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GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 600 AIRFOIL (goe600-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.58 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe600-il-1000000.txt
Download as CSV file: xf-goe600-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 600 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.9027   0.13128   0.12919  -0.0020   1.0000   0.0096
 -17.500  -0.9469   0.11778   0.11551  -0.0093   1.0000   0.0095
 -17.250  -0.9827   0.10651   0.10409  -0.0153   1.0000   0.0094
 -17.000  -1.0170   0.09587   0.09329  -0.0210   1.0000   0.0093
 -16.750  -1.0477   0.08624   0.08353  -0.0263   1.0000   0.0093
 -16.500  -1.0772   0.07731   0.07444  -0.0313   1.0000   0.0092
 -16.250  -1.1022   0.06926   0.06624  -0.0359   1.0000   0.0092
 -16.000  -1.1229   0.06205   0.05890  -0.0402   1.0000   0.0092
 -15.750  -1.1398   0.05559   0.05230  -0.0442   1.0000   0.0093
 -15.500  -1.1519   0.05001   0.04659  -0.0477   1.0000   0.0093
 -15.250  -1.1597   0.04523   0.04168  -0.0507   1.0000   0.0094
 -15.000  -1.1643   0.04104   0.03737  -0.0533   1.0000   0.0094
 -14.750  -1.1659   0.03748   0.03368  -0.0554   1.0000   0.0095
 -14.500  -1.1651   0.03451   0.03059  -0.0568   1.0000   0.0097
 -14.250  -1.1632   0.03201   0.02798  -0.0575   1.0000   0.0098
 -14.000  -1.1598   0.02998   0.02585  -0.0573   1.0000   0.0099
 -13.750  -1.1555   0.02831   0.02407  -0.0564   1.0000   0.0101
 -13.500  -1.1501   0.02694   0.02260  -0.0549   1.0000   0.0103
 -13.250  -1.1437   0.02580   0.02136  -0.0528   1.0000   0.0104
 -13.000  -1.1319   0.02476   0.02023  -0.0514   1.0000   0.0106
 -12.750  -1.1169   0.02384   0.01922  -0.0503   1.0000   0.0108
 -12.500  -1.0999   0.02302   0.01831  -0.0493   1.0000   0.0110
 -12.250  -1.0865   0.02181   0.01699  -0.0480   1.0000   0.0112
 -12.000  -1.0744   0.02044   0.01551  -0.0464   1.0000   0.0116
 -11.750  -1.0565   0.01959   0.01462  -0.0454   1.0000   0.0120
 -11.500  -1.0369   0.01893   0.01391  -0.0445   1.0000   0.0123
 -11.250  -1.0176   0.01836   0.01329  -0.0435   1.0000   0.0127
 -11.000  -1.0006   0.01786   0.01274  -0.0419   1.0000   0.0132
 -10.750  -0.9732   0.01729   0.01211  -0.0424   0.9980   0.0136
 -10.500  -0.9413   0.01676   0.01151  -0.0438   0.9955   0.0140
 -10.250  -0.9135   0.01564   0.01031  -0.0447   0.9916   0.0149
 -10.000  -0.8837   0.01504   0.00968  -0.0457   0.9864   0.0156
  -9.750  -0.8531   0.01454   0.00914  -0.0467   0.9816   0.0164
  -9.500  -0.8251   0.01411   0.00865  -0.0471   0.9740   0.0171
  -9.250  -0.7989   0.01357   0.00805  -0.0470   0.9660   0.0180
  -9.000  -0.7747   0.01309   0.00754  -0.0465   0.9567   0.0194
  -8.750  -0.7499   0.01278   0.00719  -0.0460   0.9476   0.0207
  -8.500  -0.7255   0.01247   0.00681  -0.0454   0.9391   0.0220
  -8.250  -0.7010   0.01204   0.00637  -0.0449   0.9305   0.0242
  -8.000  -0.6754   0.01180   0.00608  -0.0445   0.9230   0.0261
  -7.750  -0.6499   0.01142   0.00569  -0.0442   0.9149   0.0291
  -7.500  -0.6236   0.01123   0.00546  -0.0439   0.9075   0.0319
  -7.250  -0.5973   0.01091   0.00513  -0.0437   0.8993   0.0354
  -7.000  -0.5706   0.01072   0.00491  -0.0435   0.8916   0.0384
  -6.750  -0.5435   0.01049   0.00463  -0.0434   0.8831   0.0411
  -6.500  -0.5168   0.01021   0.00433  -0.0432   0.8751   0.0448
  -6.250  -0.4892   0.01003   0.00411  -0.0432   0.8662   0.0475
  -6.000  -0.4620   0.00978   0.00382  -0.0432   0.8576   0.0513
  -5.750  -0.4348   0.00953   0.00354  -0.0431   0.8480   0.0558
  -5.500  -0.4071   0.00931   0.00329  -0.0431   0.8379   0.0614
  -5.250  -0.3803   0.00895   0.00303  -0.0430   0.8275   0.0827
  -5.000  -0.3526   0.00875   0.00288  -0.0431   0.8163   0.1072
  -4.750  -0.3245   0.00860   0.00275  -0.0432   0.8053   0.1196
  -4.500  -0.2962   0.00848   0.00261  -0.0433   0.7950   0.1277
  -4.250  -0.2678   0.00840   0.00248  -0.0434   0.7851   0.1342
  -4.000  -0.2392   0.00830   0.00235  -0.0436   0.7759   0.1403
  -3.750  -0.2108   0.00819   0.00222  -0.0438   0.7676   0.1475
  -3.500  -0.1821   0.00809   0.00211  -0.0440   0.7590   0.1552
  -3.250  -0.1538   0.00797   0.00198  -0.0441   0.7506   0.1676
  -3.000  -0.1260   0.00768   0.00182  -0.0443   0.7422   0.2060
  -2.750  -0.0989   0.00724   0.00168  -0.0444   0.7352   0.2934
  -2.500  -0.0707   0.00702   0.00160  -0.0446   0.7285   0.3396
  -2.250  -0.0425   0.00687   0.00153  -0.0448   0.7220   0.3795
  -2.000  -0.0137   0.00671   0.00148  -0.0451   0.7160   0.4132
  -1.750   0.0148   0.00657   0.00144  -0.0453   0.7099   0.4512
  -1.500   0.0433   0.00646   0.00142  -0.0455   0.7042   0.4878
  -1.250   0.0723   0.00636   0.00141  -0.0457   0.6983   0.5180
  -1.000   0.1011   0.00632   0.00140  -0.0459   0.6928   0.5408
  -0.750   0.1302   0.00629   0.00139  -0.0462   0.6880   0.5592
  -0.500   0.1595   0.00624   0.00139  -0.0465   0.6829   0.5757
  -0.250   0.1885   0.00623   0.00139  -0.0467   0.6778   0.5914
   0.000   0.2175   0.00620   0.00140  -0.0469   0.6727   0.6092
   0.250   0.2467   0.00615   0.00141  -0.0472   0.6674   0.6256
   0.500   0.2756   0.00613   0.00141  -0.0474   0.6618   0.6429
   0.750   0.3045   0.00610   0.00143  -0.0477   0.6559   0.6620
   1.000   0.3332   0.00605   0.00144  -0.0478   0.6467   0.6849
   1.250   0.3617   0.00599   0.00146  -0.0479   0.6361   0.7112
   1.500   0.3899   0.00596   0.00148  -0.0480   0.6275   0.7405
   1.750   0.4182   0.00587   0.00153  -0.0480   0.6203   0.7763
   2.000   0.4455   0.00581   0.00158  -0.0479   0.6115   0.8166
   2.250   0.4720   0.00574   0.00164  -0.0474   0.5996   0.8618
   2.500   0.4974   0.00570   0.00171  -0.0467   0.5873   0.9051
   2.750   0.5227   0.00571   0.00177  -0.0459   0.5743   0.9394
   3.000   0.5513   0.00578   0.00183  -0.0459   0.5570   0.9630
   3.250   0.5838   0.00593   0.00189  -0.0469   0.5319   0.9792
   3.500   0.6184   0.00621   0.00200  -0.0486   0.4875   0.9901
   3.750   0.6545   0.00661   0.00218  -0.0507   0.4391   0.9964
   4.000   0.6891   0.00694   0.00237  -0.0525   0.4056   1.0000
   4.250   0.7126   0.00722   0.00252  -0.0518   0.3781   1.0000
   4.500   0.7367   0.00747   0.00267  -0.0511   0.3542   1.0000
   4.750   0.7613   0.00772   0.00282  -0.0506   0.3318   1.0000
   5.000   0.7861   0.00798   0.00299  -0.0502   0.3089   1.0000
   5.250   0.8113   0.00825   0.00317  -0.0498   0.2872   1.0000
   5.500   0.8364   0.00854   0.00336  -0.0495   0.2644   1.0000
   5.750   0.8612   0.00888   0.00359  -0.0491   0.2388   1.0000
   6.000   0.8855   0.00926   0.00384  -0.0486   0.2115   1.0000
   6.500   0.9342   0.01003   0.00439  -0.0478   0.1656   1.0000
   6.750   0.9580   0.01046   0.00470  -0.0473   0.1434   1.0000
   7.000   0.9816   0.01090   0.00502  -0.0468   0.1197   1.0000
   7.250   1.0042   0.01144   0.00541  -0.0461   0.0957   1.0000
   7.500   1.0278   0.01185   0.00576  -0.0456   0.0840   1.0000
   7.750   1.0519   0.01222   0.00610  -0.0451   0.0757   1.0000
   8.000   1.0753   0.01264   0.00647  -0.0445   0.0650   1.0000
   8.250   1.0949   0.01337   0.00700  -0.0434   0.0393   1.0000
   8.500   1.1159   0.01396   0.00754  -0.0425   0.0314   1.0000
   8.750   1.1385   0.01439   0.00799  -0.0418   0.0290   1.0000
   9.000   1.1592   0.01496   0.00856  -0.0408   0.0262   1.0000
   9.250   1.1809   0.01542   0.00906  -0.0400   0.0246   1.0000
   9.500   1.2025   0.01586   0.00953  -0.0392   0.0230   1.0000
   9.750   1.2215   0.01647   0.01015  -0.0380   0.0212   1.0000
  10.000   1.2405   0.01704   0.01077  -0.0368   0.0200   1.0000
  10.250   1.2603   0.01750   0.01126  -0.0357   0.0190   1.0000
  10.500   1.2782   0.01801   0.01180  -0.0343   0.0180   1.0000
  10.750   1.2919   0.01867   0.01249  -0.0323   0.0171   1.0000
  11.000   1.3025   0.01955   0.01343  -0.0299   0.0162   1.0000
  11.250   1.3192   0.02010   0.01402  -0.0285   0.0156   1.0000
  11.500   1.3347   0.02074   0.01471  -0.0271   0.0150   1.0000
  11.750   1.3497   0.02144   0.01544  -0.0257   0.0143   1.0000
  12.000   1.3626   0.02231   0.01635  -0.0242   0.0138   1.0000
  12.250   1.3697   0.02362   0.01773  -0.0221   0.0131   1.0000
  12.500   1.3796   0.02479   0.01897  -0.0205   0.0127   1.0000
  12.750   1.3923   0.02578   0.02003  -0.0193   0.0124   1.0000
  13.000   1.4036   0.02691   0.02122  -0.0181   0.0121   1.0000
  13.250   1.4141   0.02813   0.02251  -0.0170   0.0117   1.0000
  13.500   1.4239   0.02945   0.02388  -0.0159   0.0114   1.0000
  13.750   1.4327   0.03089   0.02540  -0.0149   0.0111   1.0000
  14.000   1.4395   0.03256   0.02713  -0.0139   0.0108   1.0000
  14.250   1.4421   0.03467   0.02931  -0.0128   0.0105   1.0000
  14.500   1.4370   0.03761   0.03235  -0.0117   0.0102   1.0000
  14.750   1.4377   0.04007   0.03491  -0.0110   0.0100   1.0000
  15.000   1.4435   0.04208   0.03701  -0.0106   0.0099   1.0000
  15.250   1.4474   0.04434   0.03936  -0.0103   0.0097   1.0000
  15.500   1.4499   0.04679   0.04190  -0.0101   0.0095   1.0000
  15.750   1.4504   0.04952   0.04473  -0.0100   0.0093   1.0000
  16.000   1.4500   0.05247   0.04777  -0.0100   0.0091   1.0000
  16.250   1.4480   0.05573   0.05113  -0.0103   0.0090   1.0000
  16.500   1.4449   0.05921   0.05471  -0.0108   0.0089   1.0000
  16.750   1.4407   0.06297   0.05856  -0.0115   0.0087   1.0000
  17.000   1.4348   0.06710   0.06280  -0.0125   0.0086   1.0000
  17.250   1.4276   0.07156   0.06736  -0.0137   0.0085   1.0000
  17.500   1.4192   0.07630   0.07221  -0.0152   0.0084   1.0000
  17.750   1.4084   0.08159   0.07760  -0.0170   0.0084   1.0000
  18.000   1.3966   0.08717   0.08330  -0.0191   0.0083   1.0000
  18.250   1.3831   0.09308   0.08932  -0.0214   0.0082   1.0000
  18.500   1.3683   0.09929   0.09563  -0.0239   0.0081   1.0000
  18.750   1.3529   0.10568   0.10213  -0.0266   0.0081   1.0000
  19.000   1.3373   0.11220   0.10876  -0.0294   0.0080   1.0000
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