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SG6051 (sg6051-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SG6051 (sg6051-il)
Reynolds number: 500,000
Max Cl/Cd: 102.29 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6051-il-500000-n5.txt
Download as CSV file: xf-sg6051-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6051                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.7780   0.04677   0.04406  -0.0701   1.0000   0.0050
 -11.750  -0.7974   0.04020   0.03719  -0.0759   0.9757   0.0049
 -11.500  -0.8033   0.03599   0.03264  -0.0768   0.9543   0.0050
 -11.250  -0.8035   0.03273   0.02904  -0.0760   0.9394   0.0050
 -11.000  -0.7976   0.03011   0.02611  -0.0750   0.9283   0.0050
 -10.750  -0.7862   0.02791   0.02363  -0.0743   0.9189   0.0051
 -10.500  -0.7713   0.02611   0.02157  -0.0735   0.9114   0.0052
 -10.250  -0.7533   0.02456   0.01980  -0.0730   0.9042   0.0053
 -10.000  -0.7340   0.02323   0.01826  -0.0725   0.8982   0.0054
  -9.750  -0.7124   0.02202   0.01686  -0.0722   0.8919   0.0056
  -9.500  -0.6903   0.02094   0.01559  -0.0719   0.8862   0.0057
  -9.250  -0.6671   0.01995   0.01441  -0.0717   0.8811   0.0059
  -9.000  -0.6430   0.01903   0.01332  -0.0716   0.8758   0.0061
  -8.750  -0.6185   0.01821   0.01233  -0.0714   0.8709   0.0063
  -8.500  -0.5932   0.01745   0.01142  -0.0713   0.8664   0.0065
  -8.250  -0.5673   0.01675   0.01058  -0.0713   0.8616   0.0068
  -8.000  -0.5412   0.01610   0.00979  -0.0713   0.8572   0.0070
  -7.750  -0.5152   0.01544   0.00900  -0.0713   0.8532   0.0075
  -7.500  -0.4882   0.01487   0.00835  -0.0715   0.8486   0.0080
  -7.250  -0.4611   0.01437   0.00775  -0.0716   0.8441   0.0087
  -7.000  -0.4339   0.01391   0.00719  -0.0717   0.8402   0.0096
  -6.750  -0.4065   0.01343   0.00666  -0.0719   0.8364   0.0117
  -6.500  -0.3787   0.01302   0.00623  -0.0721   0.8319   0.0154
  -6.250  -0.3507   0.01272   0.00591  -0.0723   0.8276   0.0197
  -6.000  -0.3227   0.01248   0.00563  -0.0726   0.8239   0.0229
  -5.750  -0.2941   0.01227   0.00536  -0.0729   0.8197   0.0257
  -5.500  -0.2656   0.01202   0.00508  -0.0732   0.8151   0.0282
  -5.250  -0.2372   0.01184   0.00487  -0.0735   0.8110   0.0314
  -5.000  -0.2086   0.01168   0.00466  -0.0738   0.8071   0.0345
  -4.750  -0.1799   0.01145   0.00443  -0.0742   0.8025   0.0383
  -4.500  -0.1511   0.01127   0.00421  -0.0745   0.7982   0.0412
  -4.250  -0.1224   0.01109   0.00395  -0.0748   0.7944   0.0429
  -4.000  -0.0935   0.01081   0.00365  -0.0751   0.7902   0.0466
  -3.750  -0.0646   0.01061   0.00344  -0.0755   0.7856   0.0505
  -3.500  -0.0356   0.01047   0.00324  -0.0758   0.7814   0.0541
  -3.250  -0.0067   0.01027   0.00303  -0.0762   0.7775   0.0611
  -3.000   0.0225   0.01009   0.00287  -0.0766   0.7729   0.0701
  -2.750   0.0515   0.00990   0.00272  -0.0770   0.7684   0.0871
  -2.500   0.0803   0.00969   0.00257  -0.0774   0.7645   0.1137
  -2.250   0.1094   0.00944   0.00244  -0.0779   0.7599   0.1547
  -2.000   0.1381   0.00907   0.00231  -0.0785   0.7551   0.2285
  -1.750   0.1665   0.00863   0.00223  -0.0790   0.7509   0.3453
  -1.500   0.1956   0.00851   0.00220  -0.0794   0.7462   0.3890
  -1.250   0.2248   0.00841   0.00216  -0.0798   0.7411   0.4174
  -1.000   0.2538   0.00832   0.00211  -0.0802   0.7361   0.4449
  -0.750   0.2828   0.00815   0.00209  -0.0807   0.7310   0.4899
  -0.500   0.3112   0.00785   0.00209  -0.0810   0.7256   0.5753
  -0.250   0.3382   0.00745   0.00212  -0.0810   0.7209   0.7057
   0.000   0.3640   0.00717   0.00217  -0.0805   0.7159   0.8025
   0.250   0.3893   0.00705   0.00220  -0.0797   0.7105   0.8611
   0.500   0.4141   0.00699   0.00219  -0.0788   0.7056   0.9076
   0.750   0.4422   0.00693   0.00218  -0.0787   0.6998   0.9458
   1.000   0.4753   0.00693   0.00215  -0.0799   0.6937   0.9760
   1.250   0.5091   0.00695   0.00215  -0.0813   0.6871   0.9949
   1.500   0.5397   0.00698   0.00214  -0.0821   0.6796   1.0000
   1.750   0.5681   0.00704   0.00216  -0.0823   0.6724   1.0000
   2.000   0.5965   0.00712   0.00220  -0.0826   0.6640   1.0000
   2.250   0.6249   0.00719   0.00225  -0.0828   0.6548   1.0000
   2.500   0.6532   0.00728   0.00230  -0.0830   0.6452   1.0000
   2.750   0.6816   0.00738   0.00236  -0.0833   0.6346   1.0000
   3.000   0.7098   0.00748   0.00245  -0.0835   0.6231   1.0000
   3.250   0.7379   0.00760   0.00253  -0.0837   0.6103   1.0000
   3.500   0.7659   0.00773   0.00263  -0.0839   0.5965   1.0000
   3.750   0.7936   0.00788   0.00274  -0.0840   0.5801   1.0000
   4.000   0.8209   0.00808   0.00287  -0.0841   0.5598   1.0000
   4.250   0.8480   0.00829   0.00301  -0.0842   0.5385   1.0000
   4.500   0.8743   0.00857   0.00320  -0.0841   0.5105   1.0000
   4.750   0.8993   0.00896   0.00343  -0.0838   0.4721   1.0000
   5.000   0.9237   0.00942   0.00371  -0.0835   0.4307   1.0000
   5.250   0.9465   0.01002   0.00407  -0.0829   0.3789   1.0000
   5.500   0.9670   0.01083   0.00455  -0.0821   0.3135   1.0000
   5.750   0.9879   0.01158   0.00502  -0.0813   0.2594   1.0000
   6.000   1.0102   0.01216   0.00544  -0.0807   0.2235   1.0000
   6.250   1.0320   0.01276   0.00589  -0.0800   0.1890   1.0000
   6.500   1.0531   0.01339   0.00636  -0.0792   0.1558   1.0000
   6.750   1.0740   0.01401   0.00684  -0.0783   0.1278   1.0000
   7.000   1.0950   0.01458   0.00732  -0.0775   0.1063   1.0000
   7.250   1.1157   0.01515   0.00782  -0.0766   0.0879   1.0000
   7.500   1.1353   0.01576   0.00835  -0.0755   0.0715   1.0000
   7.750   1.1546   0.01636   0.00889  -0.0743   0.0577   1.0000
   8.000   1.1732   0.01697   0.00945  -0.0731   0.0468   1.0000
   8.250   1.1910   0.01758   0.01003  -0.0717   0.0387   1.0000
   8.500   1.2093   0.01812   0.01060  -0.0704   0.0342   1.0000
   8.750   1.2249   0.01873   0.01122  -0.0686   0.0304   1.0000
   9.000   1.2401   0.01930   0.01184  -0.0667   0.0279   1.0000
   9.250   1.2543   0.01999   0.01254  -0.0648   0.0251   1.0000
   9.500   1.2688   0.02071   0.01330  -0.0630   0.0229   1.0000
   9.750   1.2840   0.02141   0.01407  -0.0615   0.0210   1.0000
  10.000   1.2979   0.02224   0.01493  -0.0598   0.0191   1.0000
  10.250   1.3114   0.02311   0.01586  -0.0582   0.0175   1.0000
  10.500   1.3258   0.02395   0.01677  -0.0568   0.0160   1.0000
  10.750   1.3387   0.02492   0.01778  -0.0553   0.0145   1.0000
  11.000   1.3506   0.02600   0.01891  -0.0537   0.0133   1.0000
  11.250   1.3632   0.02703   0.02003  -0.0523   0.0123   1.0000
  11.500   1.3750   0.02816   0.02122  -0.0509   0.0113   1.0000
  11.750   1.3850   0.02945   0.02255  -0.0494   0.0104   1.0000
  12.000   1.3952   0.03074   0.02392  -0.0479   0.0098   1.0000
  12.250   1.4050   0.03209   0.02536  -0.0466   0.0093   1.0000
  12.500   1.4141   0.03353   0.02689  -0.0452   0.0088   1.0000
  12.750   1.4222   0.03506   0.02851  -0.0439   0.0085   1.0000
  13.000   1.4292   0.03674   0.03025  -0.0426   0.0081   1.0000
  13.250   1.4343   0.03862   0.03224  -0.0412   0.0078   1.0000
  13.500   1.4374   0.04073   0.03445  -0.0398   0.0075   1.0000
  13.750   1.4424   0.04269   0.03653  -0.0387   0.0074   1.0000
  14.000   1.4467   0.04477   0.03872  -0.0377   0.0071   1.0000
  14.250   1.4502   0.04698   0.04104  -0.0367   0.0069   1.0000
  14.500   1.4531   0.04930   0.04347  -0.0359   0.0067   1.0000
  14.750   1.4552   0.05177   0.04606  -0.0352   0.0065   1.0000
  15.000   1.4567   0.05442   0.04882  -0.0347   0.0063   1.0000
  15.250   1.4574   0.05723   0.05174  -0.0343   0.0061   1.0000
  15.500   1.4567   0.06031   0.05493  -0.0340   0.0059   1.0000
  15.750   1.4539   0.06372   0.05846  -0.0339   0.0058   1.0000
  16.000   1.4496   0.06745   0.06233  -0.0341   0.0057   1.0000
  16.250   1.4430   0.07162   0.06662  -0.0344   0.0056   1.0000
  16.500   1.4341   0.07625   0.07138  -0.0351   0.0055   1.0000
  16.750   1.4252   0.08100   0.07627  -0.0360   0.0054   1.0000
  17.000   1.4183   0.08562   0.08104  -0.0370   0.0054   1.0000
  17.250   1.4102   0.09056   0.08612  -0.0384   0.0053   1.0000
  17.500   1.4011   0.09579   0.09151  -0.0400   0.0053   1.0000
  17.750   1.3905   0.10136   0.09723  -0.0420   0.0052   1.0000
  18.000   1.3792   0.10723   0.10325  -0.0442   0.0052   1.0000
  18.250   1.3673   0.11337   0.10953  -0.0467   0.0051   1.0000
  18.500   1.3544   0.11986   0.11617  -0.0496   0.0051   1.0000
  18.750   1.3413   0.12652   0.12298  -0.0528   0.0050   1.0000
  19.000   1.3275   0.13347   0.13007  -0.0563   0.0050   1.0000
  19.250   1.3138   0.14060   0.13734  -0.0601   0.0050   1.0000
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