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GOE 386 AIRFOIL (goe386-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 386 AIRFOIL (goe386-il)
Reynolds number: 1,000,000
Max Cl/Cd: 103.65 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe386-il-1000000.txt
Download as CSV file: xf-goe386-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.8856   0.08149   0.07830  -0.0874   1.0000   0.0426
 -18.500  -0.9125   0.07415   0.07082  -0.0923   1.0000   0.0427
 -18.250  -0.9377   0.06748   0.06402  -0.0967   1.0000   0.0429
 -18.000  -0.9607   0.06163   0.05807  -0.1002   1.0000   0.0432
 -17.750  -0.9760   0.05665   0.05301  -0.1033   1.0000   0.0434
 -17.500  -0.9883   0.05192   0.04822  -0.1063   1.0000   0.0436
 -17.250  -0.9977   0.04753   0.04375  -0.1092   1.0000   0.0438
 -17.000  -1.0046   0.04347   0.03962  -0.1119   1.0000   0.0440
 -16.750  -1.0107   0.03988   0.03596  -0.1140   1.0000   0.0442
 -16.500  -1.0143   0.03674   0.03275  -0.1159   0.9990   0.0444
 -16.250  -0.9970   0.03394   0.02988  -0.1202   0.9952   0.0447
 -16.000  -0.9776   0.03158   0.02746  -0.1241   0.9913   0.0451
 -15.750  -0.9612   0.02959   0.02539  -0.1267   0.9827   0.0454
 -15.500  -0.9452   0.02789   0.02361  -0.1285   0.9728   0.0458
 -15.250  -0.9335   0.02645   0.02207  -0.1289   0.9605   0.0461
 -15.000  -0.9242   0.02528   0.02080  -0.1282   0.9480   0.0464
 -14.750  -0.9135   0.02428   0.01971  -0.1272   0.9375   0.0466
 -14.500  -0.9019   0.02345   0.01876  -0.1259   0.9278   0.0469
 -14.250  -0.8878   0.02273   0.01795  -0.1248   0.9191   0.0471
 -14.000  -0.8731   0.02214   0.01726  -0.1233   0.9104   0.0473
 -13.750  -0.8660   0.02109   0.01614  -0.1211   0.9022   0.0478
 -13.500  -0.8494   0.02043   0.01543  -0.1199   0.8943   0.0482
 -13.250  -0.8297   0.01994   0.01490  -0.1189   0.8874   0.0486
 -13.000  -0.8082   0.01950   0.01443  -0.1182   0.8803   0.0490
 -12.750  -0.7863   0.01912   0.01400  -0.1174   0.8727   0.0493
 -12.500  -0.7637   0.01873   0.01356  -0.1167   0.8655   0.0497
 -12.250  -0.7405   0.01836   0.01315  -0.1161   0.8571   0.0502
 -12.000  -0.7171   0.01803   0.01274  -0.1154   0.8480   0.0507
 -11.750  -0.6929   0.01769   0.01234  -0.1149   0.8385   0.0512
 -11.500  -0.6690   0.01738   0.01193  -0.1142   0.8270   0.0517
 -11.250  -0.6443   0.01708   0.01156  -0.1137   0.8134   0.0520
 -11.000  -0.6222   0.01656   0.01093  -0.1128   0.7967   0.0525
 -10.750  -0.6000   0.01610   0.01039  -0.1120   0.7742   0.0531
 -10.500  -0.5767   0.01589   0.01005  -0.1111   0.7444   0.0535
 -10.250  -0.5529   0.01575   0.00977  -0.1103   0.7088   0.0540
 -10.000  -0.5288   0.01564   0.00951  -0.1096   0.6783   0.0545
  -9.750  -0.5040   0.01549   0.00925  -0.1090   0.6564   0.0550
  -9.250  -0.4526   0.01516   0.00875  -0.1081   0.6288   0.0562
  -9.000  -0.4265   0.01504   0.00853  -0.1077   0.6180   0.0568
  -8.750  -0.3992   0.01491   0.00834  -0.1074   0.6111   0.0573
  -8.500  -0.3753   0.01443   0.00782  -0.1068   0.6041   0.0580
  -8.250  -0.3498   0.01421   0.00755  -0.1063   0.5966   0.0587
  -8.000  -0.3225   0.01400   0.00734  -0.1061   0.5925   0.0592
  -7.750  -0.2953   0.01382   0.00714  -0.1059   0.5877   0.0599
  -7.500  -0.2682   0.01367   0.00695  -0.1056   0.5827   0.0606
  -7.250  -0.2414   0.01354   0.00677  -0.1053   0.5771   0.0613
  -7.000  -0.2137   0.01340   0.00659  -0.1051   0.5733   0.0620
  -6.750  -0.1853   0.01329   0.00645  -0.1050   0.5697   0.0626
  -6.500  -0.1590   0.01298   0.00612  -0.1046   0.5654   0.0634
  -6.250  -0.1326   0.01273   0.00584  -0.1043   0.5611   0.0642
  -6.000  -0.1057   0.01260   0.00568  -0.1040   0.5560   0.0650
  -5.750  -0.0780   0.01246   0.00553  -0.1038   0.5526   0.0658
  -5.500  -0.0498   0.01230   0.00537  -0.1037   0.5500   0.0666
  -5.250  -0.0215   0.01217   0.00522  -0.1036   0.5472   0.0675
  -5.000   0.0068   0.01208   0.00511  -0.1035   0.5440   0.0683
  -4.750   0.0347   0.01197   0.00496  -0.1034   0.5408   0.0690
  -4.500   0.0608   0.01169   0.00467  -0.1030   0.5372   0.0702
  -4.250   0.0880   0.01159   0.00454  -0.1027   0.5328   0.0711
  -4.000   0.1165   0.01144   0.00440  -0.1027   0.5309   0.0721
  -3.750   0.1450   0.01131   0.00428  -0.1026   0.5285   0.0732
  -3.500   0.1735   0.01121   0.00417  -0.1026   0.5258   0.0743
  -3.250   0.2020   0.01115   0.00409  -0.1025   0.5229   0.0751
  -3.000   0.2292   0.01095   0.00387  -0.1023   0.5197   0.0765
  -2.750   0.2566   0.01085   0.00375  -0.1021   0.5161   0.0779
  -2.500   0.2843   0.01080   0.00367  -0.1019   0.5123   0.0791
  -2.250   0.3131   0.01069   0.00358  -0.1019   0.5106   0.0805
  -2.000   0.3418   0.01061   0.00351  -0.1020   0.5083   0.0818
  -1.750   0.3701   0.01048   0.00338  -0.1019   0.5057   0.0838
  -1.500   0.3983   0.01038   0.00329  -0.1018   0.5029   0.0859
  -1.250   0.4264   0.01032   0.00322  -0.1017   0.5001   0.0880
  -1.000   0.4542   0.01028   0.00317  -0.1016   0.4969   0.0908
  -0.750   0.4815   0.01024   0.00313  -0.1014   0.4931   0.0969
  -0.500   0.5087   0.00996   0.00310  -0.1013   0.4911   0.1521
  -0.250   0.5374   0.00988   0.00310  -0.1013   0.4887   0.1700
   0.000   0.5659   0.00983   0.00310  -0.1014   0.4856   0.1828
   0.250   0.5941   0.00981   0.00310  -0.1013   0.4820   0.1930
   0.500   0.6217   0.00981   0.00311  -0.1012   0.4781   0.2037
   0.750   0.6487   0.00984   0.00316  -0.1010   0.4736   0.2156
   1.000   0.6774   0.00980   0.00317  -0.1010   0.4709   0.2280
   1.250   0.7057   0.00975   0.00319  -0.1011   0.4674   0.2455
   1.500   0.7334   0.00971   0.00321  -0.1010   0.4629   0.2677
   1.750   0.7601   0.00968   0.00326  -0.1008   0.4579   0.2996
   2.000   0.7869   0.00963   0.00332  -0.1006   0.4530   0.3399
   2.250   0.8145   0.00954   0.00337  -0.1006   0.4475   0.3874
   2.500   0.8405   0.00948   0.00343  -0.1002   0.4400   0.4444
   2.750   0.8660   0.00936   0.00352  -0.0999   0.4325   0.5270
   3.000   0.8905   0.00918   0.00363  -0.0994   0.4225   0.6425
   3.250   0.9127   0.00900   0.00379  -0.0982   0.4114   0.7752
   3.500   0.9318   0.00899   0.00399  -0.0963   0.3965   0.8764
   3.750   0.9510   0.00918   0.00422  -0.0944   0.3787   0.9404
   4.000   0.9808   0.00954   0.00448  -0.0949   0.3603   0.9765
   4.250   1.0185   0.00993   0.00476  -0.0972   0.3454   0.9936
   4.500   1.0520   0.01027   0.00502  -0.0987   0.3348   1.0000
   4.750   1.0675   0.01049   0.00518  -0.0964   0.3280   1.0000
   5.000   1.0839   0.01070   0.00535  -0.0942   0.3226   1.0000
   5.250   1.1006   0.01097   0.00558  -0.0921   0.3173   1.0000
   5.500   1.1201   0.01122   0.00580  -0.0907   0.3129   1.0000
   5.750   1.1419   0.01142   0.00599  -0.0897   0.3100   1.0000
   6.000   1.1631   0.01167   0.00622  -0.0886   0.3064   1.0000
   6.250   1.1831   0.01198   0.00650  -0.0874   0.3025   1.0000
   6.500   1.2013   0.01238   0.00685  -0.0859   0.2977   1.0000
   6.750   1.2242   0.01261   0.00709  -0.0853   0.2954   1.0000
   7.000   1.2469   0.01286   0.00734  -0.0846   0.2931   1.0000
   7.250   1.2686   0.01315   0.00763  -0.0838   0.2906   1.0000
   7.500   1.2894   0.01348   0.00796  -0.0829   0.2882   1.0000
   7.750   1.3090   0.01389   0.00834  -0.0818   0.2855   1.0000
   8.000   1.3270   0.01437   0.00880  -0.0806   0.2822   1.0000
   8.250   1.3460   0.01481   0.00925  -0.0796   0.2797   1.0000
   8.500   1.3682   0.01512   0.00958  -0.0790   0.2785   1.0000
   8.750   1.3900   0.01546   0.00994  -0.0784   0.2768   1.0000
   9.000   1.4108   0.01585   0.01034  -0.0777   0.2749   1.0000
   9.250   1.4304   0.01630   0.01080  -0.0769   0.2727   1.0000
   9.500   1.4490   0.01682   0.01131  -0.0760   0.2703   1.0000
   9.750   1.4653   0.01746   0.01195  -0.0748   0.2677   1.0000
  10.000   1.4797   0.01822   0.01270  -0.0735   0.2647   1.0000
  10.250   1.4988   0.01875   0.01326  -0.0728   0.2632   1.0000
  10.500   1.5192   0.01921   0.01375  -0.0722   0.2617   1.0000
  10.750   1.5389   0.01971   0.01429  -0.0717   0.2599   1.0000
  11.000   1.5567   0.02034   0.01493  -0.0709   0.2579   1.0000
  11.250   1.5734   0.02103   0.01564  -0.0701   0.2558   1.0000
  11.500   1.5885   0.02185   0.01647  -0.0691   0.2538   1.0000
  11.750   1.6016   0.02281   0.01744  -0.0680   0.2516   1.0000
  12.000   1.6117   0.02396   0.01859  -0.0667   0.2490   1.0000
  12.250   1.6278   0.02476   0.01943  -0.0660   0.2476   1.0000
  12.500   1.6450   0.02551   0.02024  -0.0654   0.2464   1.0000
  12.750   1.6607   0.02638   0.02115  -0.0648   0.2448   1.0000
  13.000   1.6762   0.02728   0.02209  -0.0642   0.2430   1.0000
  13.250   1.6890   0.02840   0.02324  -0.0635   0.2410   1.0000
  13.500   1.7004   0.02964   0.02450  -0.0627   0.2386   1.0000
  13.750   1.7079   0.03123   0.02610  -0.0617   0.2358   1.0000
  14.000   1.7151   0.03288   0.02776  -0.0608   0.2331   1.0000
  14.250   1.7303   0.03391   0.02886  -0.0604   0.2316   1.0000
  14.500   1.7431   0.03518   0.03018  -0.0600   0.2297   1.0000
  14.750   1.7542   0.03656   0.03160  -0.0595   0.2274   1.0000
  15.000   1.7618   0.03830   0.03337  -0.0589   0.2247   1.0000
  15.250   1.7660   0.04037   0.03546  -0.0582   0.2217   1.0000
  15.500   1.7698   0.04247   0.03759  -0.0575   0.2187   1.0000
  15.750   1.7808   0.04397   0.03915  -0.0572   0.2167   1.0000
  16.000   1.7900   0.04559   0.04082  -0.0568   0.2141   1.0000
  16.250   1.7942   0.04772   0.04298  -0.0564   0.2111   1.0000
  16.500   1.7948   0.05019   0.04547  -0.0558   0.2076   1.0000
  16.750   1.7964   0.05260   0.04791  -0.0553   0.2045   1.0000
  17.000   1.8043   0.05437   0.04974  -0.0550   0.2015   1.0000
  17.250   1.8056   0.05683   0.05223  -0.0546   0.1977   1.0000
  17.500   1.8009   0.05988   0.05529  -0.0540   0.1933   1.0000
  17.750   1.8031   0.06227   0.05773  -0.0537   0.1895   1.0000
  18.000   1.8030   0.06490   0.06038  -0.0534   0.1845   1.0000
  18.250   1.7935   0.06857   0.06406  -0.0530   0.1793   1.0000
  18.500   1.7946   0.07110   0.06663  -0.0528   0.1745   1.0000
  18.750   1.7841   0.07494   0.07047  -0.0526   0.1687   1.0000
  19.000   1.7792   0.07819   0.07376  -0.0525   0.1635   1.0000
  19.250   1.7681   0.08216   0.07774  -0.0524   0.1576   1.0000
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