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GOE 386 AIRFOIL (goe386-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 386 AIRFOIL (goe386-il)
Reynolds number: 200,000
Max Cl/Cd: 61.72 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe386-il-200000.txt
Download as CSV file: xf-goe386-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.0530   0.10848   0.10466  -0.0830   0.9541   0.1077
 -10.750  -0.3217   0.05577   0.05136  -0.1265   0.9374   0.0896
 -10.500  -0.3236   0.05149   0.04696  -0.1280   0.9248   0.0887
 -10.250  -0.3437   0.04698   0.04221  -0.1274   0.9094   0.0880
 -10.000  -0.3681   0.04243   0.03727  -0.1254   0.8914   0.0873
  -9.750  -0.3784   0.03892   0.03336  -0.1232   0.8741   0.0873
  -9.500  -0.3790   0.03614   0.03017  -0.1210   0.8572   0.0877
  -9.250  -0.3729   0.03386   0.02746  -0.1190   0.8407   0.0883
  -9.000  -0.3616   0.03200   0.02517  -0.1173   0.8242   0.0888
  -8.750  -0.3468   0.03052   0.02326  -0.1157   0.8073   0.0893
  -8.500  -0.3278   0.02867   0.02124  -0.1147   0.7894   0.0900
  -8.250  -0.3056   0.02740   0.01984  -0.1140   0.7727   0.0909
  -8.000  -0.2819   0.02647   0.01880  -0.1134   0.7579   0.0921
  -7.750  -0.2582   0.02561   0.01774  -0.1128   0.7453   0.0934
  -7.500  -0.2355   0.02478   0.01672  -0.1121   0.7326   0.0946
  -7.250  -0.2114   0.02400   0.01564  -0.1114   0.7232   0.0958
  -7.000  -0.1877   0.02332   0.01475  -0.1107   0.7131   0.0967
  -6.750  -0.1620   0.02245   0.01372  -0.1104   0.7053   0.0979
  -6.500  -0.1359   0.02176   0.01306  -0.1102   0.6977   0.0994
  -6.250  -0.1099   0.02126   0.01252  -0.1098   0.6905   0.1012
  -6.000  -0.0831   0.02080   0.01193  -0.1096   0.6844   0.1029
  -5.750  -0.0567   0.02038   0.01140  -0.1092   0.6784   0.1045
  -5.500  -0.0305   0.01993   0.01088  -0.1088   0.6722   0.1059
  -5.250  -0.0041   0.01942   0.01043  -0.1086   0.6670   0.1079
  -5.000   0.0233   0.01915   0.01012  -0.1085   0.6626   0.1103
  -4.750   0.0499   0.01890   0.00984  -0.1082   0.6582   0.1128
  -4.500   0.0760   0.01861   0.00955  -0.1078   0.6535   0.1151
  -4.250   0.1020   0.01831   0.00931  -0.1074   0.6486   0.1178
  -4.000   0.1290   0.01813   0.00908  -0.1071   0.6435   0.1213
  -3.750   0.1561   0.01800   0.00890  -0.1069   0.6384   0.1254
  -3.500   0.1813   0.01782   0.00881  -0.1063   0.6331   0.1302
  -3.250   0.2078   0.01767   0.00868  -0.1060   0.6282   0.1363
  -3.000   0.2351   0.01754   0.00855  -0.1057   0.6236   0.1452
  -2.750   0.2632   0.01750   0.00850  -0.1056   0.6191   0.1597
  -2.500   0.2883   0.01737   0.00853  -0.1051   0.6143   0.1807
  -2.250   0.3145   0.01734   0.00854  -0.1047   0.6091   0.2051
  -2.000   0.3416   0.01731   0.00854  -0.1044   0.6046   0.2246
  -1.750   0.3698   0.01737   0.00856  -0.1044   0.6008   0.2412
  -1.500   0.3984   0.01747   0.00866  -0.1045   0.5972   0.2557
  -1.250   0.4239   0.01749   0.00876  -0.1041   0.5933   0.2682
  -1.000   0.4498   0.01752   0.00883  -0.1036   0.5888   0.2805
  -0.750   0.4764   0.01747   0.00885  -0.1033   0.5843   0.2927
  -0.500   0.5044   0.01748   0.00882  -0.1033   0.5801   0.3076
  -0.250   0.5331   0.01751   0.00886  -0.1034   0.5764   0.3242
   0.000   0.5583   0.01752   0.00900  -0.1029   0.5724   0.3440
   0.250   0.5826   0.01745   0.00909  -0.1022   0.5677   0.3712
   0.500   0.6076   0.01729   0.00913  -0.1017   0.5630   0.4150
   0.750   0.6328   0.01701   0.00912  -0.1012   0.5585   0.4932
   1.000   0.6563   0.01667   0.00924  -0.1001   0.5544   0.6303
   1.250   0.6730   0.01638   0.00955  -0.0971   0.5496   0.7865
   1.500   0.7069   0.01639   0.00979  -0.0973   0.5439   0.9045
   1.750   0.7580   0.01650   0.00982  -0.1014   0.5383   0.9610
   2.000   0.8233   0.01670   0.00982  -0.1086   0.5326   0.9875
   2.250   0.8718   0.01678   0.00992  -0.1129   0.5253   1.0000
   2.500   0.8906   0.01680   0.00987  -0.1113   0.5195   1.0000
   2.750   0.9134   0.01684   0.00975  -0.1103   0.5143   1.0000
   3.000   0.9295   0.01697   0.00988  -0.1082   0.5079   1.0000
   3.250   0.9467   0.01702   0.00990  -0.1062   0.5010   1.0000
   3.500   0.9687   0.01705   0.00980  -0.1050   0.4951   1.0000
   3.750   0.9860   0.01718   0.00991  -0.1030   0.4881   1.0000
   4.000   1.0028   0.01725   0.00995  -0.1009   0.4803   1.0000
   4.250   1.0263   0.01731   0.00985  -0.1000   0.4738   1.0000
   4.500   1.0394   0.01746   0.01006  -0.0973   0.4646   1.0000
   4.750   1.0594   0.01753   0.01002  -0.0958   0.4569   1.0000
   5.000   1.0760   0.01773   0.01019  -0.0938   0.4480   1.0000
   5.250   1.0941   0.01787   0.01027  -0.0921   0.4397   1.0000
   5.500   1.1127   0.01812   0.01045  -0.0905   0.4317   1.0000
   5.750   1.1294   0.01836   0.01066  -0.0886   0.4235   1.0000
   6.000   1.1504   0.01864   0.01080  -0.0874   0.4168   1.0000
   6.250   1.1653   0.01898   0.01117  -0.0853   0.4092   1.0000
   6.500   1.1837   0.01928   0.01137  -0.0838   0.4030   1.0000
   6.750   1.2011   0.01967   0.01171  -0.0822   0.3969   1.0000
   7.000   1.2161   0.02007   0.01211  -0.0802   0.3908   1.0000
   7.250   1.2362   0.02046   0.01240  -0.0791   0.3856   1.0000
   7.500   1.2570   0.02093   0.01280  -0.0782   0.3808   1.0000
   7.750   1.2730   0.02144   0.01335  -0.0766   0.3760   1.0000
   8.000   1.2917   0.02192   0.01382  -0.0754   0.3717   1.0000
   8.250   1.3161   0.02238   0.01416  -0.0752   0.3677   1.0000
   8.500   1.3379   0.02293   0.01468  -0.0746   0.3637   1.0000
   8.750   1.3521   0.02355   0.01537  -0.0729   0.3598   1.0000
   9.000   1.3699   0.02412   0.01595  -0.0717   0.3560   1.0000
   9.250   1.3912   0.02466   0.01645  -0.0711   0.3526   1.0000
   9.500   1.4228   0.02514   0.01680  -0.0720   0.3491   1.0000
   9.750   1.4373   0.02587   0.01760  -0.0705   0.3461   1.0000
  10.000   1.4481   0.02664   0.01846  -0.0686   0.3426   1.0000
  10.250   1.4628   0.02732   0.01918  -0.0672   0.3389   1.0000
  10.500   1.4826   0.02790   0.01972  -0.0665   0.3353   1.0000
  10.750   1.5173   0.02835   0.02003  -0.0678   0.3316   1.0000
  11.000   1.5242   0.02931   0.02111  -0.0656   0.3288   1.0000
  11.250   1.5294   0.03032   0.02224  -0.0633   0.3256   1.0000
  11.500   1.5400   0.03121   0.02317  -0.0617   0.3221   1.0000
  11.750   1.5576   0.03187   0.02382  -0.0609   0.3186   1.0000
  12.000   1.5876   0.03230   0.02415  -0.0615   0.3153   1.0000
  12.250   1.6018   0.03330   0.02521  -0.0604   0.3125   1.0000
  12.500   1.6011   0.03470   0.02677  -0.0579   0.3100   1.0000
  12.750   1.6052   0.03602   0.02821  -0.0560   0.3073   1.0000
  13.000   1.6147   0.03715   0.02940  -0.0547   0.3045   1.0000
  13.250   1.6315   0.03796   0.03022  -0.0540   0.3018   1.0000
  13.500   1.6592   0.03835   0.03056  -0.0544   0.2991   1.0000
  13.750   1.6847   0.03911   0.03129  -0.0546   0.2963   1.0000
  14.000   1.6677   0.04146   0.03387  -0.0512   0.2939   1.0000
  14.250   1.6575   0.04374   0.03633  -0.0488   0.2910   1.0000
  14.500   1.6569   0.04559   0.03828  -0.0473   0.2880   1.0000
  14.750   1.6698   0.04661   0.03932  -0.0466   0.2851   1.0000
  15.000   1.7007   0.04657   0.03919  -0.0470   0.2822   1.0000
  15.250   1.7156   0.04775   0.04039  -0.0465   0.2793   1.0000
  15.500   1.6774   0.05220   0.04514  -0.0435   0.2763   1.0000
  15.750   1.6531   0.05623   0.04936  -0.0418   0.2729   1.0000
  16.000   1.6542   0.05833   0.05153  -0.0411   0.2697   1.0000
  16.250   1.6806   0.05824   0.05139  -0.0410   0.2669   1.0000
  16.500   1.7304   0.05650   0.04949  -0.0417   0.2641   1.0000
  16.750   1.6462   0.06621   0.05966  -0.0394   0.2601   1.0000
  17.000   1.5929   0.07434   0.06805  -0.0392   0.2551   1.0000
  17.250   1.6150   0.07442   0.06810  -0.0390   0.2523   1.0000
  17.500   1.6631   0.07171   0.06526  -0.0388   0.2500   1.0000
  17.750   1.4478   0.10080   0.09504  -0.0422   0.2377   1.0000
  18.000   1.5051   0.09598   0.09014  -0.0411   0.2370   1.0000
  18.250   1.5661   0.09089   0.08493  -0.0401   0.2358   1.0000
  18.500   1.6324   0.08537   0.07923  -0.0392   0.2342   1.0000
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