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GOE 382 AIRFOIL (goe382-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 382 AIRFOIL (goe382-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.57 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe382-il-1000000.txt
Download as CSV file: xf-goe382-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.5711   0.04614   0.04304  -0.1151   0.8675   0.0267
 -13.500  -0.5976   0.04044   0.03704  -0.1194   0.8537   0.0266
 -13.250  -0.6094   0.03713   0.03352  -0.1205   0.8400   0.0266
 -13.000  -0.6144   0.03475   0.03094  -0.1203   0.8259   0.0267
 -12.750  -0.6146   0.03289   0.02889  -0.1192   0.8111   0.0268
 -12.500  -0.6122   0.03139   0.02722  -0.1175   0.7961   0.0268
 -12.250  -0.6048   0.03011   0.02580  -0.1160   0.7815   0.0270
 -12.000  -0.5923   0.02895   0.02450  -0.1150   0.7665   0.0271
 -11.750  -0.5773   0.02793   0.02334  -0.1141   0.7510   0.0272
 -11.500  -0.5617   0.02691   0.02217  -0.1132   0.7354   0.0274
 -11.250  -0.5450   0.02594   0.02104  -0.1123   0.7204   0.0275
 -11.000  -0.5272   0.02497   0.01993  -0.1115   0.7074   0.0277
 -10.750  -0.5081   0.02413   0.01895  -0.1108   0.6956   0.0279
 -10.500  -0.4880   0.02337   0.01805  -0.1101   0.6845   0.0282
 -10.250  -0.4674   0.02257   0.01712  -0.1094   0.6755   0.0284
 -10.000  -0.4465   0.02173   0.01613  -0.1088   0.6667   0.0286
  -9.750  -0.4248   0.02092   0.01518  -0.1081   0.6592   0.0287
  -9.500  -0.4022   0.02016   0.01430  -0.1076   0.6525   0.0289
  -9.250  -0.3791   0.01949   0.01350  -0.1071   0.6459   0.0290
  -9.000  -0.3551   0.01886   0.01276  -0.1066   0.6409   0.0291
  -8.750  -0.3306   0.01825   0.01207  -0.1062   0.6362   0.0293
  -8.500  -0.3057   0.01773   0.01146  -0.1059   0.6315   0.0294
  -8.250  -0.2807   0.01726   0.01089  -0.1055   0.6266   0.0296
  -8.000  -0.2550   0.01684   0.01039  -0.1052   0.6226   0.0297
  -7.750  -0.2288   0.01644   0.00994  -0.1050   0.6191   0.0298
  -7.500  -0.2024   0.01611   0.00955  -0.1048   0.6153   0.0299
  -7.250  -0.1787   0.01511   0.00850  -0.1043   0.6114   0.0302
  -7.000  -0.1542   0.01452   0.00787  -0.1038   0.6069   0.0305
  -6.750  -0.1286   0.01407   0.00740  -0.1035   0.6037   0.0308
  -6.500  -0.1022   0.01368   0.00702  -0.1033   0.6009   0.0312
  -6.250  -0.0756   0.01337   0.00670  -0.1031   0.5975   0.0316
  -6.000  -0.0491   0.01310   0.00639  -0.1029   0.5938   0.0320
  -5.750  -0.0227   0.01284   0.00609  -0.1027   0.5899   0.0323
  -5.500   0.0037   0.01261   0.00582  -0.1024   0.5860   0.0326
  -5.250   0.0309   0.01233   0.00553  -0.1023   0.5835   0.0329
  -5.000   0.0581   0.01208   0.00527  -0.1022   0.5803   0.0332
  -4.750   0.0853   0.01186   0.00503  -0.1020   0.5767   0.0335
  -4.500   0.1124   0.01169   0.00481  -0.1019   0.5730   0.0338
  -4.250   0.1394   0.01156   0.00463  -0.1017   0.5689   0.0340
  -4.000   0.1661   0.01127   0.00433  -0.1015   0.5658   0.0345
  -3.750   0.1933   0.01100   0.00407  -0.1014   0.5625   0.0351
  -3.500   0.2208   0.01081   0.00387  -0.1013   0.5586   0.0357
  -3.250   0.2482   0.01068   0.00371  -0.1012   0.5547   0.0364
  -3.000   0.2753   0.01059   0.00358  -0.1011   0.5503   0.0371
  -2.750   0.3034   0.01048   0.00346  -0.1011   0.5469   0.0380
  -2.500   0.3316   0.01035   0.00333  -0.1012   0.5429   0.0390
  -2.250   0.3592   0.01023   0.00321  -0.1011   0.5383   0.0406
  -2.000   0.3864   0.01017   0.00312  -0.1010   0.5335   0.0424
  -1.750   0.4140   0.01008   0.00305  -0.1010   0.5293   0.0466
  -1.500   0.4421   0.00997   0.00304  -0.1011   0.5249   0.0654
  -1.250   0.4700   0.00995   0.00302  -0.1011   0.5196   0.0743
  -1.000   0.4967   0.00993   0.00297  -0.1009   0.5138   0.0806
  -0.750   0.5248   0.00987   0.00292  -0.1010   0.5090   0.0863
  -0.500   0.5522   0.00980   0.00287  -0.1010   0.5034   0.0969
  -0.250   0.5780   0.00970   0.00290  -0.1008   0.4973   0.1474
   0.000   0.6056   0.00968   0.00290  -0.1009   0.4919   0.1607
   0.250   0.6329   0.00968   0.00291  -0.1008   0.4855   0.1711
   0.500   0.6587   0.00971   0.00294  -0.1006   0.4784   0.1879
   0.750   0.6850   0.00951   0.00297  -0.1005   0.4729   0.2623
   1.000   0.7106   0.00942   0.00302  -0.1003   0.4665   0.3258
   1.250   0.7350   0.00927   0.00308  -0.1000   0.4603   0.4150
   1.500   0.7592   0.00892   0.00319  -0.0996   0.4552   0.5763
   1.750   0.7846   0.00891   0.00328  -0.0993   0.4491   0.6260
   2.000   0.8090   0.00892   0.00340  -0.0988   0.4430   0.6770
   2.250   0.8344   0.00886   0.00351  -0.0985   0.4381   0.7361
   2.500   0.8583   0.00884   0.00365  -0.0978   0.4327   0.7948
   2.750   0.8806   0.00891   0.00382  -0.0968   0.4271   0.8493
   3.000   0.9036   0.00891   0.00397  -0.0957   0.4234   0.9057
   3.250   0.9284   0.00901   0.00413  -0.0950   0.4191   0.9492
   3.500   0.9621   0.00922   0.00431  -0.0965   0.4140   0.9751
   3.750   0.9985   0.00947   0.00450  -0.0987   0.4087   0.9878
   4.000   1.0383   0.00963   0.00465  -0.1015   0.4048   0.9949
   4.250   1.0793   0.00985   0.00483  -0.1046   0.4003   0.9995
   4.500   1.0954   0.01002   0.00496  -0.1026   0.3963   1.0000
   4.750   1.1044   0.01020   0.00511  -0.0991   0.3923   1.0000
   5.000   1.1240   0.01031   0.00522  -0.0977   0.3899   1.0000
   5.250   1.1444   0.01046   0.00537  -0.0965   0.3867   1.0000
   5.500   1.1648   0.01066   0.00555  -0.0954   0.3832   1.0000
   5.750   1.1845   0.01092   0.00578  -0.0943   0.3793   1.0000
   6.000   1.2038   0.01123   0.00605  -0.0932   0.3752   1.0000
   6.250   1.2279   0.01139   0.00623  -0.0928   0.3728   1.0000
   6.500   1.2507   0.01161   0.00645  -0.0923   0.3699   1.0000
   6.750   1.2726   0.01187   0.00670  -0.0917   0.3667   1.0000
   7.000   1.2932   0.01219   0.00701  -0.0909   0.3634   1.0000
   7.250   1.3117   0.01261   0.00739  -0.0899   0.3595   1.0000
   7.500   1.3347   0.01286   0.00766  -0.0895   0.3571   1.0000
   7.750   1.3578   0.01311   0.00793  -0.0892   0.3545   1.0000
   8.000   1.3792   0.01343   0.00826  -0.0886   0.3514   1.0000
   8.250   1.3993   0.01381   0.00864  -0.0880   0.3484   1.0000
   8.500   1.4177   0.01429   0.00910  -0.0871   0.3451   1.0000
   8.750   1.4360   0.01478   0.00959  -0.0862   0.3416   1.0000
   9.000   1.4588   0.01507   0.00991  -0.0860   0.3389   1.0000
   9.250   1.4792   0.01548   0.01033  -0.0854   0.3351   1.0000
   9.500   1.4970   0.01602   0.01086  -0.0846   0.3313   1.0000
   9.750   1.5122   0.01671   0.01153  -0.0835   0.3272   1.0000
  10.000   1.5315   0.01720   0.01206  -0.0830   0.3244   1.0000
  10.250   1.5522   0.01764   0.01252  -0.0826   0.3213   1.0000
  10.500   1.5697   0.01824   0.01314  -0.0819   0.3176   1.0000
  10.750   1.5839   0.01905   0.01393  -0.0809   0.3132   1.0000
  11.000   1.5984   0.01986   0.01475  -0.0800   0.3087   1.0000
  11.250   1.6172   0.02044   0.01537  -0.0796   0.3048   1.0000
  11.500   1.6324   0.02124   0.01619  -0.0788   0.3011   1.0000
  11.750   1.6448   0.02223   0.01717  -0.0778   0.2974   1.0000
  12.000   1.6563   0.02330   0.01826  -0.0768   0.2936   1.0000
  12.250   1.6737   0.02402   0.01902  -0.0764   0.2903   1.0000
  12.500   1.6872   0.02502   0.02005  -0.0757   0.2864   1.0000
  12.750   1.6975   0.02626   0.02129  -0.0747   0.2823   1.0000
  13.000   1.7059   0.02767   0.02272  -0.0737   0.2782   1.0000
  13.250   1.7207   0.02864   0.02373  -0.0732   0.2747   1.0000
  13.500   1.7311   0.02996   0.02508  -0.0725   0.2702   1.0000
  13.750   1.7353   0.03180   0.02693  -0.0714   0.2651   1.0000
  14.000   1.7457   0.03316   0.02832  -0.0708   0.2613   1.0000
  14.250   1.7550   0.03464   0.02984  -0.0701   0.2568   1.0000
  14.500   1.7579   0.03668   0.03189  -0.0692   0.2516   1.0000
  14.750   1.7628   0.03858   0.03381  -0.0684   0.2467   1.0000
  15.000   1.7681   0.04046   0.03573  -0.0676   0.2409   1.0000
  15.250   1.7638   0.04324   0.03850  -0.0665   0.2343   1.0000
  15.500   1.7673   0.04531   0.04061  -0.0658   0.2277   1.0000
  15.750   1.7601   0.04843   0.04371  -0.0647   0.2200   1.0000
  16.000   1.7589   0.05102   0.04633  -0.0639   0.2122   1.0000
  16.250   1.7489   0.05448   0.04979  -0.0629   0.2041   1.0000
  16.500   1.7389   0.05800   0.05331  -0.0619   0.1946   1.0000
  16.750   1.7281   0.06167   0.05697  -0.0610   0.1849   1.0000
  17.000   1.7118   0.06595   0.06125  -0.0601   0.1754   1.0000
  17.250   1.6927   0.07066   0.06594  -0.0593   0.1656   1.0000
  17.500   1.6765   0.07516   0.07045  -0.0587   0.1562   1.0000
  17.750   1.6594   0.07983   0.07513  -0.0583   0.1478   1.0000
  18.000   1.6403   0.08481   0.08012  -0.0579   0.1399   1.0000
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