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GOE 382 AIRFOIL (goe382-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 382 AIRFOIL (goe382-il)
Reynolds number: 500,000
Max Cl/Cd: 86.98 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe382-il-500000.txt
Download as CSV file: xf-goe382-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 382 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.1080   0.11776   0.11493  -0.0705   0.8383   0.0397
 -12.250  -0.1009   0.11517   0.11227  -0.0712   0.8227   0.0403
 -12.000  -0.1292   0.10506   0.10211  -0.0786   0.8140   0.0435
 -11.750  -0.1176   0.10335   0.10032  -0.0782   0.7971   0.0437
 -11.500  -0.1063   0.10159   0.09847  -0.0783   0.7804   0.0440
 -11.250  -0.0360   0.08696   0.08369  -0.0896   0.7254   0.0486
 -11.000  -0.0242   0.08523   0.08189  -0.0890   0.7151   0.0489
 -10.750  -0.0140   0.08323   0.07985  -0.0890   0.7058   0.0491
 -10.500  -0.0049   0.08111   0.07766  -0.0892   0.6982   0.0495
 -10.250   0.0025   0.07862   0.07516  -0.0897   0.6911   0.0500
 -10.000  -0.0947   0.07930   0.07584  -0.0903   0.7099   0.0497
  -9.750  -0.3742   0.03225   0.02682  -0.1128   0.7162   0.0388
  -9.500  -0.3604   0.03057   0.02486  -0.1117   0.7073   0.0387
  -9.250  -0.3431   0.02934   0.02338  -0.1107   0.6993   0.0385
  -9.000  -0.3247   0.02715   0.02105  -0.1102   0.6919   0.0383
  -8.750  -0.3061   0.02548   0.01916  -0.1094   0.6849   0.0382
  -8.500  -0.2857   0.02411   0.01757  -0.1086   0.6788   0.0382
  -8.250  -0.2638   0.02290   0.01618  -0.1080   0.6728   0.0382
  -8.000  -0.2411   0.02189   0.01498  -0.1074   0.6672   0.0382
  -7.750  -0.2174   0.02105   0.01395  -0.1069   0.6620   0.0383
  -7.500  -0.1927   0.02026   0.01306  -0.1065   0.6573   0.0384
  -7.250  -0.1677   0.01947   0.01215  -0.1062   0.6524   0.0386
  -7.000  -0.1428   0.01845   0.01103  -0.1059   0.6477   0.0388
  -6.750  -0.1176   0.01770   0.01022  -0.1056   0.6431   0.0392
  -6.500  -0.0917   0.01712   0.00965  -0.1054   0.6392   0.0397
  -6.250  -0.0657   0.01664   0.00916  -0.1051   0.6348   0.0402
  -6.000  -0.0398   0.01620   0.00866  -0.1048   0.6304   0.0406
  -5.750  -0.0139   0.01581   0.00820  -0.1045   0.6262   0.0410
  -5.500   0.0122   0.01544   0.00779  -0.1042   0.6224   0.0414
  -5.250   0.0383   0.01505   0.00739  -0.1039   0.6185   0.0418
  -5.000   0.0643   0.01471   0.00702  -0.1036   0.6143   0.0423
  -4.750   0.0904   0.01442   0.00667  -0.1032   0.6102   0.0427
  -4.500   0.1169   0.01422   0.00639  -0.1030   0.6061   0.0432
  -4.250   0.1424   0.01384   0.00602  -0.1026   0.6025   0.0438
  -4.000   0.1683   0.01353   0.00573  -0.1023   0.5985   0.0447
  -3.750   0.1948   0.01330   0.00550  -0.1020   0.5942   0.0457
  -3.500   0.2216   0.01315   0.00529  -0.1018   0.5901   0.0470
  -3.250   0.2488   0.01306   0.00514  -0.1017   0.5859   0.0484
  -3.000   0.2754   0.01283   0.00496  -0.1015   0.5822   0.0503
  -2.750   0.3025   0.01269   0.00483  -0.1013   0.5778   0.0527
  -2.500   0.3296   0.01256   0.00471  -0.1012   0.5734   0.0561
  -2.250   0.3569   0.01251   0.00464  -0.1011   0.5689   0.0625
  -2.000   0.3841   0.01241   0.00456  -0.1010   0.5649   0.0738
  -1.750   0.4104   0.01219   0.00437  -0.1007   0.5604   0.0864
  -1.500   0.4357   0.01187   0.00426  -0.1004   0.5557   0.1339
  -1.250   0.4624   0.01181   0.00420  -0.1003   0.5509   0.1619
  -1.000   0.4891   0.01172   0.00417  -0.1001   0.5462   0.1814
  -0.750   0.5153   0.01155   0.00414  -0.1000   0.5413   0.2135
  -0.500   0.5408   0.01133   0.00412  -0.0997   0.5363   0.2816
  -0.250   0.5663   0.01121   0.00410  -0.0995   0.5313   0.3407
   0.000   0.5912   0.01093   0.00410  -0.0991   0.5261   0.4162
   0.250   0.6138   0.01055   0.00416  -0.0984   0.5204   0.5622
   0.500   0.6384   0.01047   0.00420  -0.0978   0.5151   0.6250
   0.750   0.6633   0.01039   0.00428  -0.0973   0.5098   0.6760
   1.000   0.6879   0.01031   0.00436  -0.0967   0.5041   0.7263
   1.250   0.7105   0.01023   0.00445  -0.0955   0.4985   0.7922
   1.500   0.7330   0.01022   0.00460  -0.0943   0.4930   0.8537
   1.750   0.7572   0.01026   0.00473  -0.0933   0.4869   0.8986
   2.000   0.7850   0.01042   0.00486  -0.0932   0.4811   0.9345
   2.250   0.8201   0.01061   0.00502  -0.0948   0.4754   0.9602
   2.500   0.8583   0.01079   0.00517  -0.0971   0.4694   0.9764
   2.750   0.9009   0.01105   0.00532  -0.1005   0.4633   0.9872
   3.000   0.9451   0.01127   0.00549  -0.1042   0.4574   0.9945
   3.250   0.9902   0.01148   0.00565  -0.1082   0.4512   1.0000
   3.500   1.0039   0.01164   0.00574  -0.1057   0.4465   1.0000
   3.750   1.0189   0.01181   0.00586  -0.1035   0.4422   1.0000
   4.000   1.0355   0.01193   0.00598  -0.1015   0.4380   1.0000
   4.250   1.0516   0.01209   0.00611  -0.0995   0.4337   1.0000
   4.500   1.0675   0.01231   0.00626  -0.0974   0.4294   1.0000
   4.750   1.0842   0.01253   0.00644  -0.0955   0.4252   1.0000
   5.000   1.1021   0.01269   0.00661  -0.0939   0.4213   1.0000
   5.250   1.1208   0.01291   0.00681  -0.0925   0.4171   1.0000
   5.500   1.1399   0.01319   0.00703  -0.0912   0.4132   1.0000
   5.750   1.1603   0.01352   0.00730  -0.0903   0.4092   1.0000
   6.000   1.1810   0.01374   0.00756  -0.0894   0.4061   1.0000
   6.250   1.2019   0.01400   0.00783  -0.0885   0.4025   1.0000
   6.500   1.2223   0.01430   0.00811  -0.0877   0.3988   1.0000
   6.750   1.2422   0.01467   0.00843  -0.0868   0.3951   1.0000
   7.000   1.2632   0.01503   0.00876  -0.0861   0.3914   1.0000
   7.250   1.2834   0.01534   0.00912  -0.0853   0.3883   1.0000
   7.500   1.3038   0.01568   0.00947  -0.0846   0.3851   1.0000
   7.750   1.3238   0.01605   0.00984  -0.0838   0.3819   1.0000
   8.000   1.3434   0.01648   0.01024  -0.0830   0.3786   1.0000
   8.250   1.3644   0.01692   0.01064  -0.0825   0.3751   1.0000
   8.500   1.3832   0.01732   0.01110  -0.0817   0.3725   1.0000
   8.750   1.4018   0.01776   0.01158  -0.0809   0.3693   1.0000
   9.000   1.4205   0.01822   0.01206  -0.0801   0.3662   1.0000
   9.250   1.4390   0.01872   0.01255  -0.0793   0.3633   1.0000
   9.500   1.4582   0.01924   0.01304  -0.0787   0.3601   1.0000
   9.750   1.4769   0.01976   0.01359  -0.0780   0.3573   1.0000
  10.000   1.4927   0.02036   0.01426  -0.0770   0.3542   1.0000
  10.250   1.5081   0.02100   0.01494  -0.0761   0.3505   1.0000
  10.500   1.5231   0.02170   0.01564  -0.0751   0.3468   1.0000
  10.750   1.5394   0.02238   0.01627  -0.0743   0.3428   1.0000
  11.000   1.5537   0.02315   0.01712  -0.0734   0.3398   1.0000
  11.250   1.5674   0.02397   0.01801  -0.0725   0.3364   1.0000
  11.500   1.5805   0.02486   0.01894  -0.0715   0.3326   1.0000
  11.750   1.5926   0.02581   0.01987  -0.0705   0.3286   1.0000
  12.000   1.6047   0.02680   0.02087  -0.0696   0.3246   1.0000
  12.250   1.6159   0.02791   0.02207  -0.0688   0.3209   1.0000
  12.500   1.6270   0.02905   0.02327  -0.0679   0.3170   1.0000
  12.750   1.6370   0.03029   0.02450  -0.0671   0.3132   1.0000
  13.000   1.6478   0.03146   0.02567  -0.0662   0.3094   1.0000
  13.250   1.6578   0.03283   0.02715  -0.0656   0.3060   1.0000
  13.500   1.6674   0.03422   0.02861  -0.0649   0.3021   1.0000
  13.750   1.6753   0.03576   0.03016  -0.0642   0.2982   1.0000
  14.000   1.6828   0.03728   0.03166  -0.0633   0.2943   1.0000
  14.250   1.6914   0.03889   0.03339  -0.0629   0.2909   1.0000
  14.500   1.6982   0.04067   0.03524  -0.0623   0.2866   1.0000
  14.750   1.7023   0.04265   0.03724  -0.0616   0.2821   1.0000
  15.000   1.7063   0.04464   0.03925  -0.0609   0.2778   1.0000
  15.250   1.7115   0.04668   0.04139  -0.0605   0.2733   1.0000
  15.500   1.7140   0.04892   0.04367  -0.0600   0.2684   1.0000
  15.750   1.7133   0.05142   0.04616  -0.0592   0.2636   1.0000
  16.000   1.7174   0.05363   0.04848  -0.0589   0.2592   1.0000
  16.250   1.7178   0.05617   0.05107  -0.0585   0.2538   1.0000
  16.500   1.7131   0.05921   0.05411  -0.0579   0.2484   1.0000
  16.750   1.7134   0.06185   0.05685  -0.0576   0.2427   1.0000
  17.000   1.7077   0.06509   0.06010  -0.0571   0.2364   1.0000
  17.250   1.7028   0.06831   0.06338  -0.0568   0.2303   1.0000
  17.500   1.6947   0.07194   0.06704  -0.0565   0.2231   1.0000
  17.750   1.6868   0.07555   0.07069  -0.0562   0.2161   1.0000
  18.000   1.6732   0.07986   0.07503  -0.0560   0.2080   1.0000
  18.250   1.6614   0.08405   0.07926  -0.0559   0.1999   1.0000
  18.500   1.6427   0.08912   0.08432  -0.0558   0.1914   1.0000
  18.750   1.6268   0.09390   0.08913  -0.0559   0.1820   1.0000
  19.000   1.6094   0.09892   0.09416  -0.0562   0.1731   1.0000
  19.250   1.5886   0.10447   0.09971  -0.0566   0.1647   1.0000
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