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BE50 (smoothed) (be50sm-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: BE50 (smoothed) (be50sm-il)
Reynolds number: 500,000
Max Cl/Cd: 104.87 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-be50sm-il-500000.txt
Download as CSV file: xf-be50sm-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.250  -0.3655   0.08462   0.08249  -0.0219   1.0000   0.0185
  -7.000  -0.3693   0.08232   0.08025  -0.0213   1.0000   0.0189
  -6.750  -0.3732   0.07998   0.07795  -0.0210   1.0000   0.0192
  -6.500  -0.3764   0.07752   0.07553  -0.0210   1.0000   0.0196
  -6.250  -0.3599   0.07295   0.07096  -0.0277   0.9985   0.0206
  -6.000  -0.3132   0.06610   0.06405  -0.0425   0.9954   0.0215
  -5.750  -0.2727   0.05923   0.05710  -0.0541   0.9924   0.0217
  -5.500  -0.2313   0.04683   0.04453  -0.0707   0.9884   0.0224
  -5.250  -0.1975   0.04313   0.04074  -0.0763   0.9861   0.0233
  -5.000  -0.1582   0.03904   0.03652  -0.0828   0.9844   0.0247
  -4.750  -0.0993   0.02356   0.02000  -0.0965   0.9832   0.0198
  -4.500  -0.0608   0.01813   0.01382  -0.1003   0.9806   0.0193
  -4.250  -0.0243   0.01556   0.01078  -0.1024   0.9778   0.0198
  -4.000   0.0135   0.01353   0.00836  -0.1045   0.9756   0.0204
  -3.750   0.0538   0.01249   0.00712  -0.1069   0.9733   0.0216
  -3.500   0.0950   0.01073   0.00516  -0.1097   0.9707   0.0246
  -3.250   0.1282   0.01029   0.00468  -0.1106   0.9633   0.0281
  -3.000   0.1621   0.00959   0.00390  -0.1117   0.9577   0.0322
  -2.750   0.1919   0.00917   0.00346  -0.1118   0.9499   0.0369
  -2.500   0.2220   0.00882   0.00305  -0.1120   0.9425   0.0421
  -2.250   0.2499   0.00843   0.00265  -0.1117   0.9322   0.0508
  -2.000   0.2779   0.00813   0.00234  -0.1114   0.9220   0.0652
  -1.750   0.3057   0.00782   0.00210  -0.1112   0.9112   0.0923
  -1.500   0.3331   0.00757   0.00193  -0.1108   0.8991   0.1318
  -1.250   0.3604   0.00732   0.00181  -0.1106   0.8857   0.1882
  -1.000   0.3879   0.00701   0.00174  -0.1104   0.8713   0.2812
  -0.750   0.4152   0.00673   0.00173  -0.1103   0.8553   0.4002
  -0.500   0.4425   0.00657   0.00171  -0.1100   0.8380   0.4802
   0.000   0.4954   0.00600   0.00170  -0.1091   0.8002   0.7209
   0.250   0.5157   0.00551   0.00160  -0.1068   0.7794   1.0000
   0.500   0.5430   0.00564   0.00157  -0.1064   0.7574   1.0000
   0.750   0.5704   0.00578   0.00157  -0.1061   0.7336   1.0000
   1.000   0.5976   0.00593   0.00158  -0.1058   0.7092   1.0000
   1.250   0.6247   0.00611   0.00160  -0.1055   0.6834   1.0000
   1.500   0.6517   0.00630   0.00164  -0.1052   0.6564   1.0000
   1.750   0.6786   0.00651   0.00170  -0.1048   0.6273   1.0000
   2.000   0.7054   0.00673   0.00178  -0.1045   0.5966   1.0000
   2.250   0.7320   0.00698   0.00187  -0.1042   0.5639   1.0000
   2.500   0.7584   0.00726   0.00198  -0.1039   0.5288   1.0000
   2.750   0.7848   0.00756   0.00211  -0.1036   0.4925   1.0000
   3.000   0.8109   0.00788   0.00227  -0.1032   0.4576   1.0000
   3.250   0.8372   0.00820   0.00244  -0.1030   0.4274   1.0000
   3.500   0.8635   0.00851   0.00262  -0.1027   0.4023   1.0000
   3.750   0.8901   0.00879   0.00281  -0.1024   0.3811   1.0000
   4.000   0.9167   0.00907   0.00303  -0.1022   0.3634   1.0000
   4.250   0.9432   0.00934   0.00324  -0.1020   0.3475   1.0000
   4.500   0.9697   0.00961   0.00346  -0.1017   0.3333   1.0000
   4.750   0.9962   0.00986   0.00369  -0.1015   0.3200   1.0000
   5.000   1.0227   0.01012   0.00394  -0.1013   0.3075   1.0000
   5.250   1.0491   0.01038   0.00419  -0.1010   0.2954   1.0000
   5.500   1.0754   0.01065   0.00444  -0.1007   0.2827   1.0000
   5.750   1.1011   0.01095   0.00467  -0.1004   0.2624   1.0000
   6.000   1.1269   0.01126   0.00494  -0.1001   0.2423   1.0000
   6.250   1.1526   0.01157   0.00522  -0.0998   0.2264   1.0000
   6.500   1.1781   0.01191   0.00553  -0.0994   0.2097   1.0000
   6.750   1.2029   0.01232   0.00587  -0.0990   0.1892   1.0000
   7.000   1.2271   0.01281   0.00626  -0.0985   0.1637   1.0000
   7.250   1.2503   0.01343   0.00676  -0.0979   0.1306   1.0000
   7.500   1.2687   0.01474   0.00765  -0.0967   0.0681   1.0000
   7.750   1.2858   0.01629   0.00891  -0.0952   0.0291   1.0000
   8.000   1.3070   0.01717   0.00983  -0.0941   0.0230   1.0000
   8.250   1.3278   0.01808   0.01085  -0.0929   0.0201   1.0000
   8.500   1.3491   0.01882   0.01168  -0.0919   0.0181   1.0000
   8.750   1.3683   0.01980   0.01274  -0.0907   0.0160   1.0000
   9.000   1.3819   0.02139   0.01449  -0.0885   0.0145   1.0000
   9.250   1.4011   0.02223   0.01543  -0.0872   0.0137   1.0000
   9.500   1.4181   0.02326   0.01657  -0.0856   0.0128   1.0000
   9.750   1.4338   0.02436   0.01777  -0.0839   0.0120   1.0000
  10.000   1.4475   0.02557   0.01906  -0.0820   0.0113   1.0000
  10.250   1.4559   0.02724   0.02083  -0.0794   0.0106   1.0000
  10.500   1.4501   0.03038   0.02416  -0.0749   0.0100   1.0000
  10.750   1.4608   0.03127   0.02519  -0.0725   0.0097   1.0000
  11.000   1.4691   0.03243   0.02648  -0.0700   0.0093   1.0000
  11.250   1.4740   0.03400   0.02819  -0.0673   0.0090   1.0000
  11.500   1.4766   0.03588   0.03022  -0.0646   0.0087   1.0000
  11.750   1.4781   0.03795   0.03243  -0.0621   0.0085   1.0000
  12.000   1.4785   0.04022   0.03486  -0.0599   0.0083   1.0000
  12.250   1.4781   0.04264   0.03743  -0.0580   0.0081   1.0000
  12.500   1.4759   0.04538   0.04033  -0.0563   0.0079   1.0000
  12.750   1.4728   0.04833   0.04344  -0.0551   0.0078   1.0000
  13.000   1.4677   0.05169   0.04697  -0.0543   0.0077   1.0000
  13.250   1.4617   0.05533   0.05077  -0.0539   0.0076   1.0000
  13.500   1.4540   0.05937   0.05498  -0.0541   0.0075   1.0000
  13.750   1.4446   0.06389   0.05967  -0.0547   0.0074   1.0000
  14.000   1.4340   0.06880   0.06474  -0.0559   0.0074   1.0000
  14.250   1.4211   0.07430   0.07042  -0.0575   0.0073   1.0000
  14.500   1.4068   0.08032   0.07663  -0.0598   0.0073   1.0000
  14.750   1.3926   0.08657   0.08304  -0.0625   0.0073   1.0000
  15.000   1.3753   0.09376   0.09043  -0.0659   0.0073   1.0000
  15.250   1.3582   0.10130   0.09815  -0.0697   0.0073   1.0000
  15.500   1.3364   0.11014   0.10720  -0.0744   0.0074   1.0000
  15.750   1.3169   0.11888   0.11611  -0.0793   0.0075   1.0000
  16.000   1.2932   0.12907   0.12649  -0.0853   0.0076   1.0000
  16.250   1.2627   0.14175   0.13941  -0.0931   0.0078   1.0000
  16.500   1.2317   0.15568   0.15353  -0.1020   0.0081   1.0000
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