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BE50 (smoothed) (be50sm-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: BE50 (smoothed) (be50sm-il)
Reynolds number: 100,000
Max Cl/Cd: 59.21 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-be50sm-il-100000-n5.txt
Download as CSV file: xf-be50sm-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -7.500  -0.3575   0.09328   0.08843  -0.0230   1.0000   0.0481
  -7.250  -0.3597   0.09100   0.08624  -0.0237   1.0000   0.0503
  -7.000  -0.3611   0.08876   0.08410  -0.0294   1.0000   0.0524
  -6.750  -0.3552   0.08558   0.08098  -0.0351   1.0000   0.0529
  -6.500  -0.3465   0.08187   0.07729  -0.0394   1.0000   0.0530
  -6.250  -0.3368   0.07790   0.07333  -0.0425   1.0000   0.0531
  -6.000  -0.3267   0.07387   0.06929  -0.0446   1.0000   0.0531
  -5.500  -0.3084   0.06075   0.05612  -0.0468   1.0000   0.0298
  -5.250  -0.2945   0.05678   0.05211  -0.0491   1.0000   0.0292
  -5.000  -0.2745   0.05207   0.04730  -0.0530   1.0000   0.0287
  -4.750  -0.2483   0.04651   0.04155  -0.0583   1.0000   0.0283
  -4.500  -0.2160   0.04033   0.03499  -0.0642   1.0000   0.0280
  -4.250  -0.1711   0.03348   0.02747  -0.0718   0.9983   0.0283
  -4.000  -0.1247   0.02825   0.02135  -0.0779   0.9959   0.0310
  -3.750  -0.0853   0.02575   0.01844  -0.0814   0.9926   0.0330
  -3.500  -0.0454   0.02331   0.01548  -0.0843   0.9891   0.0349
  -3.250  -0.0055   0.02149   0.01315  -0.0869   0.9855   0.0388
  -3.000   0.0337   0.01998   0.01134  -0.0894   0.9821   0.0435
  -2.750   0.0701   0.01888   0.01007  -0.0911   0.9766   0.0480
  -2.500   0.1089   0.01799   0.00906  -0.0934   0.9719   0.0565
  -2.250   0.1464   0.01721   0.00817  -0.0953   0.9663   0.0651
  -2.000   0.1841   0.01659   0.00753  -0.0974   0.9597   0.0813
  -1.750   0.2242   0.01596   0.00694  -0.0999   0.9524   0.1070
  -1.500   0.2657   0.01528   0.00643  -0.1026   0.9433   0.1541
  -1.250   0.3021   0.01461   0.00604  -0.1042   0.9314   0.2391
  -1.000   0.3367   0.01397   0.00588  -0.1055   0.9199   0.3963
  -0.750   0.3694   0.01347   0.00571  -0.1061   0.9088   0.5300
  -0.500   0.3955   0.01259   0.00548  -0.1049   0.8974   0.7329
  -0.250   0.4242   0.01219   0.00516  -0.1042   0.8825   1.0000
   0.000   0.4554   0.01216   0.00495  -0.1044   0.8677   1.0000
   0.250   0.4858   0.01215   0.00478  -0.1045   0.8517   1.0000
   0.500   0.5158   0.01214   0.00463  -0.1045   0.8347   1.0000
   0.750   0.5456   0.01214   0.00450  -0.1043   0.8168   1.0000
   1.000   0.5743   0.01217   0.00440  -0.1040   0.7970   1.0000
   1.250   0.6027   0.01222   0.00433  -0.1036   0.7756   1.0000
   1.500   0.6307   0.01230   0.00429  -0.1031   0.7524   1.0000
   1.750   0.6584   0.01241   0.00426  -0.1026   0.7281   1.0000
   2.000   0.6855   0.01255   0.00429  -0.1020   0.7015   1.0000
   2.250   0.7121   0.01274   0.00434  -0.1014   0.6734   1.0000
   2.500   0.7384   0.01296   0.00442  -0.1007   0.6436   1.0000
   2.750   0.7644   0.01322   0.00454  -0.1000   0.6126   1.0000
   3.000   0.7900   0.01352   0.00472  -0.0993   0.5806   1.0000
   3.250   0.8154   0.01385   0.00491  -0.0986   0.5487   1.0000
   3.500   0.8405   0.01422   0.00513  -0.0979   0.5177   1.0000
   3.750   0.8655   0.01462   0.00540  -0.0972   0.4883   1.0000
   4.000   0.8905   0.01504   0.00570  -0.0965   0.4615   1.0000
   4.250   0.9154   0.01548   0.00609  -0.0959   0.4375   1.0000
   4.500   0.9402   0.01594   0.00646  -0.0953   0.4168   1.0000
   4.750   0.9652   0.01640   0.00688  -0.0948   0.3977   1.0000
   5.000   0.9901   0.01687   0.00733  -0.0942   0.3807   1.0000
   5.250   1.0149   0.01735   0.00785  -0.0937   0.3649   1.0000
   5.500   1.0397   0.01785   0.00836  -0.0931   0.3504   1.0000
   5.750   1.0644   0.01835   0.00890  -0.0926   0.3364   1.0000
   6.000   1.0890   0.01886   0.00947  -0.0920   0.3231   1.0000
   6.250   1.1133   0.01939   0.01010  -0.0914   0.3099   1.0000
   6.500   1.1374   0.01992   0.01073  -0.0908   0.2969   1.0000
   6.750   1.1612   0.02047   0.01137  -0.0901   0.2835   1.0000
   7.000   1.1843   0.02099   0.01200  -0.0893   0.2671   1.0000
   7.250   1.2058   0.02149   0.01253  -0.0884   0.2426   1.0000
   7.500   1.2268   0.02204   0.01313  -0.0875   0.2119   1.0000
   7.750   1.2475   0.02272   0.01381  -0.0866   0.1817   1.0000
   8.000   1.2667   0.02364   0.01464  -0.0855   0.1430   1.0000
   8.250   1.2820   0.02516   0.01586  -0.0841   0.0911   1.0000
   8.500   1.2940   0.02717   0.01759  -0.0822   0.0562   1.0000
   8.750   1.3067   0.02898   0.01943  -0.0803   0.0442   1.0000
   9.000   1.3175   0.03083   0.02135  -0.0781   0.0378   1.0000
   9.250   1.3293   0.03240   0.02316  -0.0761   0.0329   1.0000
   9.500   1.3354   0.03441   0.02528  -0.0736   0.0299   1.0000
   9.750   1.3418   0.03625   0.02733  -0.0710   0.0283   1.0000
  10.000   1.3467   0.03809   0.02939  -0.0682   0.0269   1.0000
  10.250   1.3491   0.04002   0.03149  -0.0653   0.0257   1.0000
  10.500   1.3513   0.04204   0.03367  -0.0627   0.0243   1.0000
  10.750   1.3522   0.04421   0.03596  -0.0604   0.0230   1.0000
  11.000   1.3499   0.04685   0.03869  -0.0582   0.0218   1.0000
  11.250   1.3496   0.04964   0.04162  -0.0563   0.0208   1.0000
  11.500   1.3514   0.05233   0.04455  -0.0546   0.0203   1.0000
  11.750   1.3518   0.05531   0.04777  -0.0532   0.0197   1.0000
  12.000   1.3505   0.05857   0.05132  -0.0520   0.0193   1.0000
  12.250   1.3473   0.06213   0.05514  -0.0512   0.0189   1.0000
  12.500   1.3417   0.06608   0.05935  -0.0508   0.0186   1.0000
  12.750   1.3339   0.07040   0.06392  -0.0509   0.0183   1.0000
  13.000   1.3241   0.07514   0.06891  -0.0517   0.0180   1.0000
  13.250   1.3124   0.08035   0.07437  -0.0531   0.0178   1.0000
  13.500   1.2991   0.08608   0.08032  -0.0553   0.0176   1.0000
  13.750   1.2841   0.09238   0.08686  -0.0582   0.0175   1.0000
  14.000   1.2676   0.09936   0.09406  -0.0618   0.0175   1.0000
  14.250   1.2494   0.10710   0.10203  -0.0662   0.0176   1.0000
  14.500   1.2296   0.11578   0.11092  -0.0715   0.0178   1.0000
  14.750   1.2085   0.12545   0.12079  -0.0777   0.0181   1.0000
  15.000   1.1863   0.13610   0.13160  -0.0847   0.0185   1.0000
  15.250   1.1634   0.14784   0.14343  -0.0923   0.0190   1.0000
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