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SG6040 (sg6040-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SG6040 (sg6040-il)
Reynolds number: 100,000
Max Cl/Cd: 50.91 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6040-il-100000-n5.txt
Download as CSV file: xf-sg6040-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6040                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.5328   0.09221   0.08646  -0.0668   1.0000   0.0287
 -13.250  -0.5779   0.08007   0.07417  -0.0741   1.0000   0.0283
 -13.000  -0.6099   0.07220   0.06614  -0.0785   1.0000   0.0280
 -12.750  -0.6375   0.06610   0.05987  -0.0811   1.0000   0.0278
 -12.500  -0.6609   0.06129   0.05488  -0.0823   1.0000   0.0278
 -12.250  -0.6804   0.05740   0.05083  -0.0824   1.0000   0.0277
 -12.000  -0.6992   0.05404   0.04730  -0.0816   1.0000   0.0278
 -11.750  -0.7164   0.05122   0.04432  -0.0800   1.0000   0.0280
 -11.500  -0.7317   0.04894   0.04190  -0.0777   1.0000   0.0280
 -11.250  -0.7490   0.04703   0.03986  -0.0744   1.0000   0.0283
 -11.000  -0.7674   0.04548   0.03819  -0.0703   1.0000   0.0284
 -10.750  -0.7895   0.04438   0.03698  -0.0651   1.0000   0.0286
 -10.500  -0.7993   0.04296   0.03540  -0.0616   0.9989   0.0288
 -10.250  -0.7784   0.04081   0.03307  -0.0636   0.9933   0.0297
 -10.000  -0.7566   0.03916   0.03133  -0.0651   0.9870   0.0309
  -9.750  -0.7322   0.03736   0.02934  -0.0667   0.9817   0.0320
  -9.500  -0.7099   0.03564   0.02739  -0.0675   0.9752   0.0330
  -9.250  -0.6819   0.03397   0.02548  -0.0690   0.9708   0.0342
  -9.000  -0.6625   0.03262   0.02413  -0.0691   0.9629   0.0352
  -8.750  -0.6349   0.03128   0.02273  -0.0705   0.9580   0.0368
  -8.500  -0.6150   0.03011   0.02143  -0.0703   0.9500   0.0387
  -8.250  -0.5882   0.02891   0.02019  -0.0715   0.9447   0.0418
  -8.000  -0.5665   0.02793   0.01912  -0.0714   0.9374   0.0455
  -7.750  -0.5410   0.02689   0.01808  -0.0722   0.9314   0.0506
  -7.500  -0.5103   0.02581   0.01698  -0.0738   0.9277   0.0588
  -7.250  -0.4926   0.02504   0.01622  -0.0727   0.9187   0.0682
  -7.000  -0.4617   0.02425   0.01537  -0.0740   0.9143   0.0840
  -6.750  -0.4355   0.02353   0.01471  -0.0745   0.9086   0.0998
  -6.500  -0.4109   0.02294   0.01416  -0.0747   0.9016   0.1174
  -6.250  -0.3780   0.02230   0.01351  -0.0763   0.8977   0.1392
  -6.000  -0.3531   0.02170   0.01296  -0.0764   0.8913   0.1572
  -5.750  -0.3281   0.02107   0.01240  -0.0764   0.8845   0.1772
  -5.500  -0.2965   0.02036   0.01176  -0.0777   0.8804   0.2045
  -5.250  -0.2753   0.01976   0.01127  -0.0770   0.8726   0.2345
  -5.000  -0.2493   0.01900   0.01072  -0.0773   0.8665   0.2819
  -4.750  -0.2190   0.01816   0.01021  -0.0783   0.8625   0.3550
  -4.500  -0.2013   0.01782   0.01022  -0.0766   0.8534   0.4273
  -4.000  -0.1394   0.01773   0.01025  -0.0770   0.8433   0.5318
  -3.750  -0.1159   0.01782   0.01025  -0.0761   0.8349   0.5573
  -3.500  -0.0830   0.01784   0.01017  -0.0766   0.8301   0.5795
  -3.250  -0.0568   0.01795   0.01019  -0.0760   0.8228   0.5974
  -3.000  -0.0291   0.01804   0.01021  -0.0756   0.8160   0.6138
  -2.750   0.0043   0.01809   0.01017  -0.0762   0.8115   0.6300
  -2.500   0.0257   0.01826   0.01028  -0.0747   0.8026   0.6443
  -2.250   0.0558   0.01832   0.01025  -0.0747   0.7967   0.6593
  -2.000   0.0822   0.01845   0.01037  -0.0739   0.7900   0.6698
  -1.750   0.1077   0.01849   0.01034  -0.0732   0.7822   0.6799
  -1.500   0.1403   0.01842   0.01019  -0.0737   0.7772   0.6885
  -1.250   0.1619   0.01845   0.01017  -0.0726   0.7680   0.6961
  -1.000   0.1922   0.01838   0.01004  -0.0728   0.7620   0.7019
  -0.750   0.2176   0.01834   0.00993  -0.0725   0.7540   0.7086
  -0.500   0.2457   0.01827   0.00979  -0.0725   0.7468   0.7138
  -0.250   0.2742   0.01821   0.00969  -0.0724   0.7402   0.7185
   0.000   0.2990   0.01820   0.00964  -0.0720   0.7318   0.7241
   0.250   0.3321   0.01806   0.00940  -0.0730   0.7262   0.7295
   0.500   0.3530   0.01812   0.00950  -0.0717   0.7168   0.7337
   0.750   0.3837   0.01803   0.00935  -0.0721   0.7105   0.7384
   1.000   0.4078   0.01807   0.00937  -0.0717   0.7019   0.7441
   1.250   0.4368   0.01801   0.00928  -0.0718   0.6949   0.7484
   1.500   0.4613   0.01805   0.00933  -0.0712   0.6867   0.7528
   1.750   0.4891   0.01804   0.00930  -0.0712   0.6792   0.7581
   2.000   0.5163   0.01806   0.00929  -0.0712   0.6714   0.7636
   2.250   0.5416   0.01808   0.00934  -0.0707   0.6633   0.7677
   2.500   0.5686   0.01810   0.00936  -0.0705   0.6559   0.7729
   2.750   0.5942   0.01816   0.00943  -0.0703   0.6471   0.7790
   3.000   0.6214   0.01818   0.00946  -0.0701   0.6399   0.7837
   3.250   0.6448   0.01828   0.00960  -0.0693   0.6309   0.7891
   3.500   0.6733   0.01832   0.00962  -0.0695   0.6237   0.7955
   3.750   0.6957   0.01844   0.00982  -0.0685   0.6146   0.8013
   4.000   0.7236   0.01848   0.00987  -0.0685   0.6074   0.8075
   4.250   0.7466   0.01864   0.01009  -0.0678   0.5981   0.8145
   4.500   0.7733   0.01869   0.01018  -0.0675   0.5908   0.8208
   4.750   0.7951   0.01887   0.01044  -0.0665   0.5815   0.8292
   5.000   0.8211   0.01894   0.01053  -0.0661   0.5739   0.8367
   5.250   0.8423   0.01912   0.01082  -0.0650   0.5642   0.8462
   5.500   0.8658   0.01921   0.01096  -0.0641   0.5554   0.8549
   5.750   0.8876   0.01933   0.01114  -0.0630   0.5451   0.8658
   6.000   0.9069   0.01946   0.01138  -0.0614   0.5343   0.8788
   6.250   0.9291   0.01950   0.01146  -0.0602   0.5235   0.8936
   6.500   0.9493   0.01961   0.01166  -0.0588   0.5113   0.9133
   6.750   0.9735   0.01976   0.01192  -0.0584   0.4980   0.9410
   7.000   1.0021   0.01992   0.01215  -0.0591   0.4838   1.0000
   7.250   1.0234   0.02021   0.01242  -0.0583   0.4698   1.0000
   7.500   1.0435   0.02051   0.01272  -0.0574   0.4555   1.0000
   7.750   1.0619   0.02086   0.01305  -0.0561   0.4408   1.0000
   8.000   1.0777   0.02122   0.01341  -0.0543   0.4258   1.0000
   8.250   1.0915   0.02165   0.01383  -0.0523   0.4101   1.0000
   8.500   1.1036   0.02216   0.01435  -0.0500   0.3931   1.0000
   8.750   1.1143   0.02274   0.01493  -0.0477   0.3749   1.0000
   9.000   1.1238   0.02342   0.01559  -0.0453   0.3549   1.0000
   9.250   1.1319   0.02419   0.01631  -0.0428   0.3339   1.0000
   9.500   1.1384   0.02510   0.01716  -0.0403   0.3119   1.0000
   9.750   1.1437   0.02614   0.01815  -0.0378   0.2883   1.0000
  10.000   1.1471   0.02738   0.01929  -0.0353   0.2651   1.0000
  10.250   1.1496   0.02877   0.02059  -0.0330   0.2408   1.0000
  10.500   1.1502   0.03038   0.02209  -0.0307   0.2191   1.0000
  10.750   1.1514   0.03208   0.02373  -0.0287   0.1990   1.0000
  11.000   1.1523   0.03392   0.02550  -0.0269   0.1814   1.0000
  11.250   1.1530   0.03587   0.02740  -0.0253   0.1657   1.0000
  11.500   1.1539   0.03789   0.02940  -0.0239   0.1522   1.0000
  11.750   1.1548   0.04001   0.03149  -0.0226   0.1406   1.0000
  12.000   1.1546   0.04230   0.03375  -0.0215   0.1306   1.0000
  12.250   1.1571   0.04445   0.03594  -0.0206   0.1209   1.0000
  12.500   1.1585   0.04677   0.03829  -0.0199   0.1131   1.0000
  12.750   1.1594   0.04921   0.04075  -0.0193   0.1061   1.0000
  13.000   1.1618   0.05159   0.04317  -0.0187   0.0999   1.0000
  13.250   1.1634   0.05412   0.04575  -0.0184   0.0942   1.0000
  13.500   1.1650   0.05670   0.04835  -0.0181   0.0894   1.0000
  13.750   1.1687   0.05914   0.05087  -0.0179   0.0846   1.0000
  14.000   1.1697   0.06190   0.05366  -0.0179   0.0808   1.0000
  14.250   1.1739   0.06439   0.05622  -0.0178   0.0771   1.0000
  14.500   1.1779   0.06694   0.05887  -0.0178   0.0735   1.0000
  14.750   1.1804   0.06970   0.06167  -0.0180   0.0706   1.0000
  15.000   1.1845   0.07230   0.06429  -0.0181   0.0680   1.0000
  15.250   1.1894   0.07490   0.06705  -0.0183   0.0652   1.0000
  15.500   1.1930   0.07769   0.06992  -0.0187   0.0627   1.0000
  15.750   1.1961   0.08052   0.07280  -0.0192   0.0606   1.0000
  16.000   1.2008   0.08317   0.07548  -0.0195   0.0587   1.0000
  16.250   1.2044   0.08614   0.07864  -0.0200   0.0567   1.0000
  16.500   1.2073   0.08922   0.08186  -0.0207   0.0549   1.0000
  16.750   1.2098   0.09233   0.08506  -0.0215   0.0533   1.0000
  17.000   1.2127   0.09534   0.08811  -0.0224   0.0518   1.0000
  17.250   1.2171   0.09817   0.09098  -0.0230   0.0505   1.0000
  17.500   1.2155   0.10216   0.09523  -0.0244   0.0494   1.0000
  17.750   1.2130   0.10634   0.09961  -0.0260   0.0482   1.0000
  18.000   1.2099   0.11064   0.10409  -0.0278   0.0471   1.0000
  18.250   1.2068   0.11495   0.10855  -0.0297   0.0461   1.0000
  18.500   1.2046   0.11911   0.11281  -0.0317   0.0451   1.0000
  18.750   1.2054   0.12271   0.11648  -0.0334   0.0443   1.0000
  19.000   1.2090   0.12577   0.11954  -0.0348   0.0433   1.0000
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