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SG6050 (sg6050-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 100,000
Max Cl/Cd: 50.03 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6050-il-100000.txt
Download as CSV file: xf-sg6050-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4247   0.13166   0.12669  -0.0436   1.0000   0.1297
 -12.000  -0.4543   0.11017   0.10525  -0.0527   1.0000   0.0879
 -11.750  -0.6008   0.07273   0.06770  -0.0772   1.0000   0.0643
 -11.500  -0.6270   0.06679   0.06170  -0.0803   1.0000   0.0638
 -11.250  -0.6558   0.06269   0.05755  -0.0802   1.0000   0.0634
 -11.000  -0.6873   0.06059   0.05545  -0.0760   1.0000   0.0630
 -10.750  -0.7191   0.05909   0.05394  -0.0705   1.0000   0.0627
 -10.500  -0.7500   0.05753   0.05232  -0.0649   1.0000   0.0625
 -10.250  -0.7780   0.05536   0.04997  -0.0600   1.0000   0.0626
 -10.000  -0.8022   0.05257   0.04684  -0.0557   1.0000   0.0633
  -9.500  -0.8093   0.04848   0.04254  -0.0504   1.0000   0.0681
  -9.250  -0.8092   0.04651   0.04034  -0.0481   1.0000   0.0718
  -9.000  -0.8001   0.04299   0.03626  -0.0482   0.9973   0.0776
  -8.750  -0.7704   0.04164   0.03451  -0.0505   0.9924   0.0872
  -8.500  -0.7399   0.04021   0.03324  -0.0528   0.9874   0.0965
  -8.250  -0.7087   0.03812   0.03082  -0.0554   0.9831   0.1059
  -8.000  -0.6818   0.03681   0.02904  -0.0565   0.9770   0.1143
  -7.750  -0.6486   0.03491   0.02712  -0.0589   0.9726   0.1217
  -7.500  -0.6172   0.03367   0.02541  -0.0605   0.9675   0.1288
  -7.250  -0.5864   0.03204   0.02374  -0.0621   0.9622   0.1349
  -7.000  -0.5484   0.03097   0.02240  -0.0647   0.9581   0.1425
  -6.750  -0.5190   0.02976   0.02108  -0.0656   0.9525   0.1481
  -6.500  -0.4862   0.02889   0.02015  -0.0671   0.9470   0.1555
  -6.250  -0.4465   0.02783   0.01897  -0.0698   0.9433   0.1632
  -6.000  -0.4183   0.02718   0.01833  -0.0704   0.9373   0.1721
  -5.750  -0.3864   0.02639   0.01759  -0.0716   0.9317   0.1825
  -5.500  -0.3470   0.02555   0.01683  -0.0743   0.9279   0.1985
  -5.250  -0.3190   0.02496   0.01635  -0.0749   0.9219   0.2217
  -5.000  -0.2900   0.02425   0.01604  -0.0758   0.9158   0.2688
  -4.750  -0.2508   0.02431   0.01642  -0.0781   0.9115   0.3609
  -4.500  -0.2280   0.02477   0.01681  -0.0774   0.9040   0.4015
  -4.250  -0.1958   0.02496   0.01691  -0.0784   0.8980   0.4328
  -4.000  -0.1535   0.02490   0.01687  -0.0811   0.8945   0.4595
  -3.750  -0.1351   0.02515   0.01711  -0.0797   0.8862   0.4773
  -3.500  -0.0993   0.02512   0.01701  -0.0813   0.8809   0.4985
  -3.250  -0.0563   0.02491   0.01678  -0.0839   0.8776   0.5197
  -3.000  -0.0400   0.02522   0.01710  -0.0822   0.8684   0.5358
  -2.750  -0.0049   0.02509   0.01704  -0.0834   0.8634   0.5573
  -2.500   0.0359   0.02485   0.01681  -0.0853   0.8603   0.5816
  -2.250   0.0485   0.02526   0.01726  -0.0831   0.8498   0.5962
  -2.000   0.0863   0.02498   0.01697  -0.0847   0.8456   0.6121
  -1.750   0.1107   0.02512   0.01710  -0.0844   0.8381   0.6249
  -1.500   0.1397   0.02509   0.01707  -0.0848   0.8313   0.6392
  -1.250   0.1786   0.02472   0.01670  -0.0864   0.8277   0.6560
  -1.000   0.1946   0.02515   0.01719  -0.0849   0.8176   0.6720
  -0.750   0.2280   0.02485   0.01699  -0.0855   0.8127   0.6929
  -0.500   0.2544   0.02484   0.01708  -0.0850   0.8064   0.7192
  -0.250   0.2748   0.02495   0.01737  -0.0835   0.7980   0.7536
   0.000   0.3045   0.02453   0.01718  -0.0822   0.7943   0.8107
   0.250   0.3143   0.02513   0.01798  -0.0784   0.7836   0.8976
   0.500   0.3966   0.02472   0.01751  -0.0880   0.7805   0.9861
   0.750   0.4548   0.02418   0.01679  -0.0938   0.7772   1.0000
   1.000   0.4565   0.02498   0.01750  -0.0903   0.7650   1.0000
   1.250   0.4921   0.02461   0.01700  -0.0912   0.7610   1.0000
   1.500   0.5010   0.02543   0.01777  -0.0887   0.7494   1.0000
   1.750   0.5368   0.02507   0.01732  -0.0895   0.7451   1.0000
   2.000   0.5496   0.02585   0.01808  -0.0876   0.7340   1.0000
   2.250   0.5845   0.02553   0.01768  -0.0883   0.7294   1.0000
   2.500   0.6007   0.02621   0.01835  -0.0868   0.7190   1.0000
   2.750   0.6344   0.02591   0.01801  -0.0872   0.7136   1.0000
   3.000   0.6544   0.02642   0.01851  -0.0862   0.7042   1.0000
   3.250   0.6861   0.02620   0.01827  -0.0864   0.6979   1.0000
   3.500   0.7208   0.02584   0.01787  -0.0869   0.6930   1.0000
   3.750   0.7393   0.02637   0.01843  -0.0857   0.6821   1.0000
   4.000   0.7784   0.02571   0.01773  -0.0866   0.6783   1.0000
   4.250   0.7935   0.02646   0.01854  -0.0850   0.6663   1.0000
   4.500   0.8329   0.02576   0.01781  -0.0860   0.6623   1.0000
   4.750   0.8486   0.02648   0.01861  -0.0844   0.6504   1.0000
   5.000   0.8888   0.02572   0.01781  -0.0855   0.6462   1.0000
   5.250   0.9048   0.02641   0.01858  -0.0839   0.6342   1.0000
   5.500   0.9349   0.02626   0.01847  -0.0839   0.6266   1.0000
   5.750   0.9625   0.02621   0.01846  -0.0836   0.6175   1.0000
   6.000   0.9871   0.02637   0.01868  -0.0829   0.6077   1.0000
   6.250   1.0227   0.02580   0.01810  -0.0834   0.6000   1.0000
   6.500   1.0436   0.02613   0.01852  -0.0823   0.5884   1.0000
   6.750   1.0795   0.02559   0.01796  -0.0829   0.5802   1.0000
   7.000   1.1045   0.02563   0.01807  -0.0822   0.5687   1.0000
   7.250   1.1271   0.02584   0.01835  -0.0812   0.5568   1.0000
   7.500   1.1565   0.02567   0.01821  -0.0810   0.5459   1.0000
   7.750   1.1898   0.02530   0.01780  -0.0813   0.5348   1.0000
   8.000   1.2104   0.02554   0.01814  -0.0800   0.5211   1.0000
   8.250   1.2326   0.02573   0.01840  -0.0789   0.5074   1.0000
   8.500   1.2557   0.02588   0.01859  -0.0779   0.4935   1.0000
   8.750   1.2786   0.02602   0.01876  -0.0769   0.4790   1.0000
   9.000   1.3002   0.02619   0.01896  -0.0757   0.4638   1.0000
   9.250   1.3200   0.02643   0.01924  -0.0742   0.4479   1.0000
   9.500   1.3379   0.02674   0.01957  -0.0725   0.4314   1.0000
   9.750   1.3537   0.02713   0.01999  -0.0705   0.4145   1.0000
  10.000   1.3672   0.02760   0.02047  -0.0682   0.3971   1.0000
  10.250   1.3780   0.02813   0.02104  -0.0656   0.3795   1.0000
  10.500   1.3859   0.02876   0.02165  -0.0625   0.3618   1.0000
  10.750   1.3893   0.02948   0.02234  -0.0588   0.3444   1.0000
  11.000   1.3883   0.03047   0.02334  -0.0548   0.3269   1.0000
  11.250   1.3851   0.03172   0.02462  -0.0510   0.3089   1.0000
  11.500   1.3818   0.03318   0.02609  -0.0476   0.2905   1.0000
  11.750   1.3784   0.03482   0.02773  -0.0445   0.2722   1.0000
  12.000   1.3750   0.03664   0.02950  -0.0417   0.2541   1.0000
  12.250   1.3715   0.03865   0.03141  -0.0392   0.2363   1.0000
  12.500   1.3663   0.04095   0.03368  -0.0369   0.2189   1.0000
  12.750   1.3607   0.04343   0.03614  -0.0349   0.2021   1.0000
  13.000   1.3554   0.04603   0.03870  -0.0330   0.1863   1.0000
  13.250   1.3500   0.04874   0.04137  -0.0313   0.1714   1.0000
  13.500   1.3449   0.05156   0.04413  -0.0299   0.1576   1.0000
  13.750   1.3397   0.05444   0.04695  -0.0285   0.1449   1.0000
  14.000   1.3350   0.05737   0.04979  -0.0274   0.1331   1.0000
  14.250   1.3285   0.06064   0.05312  -0.0266   0.1225   1.0000
  14.500   1.3227   0.06399   0.05653  -0.0259   0.1124   1.0000
  14.750   1.3187   0.06721   0.05974  -0.0253   0.1034   1.0000
  15.000   1.3180   0.07003   0.06240  -0.0246   0.0947   1.0000
  15.250   1.3115   0.07386   0.06646  -0.0245   0.0877   1.0000
  15.500   1.3117   0.07677   0.06931  -0.0240   0.0808   1.0000
  15.750   1.3087   0.08024   0.07288  -0.0239   0.0749   1.0000
  16.000   1.3107   0.08310   0.07574  -0.0233   0.0694   1.0000
  16.250   1.3082   0.08662   0.07939  -0.0234   0.0649   1.0000
  16.500   1.3150   0.08887   0.08157  -0.0227   0.0604   1.0000
  16.750   1.3091   0.09310   0.08607  -0.0232   0.0576   1.0000
  17.000   1.3110   0.09619   0.08925  -0.0232   0.0548   1.0000
  17.250   1.3257   0.09774   0.09069  -0.0220   0.0519   1.0000
  17.500   1.3140   0.10291   0.09620  -0.0233   0.0509   1.0000
  17.750   1.3021   0.10828   0.10187  -0.0249   0.0498   1.0000
  18.000   1.2896   0.11389   0.10774  -0.0269   0.0489   1.0000
  18.250   1.2764   0.11979   0.11387  -0.0294   0.0481   1.0000
  18.500   1.2615   0.12620   0.12051  -0.0324   0.0475   1.0000
  18.750   1.2406   0.13403   0.12860  -0.0367   0.0473   1.0000
  19.000   1.1976   0.14717   0.14213  -0.0451   0.0487   1.0000
  19.250   1.1502   0.16288   0.15813  -0.0556   0.0505   1.0000
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