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SG6050 (sg6050-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 500,000
Max Cl/Cd: 105.08 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6050-il-500000.txt
Download as CSV file: xf-sg6050-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6050                                          
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.7510   0.13745   0.13454  -0.0219   1.0000   0.0113
 -17.750  -0.7703   0.12881   0.12577  -0.0266   1.0000   0.0112
 -17.500  -0.7873   0.12091   0.11776  -0.0309   1.0000   0.0112
 -17.250  -0.8028   0.11355   0.11029  -0.0349   1.0000   0.0112
 -17.000  -0.8175   0.10656   0.10318  -0.0387   1.0000   0.0111
 -16.750  -0.8313   0.09982   0.09633  -0.0424   1.0000   0.0111
 -16.500  -0.8442   0.09344   0.08985  -0.0459   1.0000   0.0111
 -16.250  -0.8563   0.08738   0.08368  -0.0493   1.0000   0.0111
 -16.000  -0.8682   0.08154   0.07773  -0.0526   1.0000   0.0111
 -15.750  -0.8805   0.07600   0.07208  -0.0556   1.0000   0.0112
 -15.500  -0.8922   0.07072   0.06669  -0.0585   1.0000   0.0112
 -15.250  -0.9031   0.06567   0.06154  -0.0613   1.0000   0.0112
 -15.000  -0.9129   0.06078   0.05654  -0.0640   1.0000   0.0112
 -14.750  -0.9210   0.05613   0.05178  -0.0667   1.0000   0.0112
 -14.500  -0.9294   0.05142   0.04697  -0.0694   1.0000   0.0113
 -14.250  -0.9376   0.04668   0.04212  -0.0723   1.0000   0.0114
 -14.000  -0.9439   0.04207   0.03740  -0.0754   1.0000   0.0114
 -13.750  -0.9483   0.03780   0.03301  -0.0785   1.0000   0.0115
 -13.500  -0.9519   0.03417   0.02926  -0.0807   1.0000   0.0117
 -13.250  -0.9548   0.03144   0.02643  -0.0812   1.0000   0.0118
 -13.000  -0.9586   0.02944   0.02435  -0.0799   1.0000   0.0119
 -12.750  -0.9677   0.02812   0.02296  -0.0762   1.0000   0.0121
 -12.500  -0.9739   0.02715   0.02194  -0.0721   0.9994   0.0122
 -12.250  -0.9473   0.02564   0.02033  -0.0743   0.9952   0.0127
 -12.000  -0.9194   0.02430   0.01888  -0.0763   0.9902   0.0132
 -11.750  -0.8910   0.02315   0.01760  -0.0780   0.9835   0.0137
 -11.500  -0.8693   0.02172   0.01608  -0.0786   0.9717   0.0143
 -11.250  -0.8472   0.02066   0.01494  -0.0787   0.9590   0.0150
 -11.000  -0.8262   0.01982   0.01399  -0.0782   0.9457   0.0158
 -10.500  -0.7877   0.01818   0.01215  -0.0761   0.9204   0.0184
 -10.000  -0.7465   0.01654   0.01041  -0.0744   0.8996   0.0283
  -9.750  -0.7223   0.01613   0.01001  -0.0741   0.8912   0.0395
  -9.500  -0.6956   0.01595   0.00982  -0.0741   0.8827   0.0456
  -9.250  -0.6696   0.01573   0.00956  -0.0739   0.8758   0.0498
  -9.000  -0.6416   0.01564   0.00940  -0.0741   0.8684   0.0535
  -8.750  -0.6154   0.01536   0.00904  -0.0740   0.8618   0.0567
  -8.500  -0.5883   0.01514   0.00880  -0.0742   0.8553   0.0600
  -8.250  -0.5605   0.01498   0.00856  -0.0743   0.8489   0.0629
  -8.000  -0.5336   0.01476   0.00823  -0.0743   0.8433   0.0652
  -7.750  -0.5069   0.01431   0.00779  -0.0745   0.8373   0.0690
  -7.500  -0.4790   0.01413   0.00756  -0.0747   0.8317   0.0724
  -7.250  -0.4508   0.01406   0.00738  -0.0748   0.8267   0.0752
  -7.000  -0.4240   0.01353   0.00686  -0.0750   0.8213   0.0796
  -6.750  -0.3960   0.01330   0.00660  -0.0752   0.8160   0.0836
  -6.500  -0.3677   0.01313   0.00634  -0.0754   0.8112   0.0868
  -6.250  -0.3400   0.01275   0.00591  -0.0756   0.8064   0.0903
  -6.000  -0.3118   0.01241   0.00557  -0.0759   0.8012   0.0950
  -5.750  -0.2833   0.01219   0.00529  -0.0762   0.7966   0.0994
  -5.500  -0.2550   0.01190   0.00496  -0.0764   0.7922   0.1058
  -5.250  -0.2261   0.01162   0.00470  -0.0768   0.7872   0.1146
  -5.000  -0.1977   0.01125   0.00439  -0.0772   0.7824   0.1322
  -4.750  -0.1698   0.01077   0.00406  -0.0775   0.7781   0.1725
  -4.500  -0.1422   0.01016   0.00380  -0.0780   0.7734   0.2542
  -4.250  -0.1134   0.00990   0.00373  -0.0784   0.7683   0.3081
  -4.000  -0.0840   0.00983   0.00367  -0.0788   0.7635   0.3354
  -3.750  -0.0544   0.00983   0.00364  -0.0792   0.7589   0.3532
  -3.500  -0.0245   0.00982   0.00360  -0.0796   0.7538   0.3664
  -3.250   0.0051   0.00978   0.00356  -0.0800   0.7490   0.3769
  -3.000   0.0348   0.00978   0.00349  -0.0804   0.7446   0.3857
  -2.750   0.0645   0.00976   0.00346  -0.0809   0.7399   0.3942
  -2.500   0.0943   0.00973   0.00341  -0.0813   0.7347   0.4023
  -2.250   0.1239   0.00969   0.00335  -0.0817   0.7300   0.4099
  -2.000   0.1536   0.00971   0.00330  -0.0821   0.7254   0.4165
  -1.750   0.1832   0.00962   0.00326  -0.0825   0.7201   0.4248
  -1.500   0.2127   0.00958   0.00323  -0.0829   0.7150   0.4383
  -1.250   0.2423   0.00961   0.00320  -0.0833   0.7103   0.4503
  -1.000   0.2718   0.00950   0.00316  -0.0838   0.7047   0.4574
  -0.750   0.3015   0.00945   0.00311  -0.0842   0.6991   0.4636
  -0.500   0.3310   0.00943   0.00305  -0.0846   0.6941   0.4697
  -0.250   0.3606   0.00935   0.00303  -0.0851   0.6881   0.4771
   0.000   0.3902   0.00931   0.00299  -0.0855   0.6824   0.4853
   0.250   0.4196   0.00927   0.00297  -0.0859   0.6771   0.4950
   0.500   0.4491   0.00919   0.00297  -0.0864   0.6708   0.5075
   0.750   0.4785   0.00913   0.00295  -0.0868   0.6648   0.5248
   1.000   0.5078   0.00905   0.00297  -0.0872   0.6589   0.5521
   1.250   0.5368   0.00887   0.00300  -0.0876   0.6521   0.6042
   1.500   0.5648   0.00864   0.00304  -0.0877   0.6458   0.6950
   1.750   0.5889   0.00832   0.00319  -0.0867   0.6385   0.8155
   2.000   0.6111   0.00828   0.00327  -0.0851   0.6316   0.8894
   2.250   0.6335   0.00827   0.00332  -0.0837   0.6244   0.9256
   2.500   0.6572   0.00827   0.00334  -0.0825   0.6171   0.9534
   2.750   0.6872   0.00830   0.00336  -0.0828   0.6095   0.9756
   3.000   0.7226   0.00836   0.00339  -0.0845   0.6013   0.9918
   3.250   0.7595   0.00841   0.00343  -0.0867   0.5929   1.0000
   3.500   0.7862   0.00851   0.00348  -0.0866   0.5844   1.0000
   3.750   0.8135   0.00860   0.00357  -0.0867   0.5757   1.0000
   4.000   0.8409   0.00874   0.00364  -0.0867   0.5668   1.0000
   4.250   0.8687   0.00884   0.00376  -0.0869   0.5570   1.0000
   4.500   0.8962   0.00899   0.00386  -0.0870   0.5468   1.0000
   4.750   0.9235   0.00915   0.00398  -0.0871   0.5358   1.0000
   5.000   0.9510   0.00930   0.00413  -0.0872   0.5249   1.0000
   5.250   0.9782   0.00948   0.00428  -0.0873   0.5142   1.0000
   5.500   1.0049   0.00969   0.00444  -0.0873   0.5028   1.0000
   5.750   1.0318   0.00987   0.00462  -0.0873   0.4907   1.0000
   6.000   1.0583   0.01008   0.00482  -0.0873   0.4784   1.0000
   6.250   1.0844   0.01032   0.00502  -0.0872   0.4661   1.0000
   6.500   1.1099   0.01058   0.00525  -0.0870   0.4537   1.0000
   6.750   1.1353   0.01084   0.00549  -0.0867   0.4406   1.0000
   7.000   1.1604   0.01111   0.00574  -0.0865   0.4269   1.0000
   7.250   1.1848   0.01141   0.00603  -0.0861   0.4127   1.0000
   7.500   1.2087   0.01173   0.00632  -0.0856   0.3986   1.0000
   7.750   1.2320   0.01207   0.00663  -0.0851   0.3843   1.0000
   8.000   1.2546   0.01244   0.00697  -0.0844   0.3696   1.0000
   8.250   1.2759   0.01285   0.00734  -0.0835   0.3526   1.0000
   8.500   1.2952   0.01333   0.00776  -0.0823   0.3330   1.0000
   8.750   1.3132   0.01387   0.00822  -0.0809   0.3142   1.0000
   9.000   1.3299   0.01442   0.00872  -0.0792   0.2953   1.0000
   9.250   1.3445   0.01502   0.00925  -0.0772   0.2747   1.0000
   9.500   1.3540   0.01574   0.00989  -0.0744   0.2546   1.0000
   9.750   1.3634   0.01657   0.01064  -0.0717   0.2349   1.0000
  10.000   1.3731   0.01748   0.01147  -0.0693   0.2132   1.0000
  10.250   1.3807   0.01858   0.01247  -0.0668   0.1921   1.0000
  10.500   1.3888   0.01972   0.01353  -0.0645   0.1728   1.0000
  10.750   1.3968   0.02095   0.01469  -0.0625   0.1551   1.0000
  11.000   1.4044   0.02227   0.01595  -0.0605   0.1390   1.0000
  11.250   1.4116   0.02368   0.01730  -0.0587   0.1242   1.0000
  11.500   1.4184   0.02517   0.01875  -0.0570   0.1108   1.0000
  11.750   1.4251   0.02672   0.02026  -0.0554   0.0988   1.0000
  12.000   1.4316   0.02833   0.02185  -0.0538   0.0879   1.0000
  12.250   1.4373   0.03004   0.02354  -0.0524   0.0781   1.0000
  12.500   1.4421   0.03186   0.02535  -0.0510   0.0695   1.0000
  13.000   1.4509   0.03570   0.02920  -0.0484   0.0550   1.0000
  13.250   1.4543   0.03776   0.03127  -0.0472   0.0490   1.0000
  13.500   1.4558   0.04002   0.03354  -0.0460   0.0434   1.0000
  13.750   1.4574   0.04237   0.03591  -0.0449   0.0381   1.0000
  14.000   1.4587   0.04481   0.03837  -0.0439   0.0334   1.0000
  14.250   1.4578   0.04754   0.04114  -0.0430   0.0291   1.0000
  14.500   1.4546   0.05061   0.04423  -0.0422   0.0255   1.0000
  14.750   1.4529   0.05362   0.04730  -0.0416   0.0227   1.0000
  15.000   1.4493   0.05692   0.05067  -0.0411   0.0206   1.0000
  15.250   1.4474   0.06012   0.05393  -0.0408   0.0190   1.0000
  15.500   1.4401   0.06406   0.05794  -0.0406   0.0179   1.0000
  15.750   1.4396   0.06726   0.06124  -0.0405   0.0169   1.0000
  16.000   1.4373   0.07071   0.06479  -0.0406   0.0162   1.0000
  16.250   1.4334   0.07445   0.06861  -0.0408   0.0156   1.0000
  16.500   1.4265   0.07866   0.07290  -0.0412   0.0151   1.0000
  16.750   1.4155   0.08351   0.07785  -0.0418   0.0146   1.0000
  17.000   1.4117   0.08742   0.08187  -0.0424   0.0143   1.0000
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