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SG6050 (sg6050-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 500,000
Max Cl/Cd: 97.26 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6050-il-500000-n5.txt
Download as CSV file: xf-sg6050-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8413   0.09341   0.08977  -0.0434   1.0000   0.0070
 -16.000  -0.8696   0.08448   0.08069  -0.0481   1.0000   0.0069
 -15.750  -0.8984   0.07603   0.07210  -0.0527   1.0000   0.0069
 -15.500  -0.9236   0.06849   0.06443  -0.0569   1.0000   0.0069
 -15.250  -0.9459   0.06159   0.05739  -0.0608   1.0000   0.0069
 -15.000  -0.9642   0.05529   0.05096  -0.0646   1.0000   0.0069
 -14.750  -0.9780   0.04949   0.04503  -0.0684   1.0000   0.0069
 -14.500  -0.9866   0.04416   0.03954  -0.0723   1.0000   0.0069
 -14.250  -0.9911   0.03945   0.03468  -0.0760   1.0000   0.0070
 -14.000  -0.9963   0.03519   0.03027  -0.0792   1.0000   0.0070
 -13.750  -1.0003   0.03204   0.02699  -0.0805   1.0000   0.0071
 -13.500  -1.0034   0.02980   0.02465  -0.0799   1.0000   0.0072
 -13.250  -1.0045   0.02817   0.02292  -0.0782   0.9956   0.0074
 -13.000  -0.9909   0.02668   0.02132  -0.0783   0.9801   0.0075
 -12.750  -0.9745   0.02544   0.01997  -0.0782   0.9601   0.0078
 -12.500  -0.9575   0.02437   0.01878  -0.0777   0.9408   0.0080
 -12.250  -0.9421   0.02346   0.01772  -0.0766   0.9225   0.0082
 -12.000  -0.9257   0.02264   0.01675  -0.0754   0.9065   0.0085
 -11.750  -0.9078   0.02188   0.01585  -0.0744   0.8929   0.0088
 -11.500  -0.8882   0.02114   0.01499  -0.0736   0.8814   0.0090
 -11.250  -0.8684   0.02035   0.01409  -0.0730   0.8715   0.0095
 -11.000  -0.8471   0.01967   0.01329  -0.0724   0.8619   0.0100
 -10.750  -0.8246   0.01904   0.01255  -0.0720   0.8534   0.0107
 -10.500  -0.8016   0.01844   0.01184  -0.0716   0.8453   0.0115
 -10.250  -0.7782   0.01780   0.01114  -0.0714   0.8385   0.0130
 -10.000  -0.7543   0.01719   0.01046  -0.0712   0.8316   0.0152
  -9.750  -0.7302   0.01660   0.00980  -0.0710   0.8254   0.0190
  -9.500  -0.7053   0.01602   0.00921  -0.0709   0.8190   0.0242
  -9.250  -0.6799   0.01554   0.00873  -0.0709   0.8130   0.0308
  -9.000  -0.6534   0.01518   0.00835  -0.0710   0.8079   0.0369
  -8.750  -0.6262   0.01486   0.00801  -0.0711   0.8023   0.0414
  -8.500  -0.5988   0.01460   0.00770  -0.0713   0.7969   0.0454
  -8.250  -0.5714   0.01434   0.00737  -0.0714   0.7920   0.0482
  -8.000  -0.5436   0.01407   0.00709  -0.0717   0.7868   0.0514
  -7.750  -0.5154   0.01388   0.00682  -0.0719   0.7817   0.0543
  -7.500  -0.4878   0.01360   0.00651  -0.0721   0.7771   0.0577
  -7.250  -0.4595   0.01337   0.00626  -0.0724   0.7725   0.0612
  -7.000  -0.4308   0.01320   0.00603  -0.0727   0.7677   0.0641
  -6.750  -0.4029   0.01291   0.00572  -0.0730   0.7632   0.0681
  -6.500  -0.3745   0.01268   0.00545  -0.0733   0.7590   0.0713
  -6.250  -0.3457   0.01247   0.00520  -0.0736   0.7545   0.0739
  -6.000  -0.3169   0.01227   0.00494  -0.0740   0.7500   0.0764
  -5.750  -0.2883   0.01203   0.00468  -0.0743   0.7456   0.0802
  -5.500  -0.2594   0.01183   0.00445  -0.0746   0.7417   0.0843
  -5.250  -0.2303   0.01164   0.00424  -0.0750   0.7373   0.0893
  -5.000  -0.2013   0.01142   0.00403  -0.0754   0.7328   0.0968
  -4.750  -0.1724   0.01123   0.00382  -0.0758   0.7286   0.1057
  -4.500  -0.1433   0.01102   0.00363  -0.0762   0.7244   0.1186
  -4.250  -0.1142   0.01076   0.00344  -0.0767   0.7196   0.1380
  -4.000  -0.0854   0.01047   0.00324  -0.0771   0.7146   0.1678
  -3.750  -0.0569   0.01011   0.00303  -0.0776   0.7102   0.2170
  -3.500  -0.0279   0.00980   0.00291  -0.0781   0.7053   0.2658
  -3.250   0.0014   0.00964   0.00284  -0.0786   0.7003   0.2981
  -3.000   0.0309   0.00957   0.00279  -0.0790   0.6957   0.3191
  -2.750   0.0606   0.00952   0.00274  -0.0794   0.6911   0.3346
  -2.500   0.0904   0.00948   0.00271  -0.0799   0.6859   0.3481
  -2.250   0.1201   0.00944   0.00266  -0.0803   0.6808   0.3582
  -2.000   0.1498   0.00944   0.00262  -0.0808   0.6761   0.3659
  -1.750   0.1796   0.00940   0.00260  -0.0812   0.6705   0.3763
  -1.500   0.2091   0.00938   0.00260  -0.0817   0.6650   0.3925
  -1.250   0.2387   0.00936   0.00258  -0.0821   0.6597   0.4046
  -1.000   0.2684   0.00934   0.00256  -0.0825   0.6536   0.4107
  -0.750   0.2979   0.00935   0.00252  -0.0829   0.6474   0.4148
  -0.500   0.3275   0.00933   0.00250  -0.0834   0.6413   0.4188
  -0.250   0.3570   0.00931   0.00248  -0.0838   0.6346   0.4238
   0.000   0.3864   0.00933   0.00247  -0.0842   0.6287   0.4288
   0.250   0.4160   0.00933   0.00247  -0.0846   0.6220   0.4335
   0.500   0.4453   0.00933   0.00248  -0.0850   0.6155   0.4396
   0.750   0.4747   0.00934   0.00249  -0.0854   0.6089   0.4459
   1.000   0.5040   0.00935   0.00252  -0.0858   0.6018   0.4531
   1.250   0.5332   0.00936   0.00255  -0.0862   0.5949   0.4621
   1.500   0.5623   0.00937   0.00258  -0.0866   0.5866   0.4724
   1.750   0.5913   0.00938   0.00263  -0.0870   0.5786   0.4862
   2.000   0.6202   0.00938   0.00269  -0.0874   0.5696   0.5074
   2.250   0.6490   0.00936   0.00276  -0.0877   0.5612   0.5387
   2.500   0.6775   0.00931   0.00285  -0.0881   0.5524   0.5843
   2.750   0.7059   0.00923   0.00295  -0.0884   0.5437   0.6436
   3.000   0.7333   0.00915   0.00307  -0.0885   0.5348   0.7131
   3.250   0.7586   0.00901   0.00324  -0.0879   0.5259   0.8023
   3.500   0.7817   0.00904   0.00339  -0.0867   0.5171   0.8698
   3.750   0.8064   0.00910   0.00351  -0.0860   0.5078   0.8993
   4.000   0.8307   0.00921   0.00363  -0.0852   0.4985   0.9220
   4.250   0.8550   0.00932   0.00375  -0.0844   0.4883   0.9423
   4.500   0.8816   0.00945   0.00386  -0.0842   0.4766   0.9632
   4.750   0.9104   0.00961   0.00400  -0.0846   0.4641   0.9840
   5.000   0.9401   0.00978   0.00413  -0.0853   0.4518   1.0000
   5.250   0.9666   0.01001   0.00431  -0.0852   0.4396   1.0000
   5.500   0.9932   0.01023   0.00450  -0.0852   0.4277   1.0000
   5.750   1.0193   0.01048   0.00472  -0.0851   0.4152   1.0000
   6.000   1.0448   0.01075   0.00495  -0.0850   0.4017   1.0000
   6.250   1.0700   0.01104   0.00519  -0.0847   0.3885   1.0000
   6.500   1.0948   0.01135   0.00546  -0.0844   0.3750   1.0000
   6.750   1.1194   0.01165   0.00573  -0.0841   0.3610   1.0000
   7.000   1.1431   0.01200   0.00604  -0.0837   0.3460   1.0000
   7.250   1.1658   0.01239   0.00637  -0.0830   0.3297   1.0000
   7.500   1.1878   0.01281   0.00673  -0.0823   0.3134   1.0000
   7.750   1.2092   0.01323   0.00711  -0.0814   0.2974   1.0000
   8.000   1.2296   0.01369   0.00752  -0.0804   0.2811   1.0000
   8.250   1.2484   0.01420   0.00797  -0.0792   0.2631   1.0000
   8.500   1.2643   0.01483   0.00850  -0.0774   0.2410   1.0000
   8.750   1.2760   0.01554   0.00910  -0.0750   0.2186   1.0000
   9.000   1.2863   0.01630   0.00978  -0.0723   0.1975   1.0000
   9.250   1.2963   0.01716   0.01054  -0.0698   0.1781   1.0000
   9.500   1.3064   0.01810   0.01139  -0.0675   0.1595   1.0000
   9.750   1.3163   0.01910   0.01232  -0.0654   0.1416   1.0000
  10.000   1.3262   0.02017   0.01332  -0.0634   0.1256   1.0000
  10.250   1.3356   0.02133   0.01442  -0.0615   0.1107   1.0000
  10.500   1.3450   0.02253   0.01558  -0.0598   0.0978   1.0000
  10.750   1.3543   0.02380   0.01682  -0.0582   0.0861   1.0000
  11.000   1.3638   0.02511   0.01810  -0.0567   0.0763   1.0000
  11.250   1.3729   0.02648   0.01945  -0.0553   0.0676   1.0000
  11.500   1.3814   0.02793   0.02089  -0.0539   0.0601   1.0000
  11.750   1.3896   0.02944   0.02241  -0.0526   0.0533   1.0000
  12.000   1.3981   0.03096   0.02393  -0.0514   0.0475   1.0000
  12.250   1.4052   0.03262   0.02560  -0.0502   0.0422   1.0000
  12.500   1.4116   0.03437   0.02737  -0.0490   0.0374   1.0000
  12.750   1.4186   0.03610   0.02913  -0.0480   0.0333   1.0000
  13.000   1.4241   0.03798   0.03105  -0.0469   0.0300   1.0000
  13.250   1.4292   0.03994   0.03305  -0.0459   0.0268   1.0000
  13.500   1.4342   0.04196   0.03511  -0.0450   0.0242   1.0000
  13.750   1.4378   0.04416   0.03735  -0.0442   0.0218   1.0000
  14.000   1.4424   0.04633   0.03958  -0.0435   0.0197   1.0000
  14.250   1.4447   0.04878   0.04208  -0.0428   0.0179   1.0000
  14.500   1.4483   0.05118   0.04454  -0.0422   0.0162   1.0000
  14.750   1.4498   0.05385   0.04727  -0.0418   0.0147   1.0000
  15.000   1.4521   0.05647   0.04997  -0.0414   0.0134   1.0000
  15.250   1.4529   0.05932   0.05289  -0.0411   0.0124   1.0000
  15.500   1.4534   0.06228   0.05592  -0.0409   0.0116   1.0000
  15.750   1.4540   0.06529   0.05901  -0.0408   0.0108   1.0000
  16.000   1.4533   0.06849   0.06229  -0.0409   0.0103   1.0000
  16.250   1.4513   0.07190   0.06578  -0.0410   0.0098   1.0000
  16.500   1.4491   0.07542   0.06939  -0.0412   0.0094   1.0000
  16.750   1.4473   0.07894   0.07301  -0.0415   0.0091   1.0000
  17.000   1.4448   0.08261   0.07677  -0.0420   0.0089   1.0000
  17.250   1.4415   0.08641   0.08068  -0.0426   0.0086   1.0000
  17.500   1.4373   0.09038   0.08475  -0.0432   0.0084   1.0000
  17.750   1.4325   0.09451   0.08897  -0.0440   0.0082   1.0000
  18.000   1.4269   0.09882   0.09338  -0.0450   0.0081   1.0000
  18.250   1.4207   0.10327   0.09792  -0.0461   0.0079   1.0000
  18.500   1.4135   0.10788   0.10264  -0.0474   0.0078   1.0000
  18.750   1.4053   0.11275   0.10760  -0.0489   0.0076   1.0000
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