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GOE 624 AIRFOIL (goe624-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 624 AIRFOIL (goe624-il)
Reynolds number: 500,000
Max Cl/Cd: 97.55 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe624-il-500000-n5.txt
Download as CSV file: xf-goe624-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 624 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7846   0.04559   0.04198  -0.0967   0.9709   0.0252
 -13.750  -0.7977   0.03868   0.03478  -0.1051   0.9437   0.0252
 -13.500  -0.8044   0.03555   0.03144  -0.1065   0.9229   0.0253
 -13.000  -0.8036   0.03195   0.02748  -0.1043   0.8923   0.0257
 -12.750  -0.7944   0.03048   0.02584  -0.1034   0.8818   0.0259
 -12.500  -0.7826   0.02910   0.02429  -0.1026   0.8721   0.0260
 -12.250  -0.7682   0.02783   0.02285  -0.1018   0.8638   0.0262
 -12.000  -0.7521   0.02667   0.02151  -0.1011   0.8554   0.0265
 -11.750  -0.7343   0.02559   0.02027  -0.1004   0.8479   0.0267
 -11.500  -0.7150   0.02459   0.01910  -0.0998   0.8400   0.0269
 -11.000  -0.6733   0.02282   0.01703  -0.0987   0.8265   0.0273
 -10.750  -0.6510   0.02205   0.01610  -0.0982   0.8199   0.0275
 -10.500  -0.6279   0.02138   0.01528  -0.0978   0.8139   0.0277
 -10.250  -0.6052   0.02052   0.01434  -0.0974   0.8075   0.0281
 -10.000  -0.5820   0.01977   0.01351  -0.0970   0.8007   0.0284
  -9.750  -0.5579   0.01916   0.01281  -0.0966   0.7945   0.0286
  -9.500  -0.5329   0.01856   0.01215  -0.0963   0.7880   0.0289
  -9.250  -0.5078   0.01802   0.01153  -0.0961   0.7817   0.0292
  -9.000  -0.4823   0.01751   0.01094  -0.0958   0.7753   0.0295
  -8.750  -0.4564   0.01702   0.01037  -0.0955   0.7669   0.0298
  -8.500  -0.4306   0.01657   0.00981  -0.0952   0.7585   0.0301
  -8.250  -0.4042   0.01612   0.00929  -0.0950   0.7490   0.0304
  -8.000  -0.3779   0.01572   0.00878  -0.0948   0.7396   0.0308
  -7.750  -0.3512   0.01532   0.00830  -0.0946   0.7294   0.0312
  -7.500  -0.3243   0.01497   0.00785  -0.0944   0.7210   0.0315
  -7.250  -0.2970   0.01464   0.00744  -0.0943   0.7130   0.0318
  -7.000  -0.2704   0.01422   0.00697  -0.0942   0.7053   0.0324
  -6.750  -0.2431   0.01386   0.00658  -0.0941   0.6971   0.0330
  -6.500  -0.2156   0.01358   0.00623  -0.0940   0.6894   0.0336
  -6.250  -0.1878   0.01330   0.00591  -0.0940   0.6826   0.0342
  -6.000  -0.1599   0.01305   0.00559  -0.0939   0.6752   0.0348
  -5.750  -0.1320   0.01283   0.00530  -0.0939   0.6683   0.0355
  -5.500  -0.1038   0.01262   0.00503  -0.0939   0.6607   0.0361
  -5.250  -0.0760   0.01238   0.00475  -0.0938   0.6537   0.0371
  -5.000  -0.0477   0.01217   0.00451  -0.0939   0.6475   0.0382
  -4.750  -0.0194   0.01198   0.00429  -0.0939   0.6411   0.0396
  -4.250   0.0373   0.01164   0.00389  -0.0940   0.6290   0.0442
  -4.000   0.0656   0.01147   0.00372  -0.0940   0.6222   0.0491
  -3.750   0.0939   0.01134   0.00359  -0.0940   0.6159   0.0572
  -3.500   0.1226   0.01122   0.00349  -0.0942   0.6096   0.0659
  -3.250   0.1512   0.01114   0.00340  -0.0942   0.6033   0.0729
  -3.000   0.1797   0.01107   0.00332  -0.0943   0.5975   0.0785
  -2.750   0.2087   0.01101   0.00324  -0.0945   0.5913   0.0831
  -2.500   0.2372   0.01094   0.00316  -0.0945   0.5844   0.0881
  -2.250   0.2658   0.01090   0.00309  -0.0946   0.5778   0.0929
  -2.000   0.2944   0.01082   0.00302  -0.0947   0.5700   0.0983
  -1.750   0.3227   0.01080   0.00296  -0.0948   0.5627   0.1044
  -1.500   0.3514   0.01073   0.00291  -0.0949   0.5552   0.1110
  -1.250   0.3796   0.01070   0.00286  -0.0950   0.5474   0.1188
  -1.000   0.4081   0.01064   0.00283  -0.0951   0.5396   0.1307
  -0.750   0.4360   0.01059   0.00280  -0.0951   0.5305   0.1491
  -0.500   0.4640   0.01051   0.00280  -0.0952   0.5214   0.1787
  -0.250   0.4916   0.01047   0.00280  -0.0952   0.5117   0.2101
   0.000   0.5196   0.01041   0.00281  -0.0953   0.5027   0.2421
   0.250   0.5470   0.01039   0.00284  -0.0953   0.4941   0.2786
   0.500   0.5747   0.01032   0.00288  -0.0954   0.4855   0.3238
   0.750   0.6016   0.01025   0.00294  -0.0953   0.4771   0.3841
   1.000   0.6285   0.01009   0.00300  -0.0953   0.4693   0.4717
   1.250   0.6544   0.00990   0.00310  -0.0951   0.4623   0.5812
   1.500   0.6797   0.00968   0.00321  -0.0947   0.4566   0.6943
   1.750   0.7030   0.00950   0.00334  -0.0936   0.4505   0.8057
   2.000   0.7245   0.00943   0.00350  -0.0918   0.4447   0.9181
   2.250   0.7647   0.00954   0.00361  -0.0943   0.4393   0.9774
   2.500   0.8064   0.00968   0.00371  -0.0974   0.4338   1.0000
   2.750   0.8312   0.00985   0.00381  -0.0969   0.4289   1.0000
   3.000   0.8566   0.01000   0.00391  -0.0964   0.4247   1.0000
   3.250   0.8827   0.01012   0.00401  -0.0962   0.4206   1.0000
   3.500   0.9083   0.01028   0.00413  -0.0958   0.4155   1.0000
   3.750   0.9332   0.01049   0.00427  -0.0954   0.4098   1.0000
   4.000   0.9593   0.01063   0.00440  -0.0951   0.4045   1.0000
   4.250   0.9850   0.01080   0.00453  -0.0948   0.3984   1.0000
   4.500   1.0098   0.01102   0.00469  -0.0944   0.3930   1.0000
   4.750   1.0358   0.01118   0.00484  -0.0942   0.3891   1.0000
   5.000   1.0619   0.01133   0.00500  -0.0940   0.3852   1.0000
   5.250   1.0874   0.01151   0.00516  -0.0937   0.3809   1.0000
   5.500   1.1121   0.01173   0.00535  -0.0933   0.3766   1.0000
   5.750   1.1372   0.01192   0.00554  -0.0929   0.3730   1.0000
   6.000   1.1628   0.01209   0.00572  -0.0927   0.3694   1.0000
   6.250   1.1878   0.01228   0.00592  -0.0923   0.3654   1.0000
   6.500   1.2119   0.01251   0.00613  -0.0919   0.3613   1.0000
   6.750   1.2352   0.01276   0.00637  -0.0913   0.3574   1.0000
   7.000   1.2600   0.01294   0.00659  -0.0909   0.3536   1.0000
   7.250   1.2838   0.01316   0.00682  -0.0904   0.3490   1.0000
   7.500   1.3057   0.01344   0.00709  -0.0896   0.3436   1.0000
   7.750   1.3276   0.01371   0.00736  -0.0888   0.3379   1.0000
   8.000   1.3480   0.01398   0.00764  -0.0877   0.3310   1.0000
   8.250   1.3655   0.01434   0.00798  -0.0861   0.3249   1.0000
   8.500   1.3863   0.01463   0.00830  -0.0852   0.3190   1.0000
   8.750   1.4038   0.01504   0.00870  -0.0838   0.3113   1.0000
   9.000   1.4221   0.01546   0.00912  -0.0826   0.3031   1.0000
   9.250   1.4379   0.01601   0.00964  -0.0811   0.2942   1.0000
   9.500   1.4560   0.01648   0.01013  -0.0799   0.2866   1.0000
  10.000   1.4877   0.01772   0.01136  -0.0773   0.2703   1.0000
  10.250   1.5014   0.01849   0.01211  -0.0758   0.2621   1.0000
  10.500   1.5156   0.01926   0.01288  -0.0745   0.2527   1.0000
  10.750   1.5276   0.02020   0.01380  -0.0730   0.2433   1.0000
  11.000   1.5374   0.02131   0.01488  -0.0714   0.2334   1.0000
  11.250   1.5497   0.02230   0.01588  -0.0701   0.2246   1.0000
  11.500   1.5597   0.02348   0.01705  -0.0687   0.2177   1.0000
  11.750   1.5720   0.02453   0.01813  -0.0676   0.2115   1.0000
  12.000   1.5805   0.02587   0.01948  -0.0663   0.2051   1.0000
  12.250   1.5902   0.02716   0.02079  -0.0651   0.1984   1.0000
  12.500   1.5965   0.02874   0.02237  -0.0637   0.1914   1.0000
  12.750   1.6043   0.03025   0.02390  -0.0626   0.1852   1.0000
  13.000   1.6102   0.03194   0.02561  -0.0614   0.1788   1.0000
  13.250   1.6152   0.03373   0.02743  -0.0603   0.1738   1.0000
  13.500   1.6227   0.03536   0.02910  -0.0593   0.1691   1.0000
  13.750   1.6270   0.03732   0.03110  -0.0584   0.1643   1.0000
  14.000   1.6304   0.03943   0.03324  -0.0575   0.1599   1.0000
  14.250   1.6366   0.04131   0.03518  -0.0567   0.1550   1.0000
  14.500   1.6380   0.04370   0.03760  -0.0559   0.1498   1.0000
  14.750   1.6403   0.04607   0.04002  -0.0553   0.1452   1.0000
  15.000   1.6432   0.04843   0.04242  -0.0547   0.1397   1.0000
  15.250   1.6405   0.05139   0.04541  -0.0541   0.1342   1.0000
  15.500   1.6416   0.05400   0.04808  -0.0537   0.1278   1.0000
  15.750   1.6371   0.05729   0.05138  -0.0532   0.1208   1.0000
  16.000   1.6312   0.06079   0.05490  -0.0529   0.1125   1.0000
  16.250   1.6229   0.06461   0.05873  -0.0526   0.1044   1.0000
  16.500   1.6129   0.06873   0.06287  -0.0525   0.0977   1.0000
  16.750   1.6042   0.07278   0.06695  -0.0525   0.0925   1.0000
  17.000   1.5952   0.07691   0.07112  -0.0526   0.0883   1.0000
  17.250   1.5877   0.08091   0.07518  -0.0528   0.0846   1.0000
  17.500   1.5774   0.08534   0.07966  -0.0531   0.0812   1.0000
  17.750   1.5721   0.08917   0.08356  -0.0535   0.0784   1.0000
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