045   0.3016   1.0000
   3.000   0.8128   0.00750   0.00203  -0.1045   0.2907   1.0000
   3.250   0.8404   0.00765   0.00214  -0.1044   0.2817   1.0000
   3.500   0.8679   0.00781   0.00226  -0.1043   0.2720   1.0000
   3.750   0.8953   0.00798   0.00238  -0.1042   0.2623   1.0000
   4.000   0.9228   0.00813   0.00253  -0.1041   0.2538   1.0000
   4.250   0.9500   0.00832   0.00267  -0.1040   0.2444   1.0000
   4.500   0.9772   0.00850   0.00282  -0.1039   0.2350   1.0000
   4.750   1.0043   0.00868   0.00298  -0.1037   0.2260   1.0000
   5.000   1.0312   0.00890   0.00318  -0.1036   0.2145   1.0000
   5.250   1.0568   0.00929   0.00341  -0.1033   0.1857   1.0000
   5.500   1.0820   0.00973   0.00369  -0.1029   0.1557   1.0000
   5.750   1.1077   0.01010   0.00397  -0.1026   0.1367   1.0000
   6.000   1.1326   0.01057   0.00432  -0.1022   0.1118   1.0000
   6.250   1.1570   0.01111   0.00472  -0.1017   0.0852   1.0000
   6.500   1.1808   0.01172   0.00518  -0.1012   0.0584   1.0000
   6.750   1.2046   0.01233   0.00567  -0.1006   0.0366   1.0000
   7.000   1.2288   0.01285   0.00613  -0.1001   0.0246   1.0000
   7.250   1.2533   0.01330   0.00657  -0.0996   0.0181   1.0000
   7.500   1.2778   0.01374   0.00700  -0.0991   0.0141   1.0000
   7.750   1.3023   0.01416   0.00743  -0.0986   0.0119   1.0000
   8.000   1.3264   0.01463   0.00792  -0.0980   0.0099   1.0000
   8.250   1.3507   0.01503   0.00835  -0.0975   0.0091   1.0000
   8.500   1.3746   0.01547   0.00884  -0.0969   0.0083   1.0000
   8.750   1.3978   0.01598   0.00937  -0.0963   0.0075   1.0000
   9.000   1.4202   0.01658   0.01002  -0.0955   0.0067   1.0000
   9.250   1.4434   0.01703   0.01052  -0.0948   0.0064   1.0000
   9.500   1.4661   0.01752   0.01107  -0.0941   0.0059   1.0000
   9.750   1.4884   0.01804   0.01163  -0.0934   0.0054   1.0000
  10.000   1.5099   0.01861   0.01225  -0.0925   0.0049   1.0000
  10.250   1.5301   0.01930   0.01300  -0.0915   0.0044   1.0000
  10.500   1.5497   0.02003   0.01380  -0.0903   0.0041   1.0000
  10.750   1.5697   0.02065   0.01450  -0.0892   0.0040   1.0000
  11.000   1.5888   0.02134   0.01525  -0.0881   0.0038   1.0000
  11.250   1.6070   0.02207   0.01606  -0.0867   0.0035   1.0000
  11.500   1.6242   0.02283   0.01690  -0.0853   0.0033   1.0000
  11.750   1.6403   0.02363   0.01780  -0.0838   0.0032   1.0000
  12.000   1.6550   0.02449   0.01873  -0.0820   0.0030   1.0000
  12.250   1.6678   0.02540   0.01972  -0.0800   0.0029   1.0000
  12.500   1.6761   0.02639   0.02079  -0.0773   0.0027   1.0000
  12.750   1.6812   0.02757   0.02207  -0.0742   0.0026   1.0000
  13.000   1.6832   0.02903   0.02365  -0.0710   0.0025   1.0000
  13.250   1.6818   0.03085   0.02561  -0.0679   0.0024   1.0000
  13.500   1.6850   0.03243   0.02730  -0.0656   0.0024   1.0000
  13.750   1.6869   0.03424   0.02924  -0.0635   0.0023   1.0000
  14.000   1.6877   0.03629   0.03140  -0.0617   0.0023   1.0000
  14.250   1.6867   0.03869   0.03393  -0.0603   0.0023   1.0000
  14.500   1.6843   0.04142   0.03679  -0.0592   0.0023   1.0000
  14.750   1.6811   0.04445   0.03996  -0.0586   0.0022   1.0000
  15.000   1.6752   0.04808   0.04374  -0.0585   0.0022   1.0000
  15.250   1.6675   0.05219   0.04799  -0.0589   0.0022   1.0000
  15.500   1.6562   0.05713   0.05309  -0.0600   0.0022   1.0000
  15.750   1.6444   0.06242   0.05852  -0.0616   0.0021   1.0000
  16.000   1.6284   0.06864   0.06490  -0.0638   0.0021   1.0000
  16.250   1.6112   0.07536   0.07176  -0.0664   0.0021   1.0000
  16.500   1.5921   0.08257   0.07912  -0.0694   0.0021   1.0000
  16.750   1.5697   0.09058   0.08729  -0.0728   0.0021   1.0000
  17.000   1.5460   0.09890   0.09575  -0.0763   0.0021   1.0000
  17.250   1.5218   0.10739   0.10438  -0.0800   0.0021   1.0000
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