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SG6040 (sg6040-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SG6040 (sg6040-il)
Reynolds number: 100,000
Max Cl/Cd: 50.51 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sg6040-il-100000.txt
Download as CSV file: xf-sg6040-il-100000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.4430   0.10040   0.09530  -0.0615   1.0000   0.0846
 -11.250  -0.4337   0.09813   0.09303  -0.0598   1.0000   0.0828
 -11.000  -0.6278   0.07013   0.06472  -0.0747   1.0000   0.0627
 -10.750  -0.6465   0.06736   0.06197  -0.0723   1.0000   0.0623
 -10.500  -0.6686   0.06531   0.05994  -0.0687   1.0000   0.0619
 -10.250  -0.7004   0.06397   0.05860  -0.0636   1.0000   0.0617
 -10.000  -0.7269   0.06207   0.05665  -0.0591   1.0000   0.0614
  -9.750  -0.7479   0.05983   0.05431  -0.0552   1.0000   0.0609
  -9.500  -0.7669   0.05727   0.05161  -0.0515   1.0000   0.0605
  -9.250  -0.7823   0.05448   0.04861  -0.0482   1.0000   0.0601
  -9.000  -0.7934   0.05151   0.04539  -0.0452   1.0000   0.0598
  -8.750  -0.7995   0.04858   0.04214  -0.0425   1.0000   0.0596
  -8.500  -0.8010   0.04588   0.03909  -0.0402   1.0000   0.0602
  -8.250  -0.7982   0.04329   0.03610  -0.0381   1.0000   0.0610
  -8.000  -0.7915   0.04094   0.03330  -0.0363   1.0000   0.0619
  -7.750  -0.7713   0.03843   0.03028  -0.0365   0.9974   0.0629
  -7.500  -0.7375   0.03602   0.02779  -0.0388   0.9925   0.0648
  -7.250  -0.7041   0.03439   0.02601  -0.0408   0.9867   0.0676
  -7.000  -0.6681   0.03283   0.02413  -0.0428   0.9814   0.0716
  -6.750  -0.6371   0.03149   0.02285  -0.0442   0.9750   0.0779
  -6.500  -0.6010   0.03024   0.02156  -0.0464   0.9699   0.0878
  -6.250  -0.5734   0.02899   0.02037  -0.0470   0.9626   0.1023
  -6.000  -0.5371   0.02786   0.01933  -0.0495   0.9575   0.1298
  -5.750  -0.5127   0.02711   0.01858  -0.0498   0.9492   0.1562
  -5.500  -0.4751   0.02648   0.01806  -0.0527   0.9437   0.1880
  -5.250  -0.4521   0.02579   0.01758  -0.0527   0.9356   0.2129
  -5.000  -0.4165   0.02504   0.01704  -0.0548   0.9298   0.2481
  -4.750  -0.3921   0.02421   0.01656  -0.0550   0.9222   0.2930
  -4.500  -0.3654   0.02298   0.01624  -0.0556   0.9156   0.4101
  -4.250  -0.3384   0.02342   0.01721  -0.0546   0.9086   0.5424
  -4.000  -0.3119   0.02412   0.01783  -0.0536   0.9002   0.5910
  -3.750  -0.2715   0.02491   0.01850  -0.0546   0.8955   0.6251
  -3.500  -0.2579   0.02547   0.01903  -0.0514   0.8849   0.6439
  -3.250  -0.2209   0.02606   0.01955  -0.0517   0.8799   0.6644
  -3.000  -0.2060   0.02653   0.01996  -0.0490   0.8699   0.6803
  -2.750  -0.1720   0.02689   0.02025  -0.0489   0.8643   0.6978
  -2.500  -0.1536   0.02727   0.02056  -0.0468   0.8554   0.7131
  -2.250  -0.1247   0.02753   0.02074  -0.0461   0.8488   0.7293
  -2.000  -0.0861   0.02771   0.02086  -0.0464   0.8451   0.7463
  -1.750  -0.0828   0.02815   0.02132  -0.0415   0.8333   0.7577
  -1.500  -0.0477   0.02820   0.02131  -0.0412   0.8292   0.7738
  -1.250  -0.0411   0.02849   0.02157  -0.0374   0.8181   0.7862
  -1.000  -0.0060   0.02831   0.02130  -0.0380   0.8134   0.7996
  -0.750   0.0069   0.02850   0.02146  -0.0353   0.8039   0.8100
  -0.500   0.0377   0.02828   0.02118  -0.0354   0.7978   0.8193
  -0.250   0.0829   0.02784   0.02065  -0.0380   0.7949   0.8283
   0.000   0.0856   0.02814   0.02094  -0.0343   0.7826   0.8361
   0.250   0.1291   0.02767   0.02040  -0.0366   0.7792   0.8433
   0.500   0.1731   0.02724   0.01989  -0.0392   0.7756   0.8497
   0.750   0.1773   0.02751   0.02017  -0.0357   0.7637   0.8571
   1.000   0.2286   0.02694   0.01952  -0.0396   0.7612   0.8635
   1.250   0.2274   0.02737   0.01997  -0.0353   0.7485   0.8707
   1.500   0.2758   0.02680   0.01936  -0.0384   0.7454   0.8768
   1.750   0.3272   0.02614   0.01865  -0.0420   0.7431   0.8820
   2.000   0.3250   0.02670   0.01925  -0.0377   0.7299   0.8904
   2.250   0.3758   0.02601   0.01852  -0.0412   0.7273   0.8964
   2.500   0.3779   0.02659   0.01915  -0.0377   0.7147   0.9048
   2.750   0.4277   0.02591   0.01844  -0.0409   0.7116   0.9112
   3.250   0.4828   0.02583   0.01842  -0.0412   0.6961   0.9274
   3.500   0.5405   0.02508   0.01766  -0.0456   0.6932   0.9324
   3.750   0.5503   0.02576   0.01843  -0.0438   0.6810   0.9445
   4.000   0.6116   0.02502   0.01768  -0.0490   0.6774   0.9490
   4.250   0.6367   0.02557   0.01834  -0.0497   0.6663   0.9601
   4.500   0.6987   0.02490   0.01768  -0.0553   0.6615   0.9650
   4.750   0.7371   0.02525   0.01813  -0.0581   0.6514   0.9745
   5.000   0.7967   0.02466   0.01756  -0.0635   0.6449   0.9795
   5.250   0.8408   0.02483   0.01784  -0.0673   0.6341   0.9885
   5.500   0.9036   0.02399   0.01697  -0.0729   0.6266   0.9937
   5.750   0.9009   0.02448   0.01756  -0.0690   0.6150   1.0000
   6.000   0.9286   0.02400   0.01704  -0.0689   0.6071   1.0000
   6.250   0.9409   0.02412   0.01718  -0.0669   0.5958   1.0000
   6.500   0.9644   0.02422   0.01732  -0.0666   0.5842   1.0000
   6.750   1.0060   0.02371   0.01677  -0.0686   0.5735   1.0000
   7.000   1.0355   0.02358   0.01664  -0.0688   0.5607   1.0000
   7.250   1.0582   0.02368   0.01678  -0.0681   0.5469   1.0000
   7.500   1.0839   0.02367   0.01679  -0.0677   0.5332   1.0000
   7.750   1.1107   0.02361   0.01673  -0.0674   0.5192   1.0000
   8.000   1.1363   0.02354   0.01666  -0.0668   0.5044   1.0000
   8.250   1.1589   0.02353   0.01664  -0.0657   0.4884   1.0000
   8.500   1.1775   0.02358   0.01670  -0.0640   0.4713   1.0000
   8.750   1.1931   0.02370   0.01684  -0.0618   0.4533   1.0000
   9.000   1.2061   0.02388   0.01703  -0.0592   0.4341   1.0000
   9.250   1.2169   0.02410   0.01723  -0.0563   0.4142   1.0000
   9.500   1.2244   0.02439   0.01744  -0.0529   0.3936   1.0000
   9.750   1.2233   0.02500   0.01808  -0.0485   0.3713   1.0000
  10.000   1.2240   0.02569   0.01868  -0.0445   0.3471   1.0000
  10.250   1.2207   0.02670   0.01964  -0.0404   0.3204   1.0000
  10.500   1.2166   0.02796   0.02075  -0.0366   0.2929   1.0000
  10.750   1.2111   0.02953   0.02211  -0.0331   0.2657   1.0000
  11.000   1.2055   0.03137   0.02381  -0.0299   0.2393   1.0000
  11.250   1.2012   0.03338   0.02560  -0.0272   0.2164   1.0000
  11.500   1.1991   0.03544   0.02752  -0.0249   0.1962   1.0000
  11.750   1.1996   0.03750   0.02943  -0.0230   0.1789   1.0000
  12.000   1.2030   0.03949   0.03131  -0.0214   0.1640   1.0000
  12.250   1.2092   0.04142   0.03315  -0.0201   0.1510   1.0000
  12.500   1.2182   0.04327   0.03492  -0.0189   0.1398   1.0000
  12.750   1.2325   0.04492   0.03641  -0.0181   0.1297   1.0000
  13.000   1.2403   0.04683   0.03844  -0.0171   0.1220   1.0000
  13.250   1.2576   0.04851   0.04006  -0.0165   0.1145   1.0000
  13.500   1.2683   0.05038   0.04204  -0.0157   0.1085   1.0000
  13.750   1.2923   0.05202   0.04358  -0.0155   0.1023   1.0000
  14.000   1.2967   0.05431   0.04611  -0.0145   0.0983   1.0000
  14.250   1.3133   0.05608   0.04788  -0.0141   0.0939   1.0000
  14.500   1.3340   0.05835   0.05020  -0.0139   0.0899   1.0000
  14.750   1.3319   0.06116   0.05331  -0.0129   0.0876   1.0000
  15.000   1.3333   0.06394   0.05629  -0.0122   0.0851   1.0000
  15.250   1.3392   0.06657   0.05905  -0.0117   0.0828   1.0000
  15.500   1.3678   0.06918   0.06157  -0.0120   0.0796   1.0000
  15.750   1.3509   0.07305   0.06577  -0.0112   0.0789   1.0000
  16.000   1.3318   0.07741   0.07048  -0.0109   0.0783   1.0000
  16.250   1.3110   0.08229   0.07567  -0.0112   0.0777   1.0000
  16.500   1.2875   0.08778   0.08146  -0.0121   0.0773   1.0000
  16.750   1.2606   0.09409   0.08807  -0.0138   0.0771   1.0000
  17.000   1.2292   0.10147   0.09573  -0.0166   0.0772   1.0000
  17.250   1.1932   0.11019   0.10472  -0.0206   0.0776   1.0000
  17.500   1.1523   0.12062   0.11539  -0.0262   0.0783   1.0000
  17.750   1.1076   0.13306   0.12803  -0.0334   0.0792   1.0000
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