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GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 410 AIRFOIL (goe410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.98 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe410-il-1000000.txt
Download as CSV file: xf-goe410-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 410 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.3411   0.08915   0.08516  -0.0151   1.0000   0.0327
 -19.500  -1.3550   0.08379   0.07972  -0.0175   1.0000   0.0331
 -19.250  -1.3670   0.07884   0.07469  -0.0197   1.0000   0.0335
 -19.000  -1.3782   0.07408   0.06985  -0.0216   1.0000   0.0339
 -18.750  -1.3866   0.06979   0.06548  -0.0233   1.0000   0.0344
 -18.500  -1.3931   0.06585   0.06145  -0.0248   1.0000   0.0348
 -18.250  -1.3986   0.06210   0.05761  -0.0261   1.0000   0.0352
 -18.000  -1.4010   0.05881   0.05424  -0.0272   1.0000   0.0357
 -17.750  -1.4120   0.05454   0.04990  -0.0287   1.0000   0.0364
 -17.500  -1.4201   0.05073   0.04602  -0.0298   1.0000   0.0370
 -17.250  -1.4259   0.04731   0.04253  -0.0308   1.0000   0.0375
 -17.000  -1.4302   0.04408   0.03925  -0.0316   1.0000   0.0385
 -16.750  -1.4315   0.04123   0.03632  -0.0322   1.0000   0.0393
 -16.500  -1.4298   0.03869   0.03371  -0.0327   1.0000   0.0401
 -16.250  -1.4321   0.03579   0.03076  -0.0333   1.0000   0.0413
 -16.000  -1.4323   0.03316   0.02809  -0.0336   1.0000   0.0428
 -15.750  -1.4292   0.03095   0.02583  -0.0338   1.0000   0.0443
 -15.500  -1.4260   0.02883   0.02367  -0.0337   1.0000   0.0462
 -15.250  -1.4223   0.02688   0.02170  -0.0335   1.0000   0.0486
 -15.000  -1.4157   0.02527   0.02005  -0.0330   1.0000   0.0511
 -14.750  -1.4096   0.02373   0.01851  -0.0324   1.0000   0.0542
 -14.500  -1.3999   0.02256   0.01731  -0.0315   1.0000   0.0569
 -14.250  -1.3916   0.02140   0.01615  -0.0305   1.0000   0.0596
 -14.000  -1.3791   0.02059   0.01531  -0.0294   1.0000   0.0621
 -13.750  -1.3684   0.01977   0.01445  -0.0279   1.0000   0.0642
 -13.500  -1.3578   0.01903   0.01371  -0.0262   1.0000   0.0663
 -13.250  -1.3445   0.01848   0.01314  -0.0246   1.0000   0.0682
 -13.000  -1.3290   0.01808   0.01269  -0.0230   1.0000   0.0696
 -12.750  -1.3181   0.01754   0.01213  -0.0206   1.0000   0.0711
 -12.500  -1.3069   0.01704   0.01162  -0.0182   1.0000   0.0729
 -12.250  -1.2896   0.01663   0.01121  -0.0167   1.0000   0.0746
 -12.000  -1.2697   0.01630   0.01085  -0.0156   1.0000   0.0762
 -11.750  -1.2484   0.01601   0.01053  -0.0146   1.0000   0.0774
 -11.500  -1.2287   0.01562   0.01011  -0.0134   1.0000   0.0788
 -11.250  -1.2100   0.01514   0.00963  -0.0121   1.0000   0.0806
 -11.000  -1.1890   0.01477   0.00926  -0.0111   1.0000   0.0823
 -10.750  -1.1669   0.01444   0.00893  -0.0102   1.0000   0.0837
 -10.500  -1.1438   0.01417   0.00863  -0.0094   1.0000   0.0852
 -10.250  -1.1203   0.01392   0.00835  -0.0086   1.0000   0.0863
 -10.000  -1.0983   0.01355   0.00797  -0.0077   1.0000   0.0878
  -9.750  -1.0764   0.01317   0.00760  -0.0067   1.0000   0.0898
  -9.500  -1.0534   0.01286   0.00729  -0.0059   1.0000   0.0915
  -9.250  -1.0300   0.01258   0.00702  -0.0051   1.0000   0.0932
  -9.000  -1.0061   0.01234   0.00677  -0.0043   1.0000   0.0948
  -8.750  -0.9819   0.01215   0.00655  -0.0036   1.0000   0.0960
  -8.500  -0.9600   0.01179   0.00622  -0.0025   1.0000   0.0991
  -8.250  -0.9301   0.01149   0.00596  -0.0030   0.9922   0.1019
  -8.000  -0.8884   0.01123   0.00571  -0.0059   0.9749   0.1051
  -7.750  -0.8448   0.01094   0.00540  -0.0092   0.9450   0.1087
  -7.500  -0.8172   0.01077   0.00515  -0.0089   0.8945   0.1128
  -7.250  -0.7934   0.01070   0.00495  -0.0079   0.8556   0.1162
  -7.000  -0.7683   0.01059   0.00475  -0.0072   0.8294   0.1194
  -6.750  -0.7433   0.01041   0.00453  -0.0065   0.8080   0.1244
  -6.500  -0.7172   0.01029   0.00436  -0.0060   0.7887   0.1285
  -6.250  -0.6905   0.01018   0.00418  -0.0056   0.7705   0.1319
  -6.000  -0.6645   0.00999   0.00396  -0.0051   0.7518   0.1373
  -5.750  -0.6378   0.00987   0.00379  -0.0047   0.7320   0.1416
  -5.500  -0.6105   0.00980   0.00365  -0.0044   0.7111   0.1444
  -5.250  -0.5843   0.00962   0.00342  -0.0040   0.6888   0.1506
  -5.000  -0.5575   0.00950   0.00325  -0.0036   0.6664   0.1556
  -4.750  -0.5302   0.00943   0.00309  -0.0033   0.6449   0.1599
  -4.500  -0.5035   0.00925   0.00290  -0.0030   0.6253   0.1685
  -3.750  -0.4265   0.00827   0.00225  -0.0017   0.5803   0.2690
  -3.500  -0.3997   0.00805   0.00213  -0.0014   0.5692   0.3006
  -3.250  -0.3720   0.00792   0.00204  -0.0012   0.5599   0.3215
  -3.000  -0.3442   0.00783   0.00196  -0.0010   0.5497   0.3386
  -2.750  -0.3160   0.00773   0.00190  -0.0009   0.5404   0.3541
  -2.500  -0.2879   0.00766   0.00184  -0.0007   0.5313   0.3681
  -2.250  -0.2594   0.00761   0.00181  -0.0006   0.5242   0.3808
  -2.000  -0.2306   0.00756   0.00177  -0.0006   0.5179   0.3935
  -1.750  -0.2022   0.00752   0.00175  -0.0004   0.5111   0.4041
  -1.500  -0.1732   0.00752   0.00173  -0.0004   0.5044   0.4125
  -1.250  -0.1446   0.00746   0.00171  -0.0003   0.4967   0.4232
  -1.000  -0.1158   0.00748   0.00170  -0.0002   0.4893   0.4328
  -0.750  -0.0869   0.00744   0.00170  -0.0002   0.4841   0.4428
  -0.500  -0.0577   0.00744   0.00169  -0.0001   0.4781   0.4507
  -0.250  -0.0291   0.00743   0.00169   0.0000   0.4717   0.4590
   0.000   0.0000   0.00743   0.00170   0.0000   0.4659   0.4659
   0.250   0.0291   0.00743   0.00169   0.0000   0.4589   0.4717
   0.500   0.0577   0.00744   0.00169   0.0001   0.4506   0.4781
   0.750   0.0869   0.00744   0.00170   0.0002   0.4427   0.4841
   1.000   0.1158   0.00748   0.00170   0.0002   0.4328   0.4893
   1.250   0.1446   0.00746   0.00171   0.0003   0.4232   0.4968
   1.500   0.1732   0.00752   0.00173   0.0004   0.4125   0.5043
   1.750   0.2022   0.00752   0.00175   0.0004   0.4041   0.5111
   2.000   0.2307   0.00756   0.00177   0.0006   0.3935   0.5179
   2.250   0.2594   0.00761   0.00181   0.0006   0.3809   0.5242
   2.500   0.2879   0.00767   0.00184   0.0007   0.3680   0.5312
   2.750   0.3161   0.00773   0.00190   0.0009   0.3541   0.5405
   3.000   0.3442   0.00783   0.00196   0.0010   0.3386   0.5497
   3.250   0.3720   0.00792   0.00204   0.0012   0.3215   0.5600
   3.500   0.3998   0.00805   0.00213   0.0014   0.3006   0.5692
   3.750   0.4265   0.00827   0.00225   0.0017   0.2689   0.5804
   4.500   0.5035   0.00925   0.00290   0.0030   0.1685   0.6252
   4.750   0.5302   0.00942   0.00309   0.0033   0.1600   0.6449
   5.000   0.5575   0.00950   0.00325   0.0036   0.1555   0.6662
   5.250   0.5843   0.00962   0.00342   0.0040   0.1506   0.6887
   5.500   0.6105   0.00980   0.00365   0.0044   0.1445   0.7110
   5.750   0.6378   0.00987   0.00379   0.0047   0.1416   0.7320
   6.000   0.6645   0.00999   0.00396   0.0051   0.1374   0.7520
   6.250   0.6905   0.01018   0.00418   0.0056   0.1320   0.7705
   6.500   0.7172   0.01029   0.00436   0.0060   0.1285   0.7888
   6.750   0.7434   0.01041   0.00453   0.0065   0.1245   0.8076
   7.000   0.7684   0.01059   0.00475   0.0071   0.1194   0.8293
   7.250   0.7934   0.01069   0.00495   0.0079   0.1162   0.8556
   7.500   0.8172   0.01077   0.00515   0.0089   0.1129   0.8943
   7.750   0.8448   0.01094   0.00540   0.0092   0.1087   0.9448
   8.000   0.8885   0.01123   0.00570   0.0059   0.1051   0.9750
   8.250   0.9302   0.01149   0.00595   0.0030   0.1018   0.9922
   8.500   0.9600   0.01179   0.00622   0.0025   0.0990   1.0000
   8.750   0.9819   0.01215   0.00655   0.0036   0.0961   1.0000
   9.000   1.0061   0.01234   0.00677   0.0043   0.0948   1.0000
   9.250   1.0300   0.01258   0.00702   0.0051   0.0932   1.0000
   9.500   1.0534   0.01285   0.00729   0.0059   0.0915   1.0000
   9.750   1.0764   0.01317   0.00760   0.0067   0.0897   1.0000
  10.000   1.0983   0.01355   0.00797   0.0077   0.0878   1.0000
  10.250   1.1202   0.01392   0.00835   0.0086   0.0862   1.0000
  10.500   1.1439   0.01416   0.00863   0.0094   0.0851   1.0000
  10.750   1.1669   0.01444   0.00893   0.0102   0.0837   1.0000
  11.000   1.1890   0.01476   0.00925   0.0111   0.0822   1.0000
  11.250   1.2100   0.01514   0.00963   0.0121   0.0806   1.0000
  11.500   1.2287   0.01562   0.01011   0.0134   0.0787   1.0000
  11.750   1.2485   0.01601   0.01052   0.0146   0.0774   1.0000
  12.000   1.2697   0.01630   0.01085   0.0156   0.0762   1.0000
  12.250   1.2897   0.01663   0.01121   0.0167   0.0747   1.0000
  12.500   1.3070   0.01703   0.01162   0.0182   0.0729   1.0000
  12.750   1.3182   0.01754   0.01212   0.0206   0.0711   1.0000
  13.000   1.3294   0.01807   0.01268   0.0229   0.0696   1.0000
  13.250   1.3449   0.01847   0.01313   0.0245   0.0681   1.0000
  13.500   1.3581   0.01903   0.01371   0.0262   0.0663   1.0000
  13.750   1.3688   0.01976   0.01445   0.0279   0.0642   1.0000
  14.000   1.3793   0.02060   0.01531   0.0293   0.0622   1.0000
  14.250   1.3921   0.02139   0.01613   0.0304   0.0596   1.0000
  14.500   1.4003   0.02256   0.01730   0.0315   0.0568   1.0000
  14.750   1.4105   0.02370   0.01848   0.0323   0.0542   1.0000
  15.000   1.4166   0.02523   0.02002   0.0329   0.0511   1.0000
  15.250   1.4234   0.02683   0.02165   0.0334   0.0487   1.0000
  15.500   1.4275   0.02876   0.02360   0.0336   0.0463   1.0000
  15.750   1.4306   0.03090   0.02577   0.0336   0.0442   1.0000
  16.000   1.4337   0.03312   0.02804   0.0335   0.0427   1.0000
  16.250   1.4337   0.03573   0.03070   0.0331   0.0413   1.0000
  16.500   1.4319   0.03859   0.03360   0.0325   0.0400   1.0000
  16.750   1.4335   0.04114   0.03623   0.0320   0.0392   1.0000
  17.000   1.4319   0.04405   0.03921   0.0313   0.0384   1.0000
  17.250   1.4284   0.04719   0.04241   0.0305   0.0376   1.0000
  17.500   1.4220   0.05068   0.04598   0.0296   0.0370   1.0000
  17.750   1.4146   0.05443   0.04979   0.0284   0.0364   1.0000
  18.000   1.4047   0.05858   0.05401   0.0270   0.0356   1.0000
  18.250   1.4019   0.06191   0.05742   0.0259   0.0352   1.0000
  18.500   1.3967   0.06562   0.06122   0.0246   0.0348   1.0000
  18.750   1.3900   0.06959   0.06527   0.0231   0.0344   1.0000
  19.000   1.3806   0.07400   0.06976   0.0213   0.0339   1.0000
  19.250   1.3703   0.07865   0.07449   0.0194   0.0335   1.0000
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