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BE50 (smoothed) (be50sm-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: BE50 (smoothed) (be50sm-il)
Reynolds number: 200,000
Max Cl/Cd: 74.36 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-be50sm-il-200000-n5.txt
Download as CSV file: xf-be50sm-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3721   0.09684   0.09328  -0.0225   1.0000   0.0228
  -8.000  -0.3681   0.09376   0.09024  -0.0234   1.0000   0.0229
  -7.750  -0.3662   0.09073   0.08726  -0.0243   1.0000   0.0229
  -7.500  -0.2865   0.07504   0.07184  -0.0273   1.0000   0.0199
  -7.250  -0.2916   0.07222   0.06908  -0.0262   1.0000   0.0192
  -7.000  -0.3647   0.08253   0.07920  -0.0242   1.0000   0.0196
  -6.750  -0.3647   0.07944   0.07616  -0.0250   1.0000   0.0185
  -6.500  -0.3649   0.07580   0.07257  -0.0267   1.0000   0.0175
  -6.000  -0.3359   0.06231   0.05904  -0.0421   0.9970   0.0153
  -5.500  -0.2633   0.05031   0.04686  -0.0616   0.9885   0.0166
  -5.250  -0.2217   0.04454   0.04090  -0.0709   0.9850   0.0179
  -5.000  -0.1659   0.03073   0.02629  -0.0860   0.9825   0.0172
  -4.750  -0.1243   0.02342   0.01801  -0.0920   0.9792   0.0174
  -4.500  -0.0870   0.02027   0.01423  -0.0949   0.9759   0.0183
  -4.250  -0.0498   0.01809   0.01154  -0.0972   0.9731   0.0195
  -4.000  -0.0123   0.01669   0.00977  -0.0993   0.9707   0.0214
  -3.750   0.0216   0.01567   0.00863  -0.1008   0.9665   0.0242
  -3.500   0.0559   0.01478   0.00759  -0.1022   0.9619   0.0267
  -3.250   0.0918   0.01400   0.00664  -0.1037   0.9581   0.0297
  -3.000   0.1256   0.01331   0.00593  -0.1050   0.9530   0.0347
  -2.750   0.1592   0.01274   0.00527  -0.1060   0.9457   0.0392
  -2.500   0.1932   0.01218   0.00468  -0.1071   0.9355   0.0470
  -2.250   0.2268   0.01169   0.00414  -0.1080   0.9231   0.0562
  -2.000   0.2587   0.01130   0.00376  -0.1086   0.9110   0.0723
  -1.750   0.2896   0.01097   0.00346  -0.1090   0.8998   0.0963
  -1.500   0.3191   0.01066   0.00323  -0.1091   0.8869   0.1334
  -1.250   0.3482   0.01036   0.00305  -0.1092   0.8730   0.1827
  -1.000   0.3770   0.01001   0.00291  -0.1093   0.8583   0.2620
  -0.750   0.4051   0.00967   0.00286  -0.1093   0.8422   0.3743
  -0.500   0.4325   0.00944   0.00281  -0.1089   0.8244   0.4635
  -0.250   0.4593   0.00924   0.00274  -0.1084   0.8054   0.5399
   0.000   0.4844   0.00889   0.00268  -0.1075   0.7860   0.6548
   0.500   0.5325   0.00841   0.00244  -0.1046   0.7422   1.0000
   0.750   0.5596   0.00855   0.00241  -0.1041   0.7181   1.0000
   1.000   0.5865   0.00871   0.00240  -0.1037   0.6929   1.0000
   1.250   0.6133   0.00890   0.00241  -0.1032   0.6668   1.0000
   1.500   0.6398   0.00911   0.00245  -0.1028   0.6391   1.0000
   1.750   0.6663   0.00934   0.00251  -0.1023   0.6105   1.0000
   2.000   0.6925   0.00960   0.00260  -0.1018   0.5806   1.0000
   2.250   0.7186   0.00987   0.00270  -0.1013   0.5496   1.0000
   2.500   0.7444   0.01017   0.00283  -0.1009   0.5180   1.0000
   2.750   0.7702   0.01049   0.00298  -0.1004   0.4869   1.0000
   3.000   0.7959   0.01082   0.00318  -0.1000   0.4577   1.0000
   3.250   0.8217   0.01116   0.00339  -0.0996   0.4313   1.0000
   3.500   0.8475   0.01149   0.00361  -0.0992   0.4085   1.0000
   3.750   0.8733   0.01183   0.00385  -0.0988   0.3888   1.0000
   4.000   0.8992   0.01216   0.00414  -0.0984   0.3715   1.0000
   4.250   0.9251   0.01249   0.00443  -0.0981   0.3559   1.0000
   4.500   0.9509   0.01282   0.00472  -0.0977   0.3417   1.0000
   4.750   0.9767   0.01315   0.00504  -0.0974   0.3284   1.0000
   5.000   1.0024   0.01350   0.00537  -0.0970   0.3160   1.0000
   5.250   1.0281   0.01383   0.00574  -0.0966   0.3037   1.0000
   5.500   1.0537   0.01417   0.00610  -0.0962   0.2919   1.0000
   5.750   1.0792   0.01452   0.00649  -0.0958   0.2802   1.0000
   6.000   1.1044   0.01488   0.00689  -0.0954   0.2687   1.0000
   6.250   1.1294   0.01526   0.00733  -0.0949   0.2559   1.0000
   6.500   1.1534   0.01570   0.00772  -0.0944   0.2334   1.0000
   6.750   1.1770   0.01619   0.00813  -0.0938   0.2055   1.0000
   7.000   1.2004   0.01672   0.00861  -0.0932   0.1799   1.0000
   7.250   1.2227   0.01739   0.00917  -0.0925   0.1502   1.0000
   7.500   1.2438   0.01823   0.00989  -0.0917   0.1140   1.0000
   7.750   1.2623   0.01943   0.01084  -0.0906   0.0718   1.0000
   8.000   1.2793   0.02084   0.01204  -0.0892   0.0407   1.0000
   8.250   1.2974   0.02203   0.01321  -0.0879   0.0293   1.0000
   8.500   1.3168   0.02300   0.01431  -0.0866   0.0248   1.0000
   8.750   1.3330   0.02431   0.01573  -0.0850   0.0215   1.0000
   9.000   1.3502   0.02539   0.01700  -0.0835   0.0197   1.0000
   9.250   1.3666   0.02647   0.01823  -0.0820   0.0177   1.0000
   9.500   1.3808   0.02770   0.01958  -0.0802   0.0161   1.0000
   9.750   1.3890   0.02943   0.02143  -0.0777   0.0150   1.0000
  10.000   1.3968   0.03108   0.02323  -0.0752   0.0143   1.0000
  10.250   1.4049   0.03253   0.02485  -0.0726   0.0137   1.0000
  10.500   1.4106   0.03400   0.02648  -0.0698   0.0130   1.0000
  10.750   1.4157   0.03555   0.02817  -0.0673   0.0122   1.0000
  11.000   1.4201   0.03719   0.02997  -0.0649   0.0114   1.0000
  11.250   1.4226   0.03906   0.03197  -0.0628   0.0109   1.0000
  11.500   1.4219   0.04136   0.03439  -0.0606   0.0105   1.0000
  11.750   1.4181   0.04418   0.03734  -0.0587   0.0102   1.0000
  12.000   1.4133   0.04734   0.04065  -0.0570   0.0099   1.0000
  12.250   1.4123   0.05021   0.04372  -0.0558   0.0098   1.0000
  12.500   1.4097   0.05339   0.04711  -0.0550   0.0096   1.0000
  12.750   1.4058   0.05690   0.05083  -0.0545   0.0094   1.0000
  13.000   1.4003   0.06076   0.05490  -0.0545   0.0092   1.0000
  13.250   1.3933   0.06500   0.05936  -0.0548   0.0091   1.0000
  13.500   1.3849   0.06963   0.06420  -0.0556   0.0090   1.0000
  13.750   1.3747   0.07470   0.06949  -0.0570   0.0089   1.0000
  14.000   1.3634   0.08018   0.07518  -0.0588   0.0088   1.0000
  14.250   1.3508   0.08609   0.08130  -0.0611   0.0087   1.0000
  14.500   1.3371   0.09247   0.08788  -0.0639   0.0087   1.0000
  14.750   1.3224   0.09935   0.09496  -0.0673   0.0087   1.0000
  15.000   1.3073   0.10661   0.10241  -0.0711   0.0087   1.0000
  15.250   1.2914   0.11434   0.11033  -0.0753   0.0087   1.0000
  15.500   1.2753   0.12247   0.11863  -0.0800   0.0087   1.0000
  15.750   1.2589   0.13104   0.12737  -0.0851   0.0087   1.0000
  16.000   1.2420   0.14012   0.13661  -0.0906   0.0088   1.0000
  16.250   1.2247   0.14979   0.14643  -0.0967   0.0089   1.0000
  16.500   1.2069   0.16032   0.15710  -0.1034   0.0090   1.0000
  16.750   1.1878   0.17209   0.16899  -0.1108   0.0092   1.0000
  17.000   1.1648   0.18653   0.18351  -0.1196   0.0094   1.0000
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