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GOE 386 AIRFOIL (goe386-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 386 AIRFOIL (goe386-il)
Reynolds number: 500,000
Max Cl/Cd: 88.74 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe386-il-500000.txt
Download as CSV file: xf-goe386-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 386 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.6886   0.05692   0.05327  -0.1073   0.9950   0.0531
 -14.500  -0.7081   0.04834   0.04442  -0.1185   0.9906   0.0533
 -14.250  -0.7059   0.04406   0.04000  -0.1243   0.9845   0.0536
 -14.000  -0.6953   0.04107   0.03689  -0.1285   0.9792   0.0540
 -13.750  -0.6898   0.03850   0.03420  -0.1309   0.9702   0.0543
 -13.500  -0.6834   0.03629   0.03184  -0.1323   0.9617   0.0547
 -13.250  -0.6836   0.03452   0.02991  -0.1313   0.9495   0.0550
 -13.000  -0.6845   0.03304   0.02827  -0.1291   0.9380   0.0554
 -12.500  -0.6757   0.03031   0.02514  -0.1251   0.9178   0.0564
 -12.250  -0.6668   0.02915   0.02372  -0.1233   0.9091   0.0570
 -12.000  -0.6558   0.02802   0.02240  -0.1216   0.8994   0.0575
 -11.750  -0.6361   0.02695   0.02130  -0.1208   0.8913   0.0580
 -11.500  -0.6153   0.02632   0.02066  -0.1200   0.8822   0.0585
 -11.250  -0.5945   0.02573   0.02001  -0.1191   0.8725   0.0589
 -11.000  -0.5732   0.02511   0.01933  -0.1183   0.8624   0.0595
 -10.750  -0.5520   0.02448   0.01861  -0.1174   0.8510   0.0600
 -10.500  -0.5309   0.02380   0.01783  -0.1165   0.8383   0.0607
 -10.250  -0.5099   0.02313   0.01699  -0.1156   0.8240   0.0614
 -10.000  -0.4889   0.02251   0.01618  -0.1145   0.8061   0.0621
  -9.750  -0.4677   0.02205   0.01549  -0.1134   0.7837   0.0627
  -9.500  -0.4459   0.02117   0.01446  -0.1126   0.7562   0.0634
  -9.250  -0.4230   0.02066   0.01383  -0.1118   0.7265   0.0640
  -9.000  -0.3999   0.02034   0.01337  -0.1110   0.7008   0.0647
  -8.750  -0.3763   0.02003   0.01293  -0.1102   0.6809   0.0655
  -8.500  -0.3520   0.01968   0.01246  -0.1096   0.6659   0.0662
  -8.250  -0.3274   0.01931   0.01197  -0.1090   0.6545   0.0671
  -8.000  -0.3027   0.01900   0.01151  -0.1085   0.6446   0.0679
  -7.750  -0.2774   0.01878   0.01114  -0.1079   0.6367   0.0686
  -7.500  -0.2520   0.01808   0.01041  -0.1076   0.6298   0.0694
  -7.250  -0.2264   0.01761   0.00994  -0.1072   0.6234   0.0703
  -7.000  -0.2004   0.01733   0.00960  -0.1069   0.6175   0.0713
  -6.750  -0.1738   0.01700   0.00927  -0.1066   0.6130   0.0724
  -6.500  -0.1472   0.01671   0.00893  -0.1063   0.6080   0.0733
  -6.250  -0.1206   0.01648   0.00861  -0.1059   0.6032   0.0743
  -6.000  -0.0937   0.01637   0.00839  -0.1056   0.5983   0.0750
  -5.750  -0.0680   0.01576   0.00781  -0.1053   0.5945   0.0762
  -5.500  -0.0416   0.01536   0.00746  -0.1050   0.5905   0.0774
  -5.250  -0.0150   0.01509   0.00719  -0.1047   0.5862   0.0786
  -5.000   0.0118   0.01487   0.00693  -0.1044   0.5819   0.0799
  -4.750   0.0388   0.01472   0.00670  -0.1041   0.5776   0.0810
  -4.500   0.0665   0.01461   0.00654  -0.1039   0.5741   0.0819
  -4.250   0.0922   0.01415   0.00613  -0.1035   0.5714   0.0834
  -4.000   0.1187   0.01386   0.00587  -0.1032   0.5677   0.0850
  -3.750   0.1456   0.01364   0.00565  -0.1029   0.5639   0.0866
  -3.500   0.1729   0.01349   0.00547  -0.1027   0.5605   0.0881
  -3.250   0.2006   0.01340   0.00533  -0.1025   0.5574   0.0894
  -3.000   0.2276   0.01322   0.00513  -0.1023   0.5536   0.0915
  -2.750   0.2546   0.01300   0.00495  -0.1021   0.5508   0.0938
  -2.500   0.2821   0.01284   0.00480  -0.1018   0.5472   0.0964
  -2.250   0.3095   0.01268   0.00467  -0.1016   0.5438   0.0997
  -2.000   0.3371   0.01255   0.00456  -0.1015   0.5408   0.1045
  -1.750   0.3644   0.01239   0.00449  -0.1013   0.5379   0.1207
  -1.500   0.3921   0.01232   0.00452  -0.1013   0.5347   0.1588
  -1.250   0.4203   0.01228   0.00456  -0.1012   0.5318   0.1786
  -1.000   0.4481   0.01221   0.00456  -0.1011   0.5290   0.1933
  -0.750   0.4760   0.01218   0.00456  -0.1010   0.5257   0.2043
  -0.500   0.5037   0.01212   0.00455  -0.1009   0.5224   0.2151
  -0.250   0.5316   0.01211   0.00454  -0.1008   0.5191   0.2258
   0.000   0.5594   0.01211   0.00455  -0.1007   0.5158   0.2375
   0.250   0.5876   0.01216   0.00461  -0.1007   0.5121   0.2496
   0.500   0.6149   0.01209   0.00462  -0.1005   0.5094   0.2643
   0.750   0.6420   0.01201   0.00464  -0.1003   0.5059   0.2851
   1.000   0.6688   0.01191   0.00465  -0.1001   0.5020   0.3162
   1.250   0.6952   0.01181   0.00466  -0.0998   0.4979   0.3577
   1.500   0.7216   0.01175   0.00472  -0.0995   0.4934   0.4097
   1.750   0.7471   0.01156   0.00478  -0.0991   0.4897   0.4801
   2.000   0.7713   0.01126   0.00485  -0.0985   0.4854   0.5893
   2.250   0.7931   0.01091   0.00496  -0.0972   0.4808   0.7273
   2.500   0.8127   0.01071   0.00510  -0.0951   0.4761   0.8510
   2.750   0.8395   0.01075   0.00527  -0.0943   0.4711   0.9316
   3.000   0.8809   0.01085   0.00539  -0.0969   0.4644   0.9708
   3.250   0.9234   0.01103   0.00548  -0.1000   0.4568   0.9897
   3.500   0.9724   0.01118   0.00560  -0.1044   0.4478   0.9986
   3.750   0.9939   0.01129   0.00565  -0.1033   0.4388   1.0000
   4.000   1.0106   0.01140   0.00572  -0.1011   0.4296   1.0000
   4.250   1.0246   0.01156   0.00580  -0.0985   0.4187   1.0000
   4.500   1.0409   0.01173   0.00591  -0.0963   0.4057   1.0000
   4.750   1.0554   0.01198   0.00607  -0.0938   0.3925   1.0000
   5.000   1.0672   0.01229   0.00628  -0.0909   0.3800   1.0000
   5.250   1.0812   0.01264   0.00654  -0.0884   0.3687   1.0000
   5.500   1.0976   0.01300   0.00684  -0.0865   0.3597   1.0000
   5.750   1.1135   0.01343   0.00718  -0.0846   0.3516   1.0000
   6.000   1.1314   0.01382   0.00753  -0.0831   0.3452   1.0000
   6.250   1.1505   0.01420   0.00788  -0.0818   0.3397   1.0000
   6.500   1.1676   0.01467   0.00829  -0.0803   0.3346   1.0000
   6.750   1.1853   0.01515   0.00872  -0.0789   0.3302   1.0000
   7.000   1.2062   0.01550   0.00909  -0.0780   0.3269   1.0000
   7.250   1.2257   0.01592   0.00951  -0.0770   0.3233   1.0000
   7.500   1.2437   0.01642   0.00997  -0.0758   0.3197   1.0000
   7.750   1.2597   0.01704   0.01054  -0.0743   0.3156   1.0000
   8.000   1.2788   0.01753   0.01102  -0.0734   0.3123   1.0000
   8.250   1.2985   0.01797   0.01150  -0.0725   0.3094   1.0000
   8.500   1.3174   0.01847   0.01201  -0.0716   0.3066   1.0000
   8.750   1.3351   0.01904   0.01257  -0.0706   0.3037   1.0000
   9.000   1.3515   0.01970   0.01320  -0.0694   0.3009   1.0000
   9.250   1.3679   0.02040   0.01386  -0.0683   0.2976   1.0000
   9.500   1.3864   0.02096   0.01446  -0.0675   0.2956   1.0000
   9.750   1.4043   0.02155   0.01509  -0.0666   0.2936   1.0000
  10.000   1.4220   0.02217   0.01574  -0.0658   0.2913   1.0000
  10.250   1.4388   0.02285   0.01645  -0.0649   0.2889   1.0000
  10.500   1.4548   0.02358   0.01720  -0.0640   0.2866   1.0000
  10.750   1.4701   0.02437   0.01797  -0.0630   0.2842   1.0000
  11.000   1.4854   0.02518   0.01876  -0.0620   0.2815   1.0000
  11.250   1.5014   0.02596   0.01956  -0.0612   0.2792   1.0000
  11.500   1.5161   0.02681   0.02048  -0.0603   0.2772   1.0000
  11.750   1.5305   0.02771   0.02143  -0.0595   0.2750   1.0000
  12.000   1.5448   0.02862   0.02239  -0.0587   0.2728   1.0000
  12.250   1.5581   0.02962   0.02342  -0.0579   0.2706   1.0000
  12.500   1.5714   0.03063   0.02444  -0.0571   0.2684   1.0000
  12.750   1.5844   0.03167   0.02547  -0.0562   0.2661   1.0000
  13.000   1.5996   0.03255   0.02634  -0.0555   0.2637   1.0000
  13.250   1.6115   0.03374   0.02763  -0.0548   0.2622   1.0000
  13.500   1.6230   0.03501   0.02896  -0.0542   0.2603   1.0000
  13.750   1.6346   0.03627   0.03029  -0.0536   0.2582   1.0000
  14.000   1.6455   0.03762   0.03169  -0.0530   0.2560   1.0000
  14.250   1.6562   0.03900   0.03311  -0.0525   0.2539   1.0000
  14.500   1.6664   0.04041   0.03452  -0.0519   0.2516   1.0000
  14.750   1.6792   0.04148   0.03557  -0.0512   0.2489   1.0000
  15.000   1.6876   0.04315   0.03733  -0.0508   0.2470   1.0000
  15.250   1.6945   0.04502   0.03930  -0.0504   0.2447   1.0000
  15.500   1.7010   0.04694   0.04129  -0.0501   0.2421   1.0000
  15.750   1.7072   0.04892   0.04333  -0.0498   0.2393   1.0000
  16.000   1.7136   0.05082   0.04524  -0.0495   0.2365   1.0000
  16.250   1.7226   0.05230   0.04668  -0.0490   0.2333   1.0000
  16.500   1.7250   0.05479   0.04930  -0.0488   0.2311   1.0000
  16.750   1.7281   0.05719   0.05181  -0.0487   0.2281   1.0000
  17.000   1.7315   0.05954   0.05421  -0.0486   0.2249   1.0000
  17.250   1.7334   0.06201   0.05668  -0.0484   0.2217   1.0000
  17.500   1.7368   0.06423   0.05893  -0.0482   0.2184   1.0000
  17.750   1.7362   0.06714   0.06196  -0.0482   0.2150   1.0000
  18.000   1.7368   0.06986   0.06475  -0.0483   0.2112   1.0000
  18.250   1.7345   0.07288   0.06777  -0.0483   0.2074   1.0000
  18.500   1.7341   0.07568   0.07062  -0.0483   0.2036   1.0000
  18.750   1.7308   0.07895   0.07399  -0.0485   0.1992   1.0000
  19.000   1.7268   0.08221   0.07726  -0.0486   0.1946   1.0000
  19.250   1.7206   0.08579   0.08089  -0.0488   0.1902   1.0000
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