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GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 648 AIRFOIL (goe648-il)
Reynolds number: 500,000
Max Cl/Cd: 79.75 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe648-il-500000.txt
Download as CSV file: xf-goe648-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 648 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7683   0.07572   0.07230  -0.0744   1.0000   0.0262
 -15.750  -0.8126   0.06522   0.06157  -0.0817   1.0000   0.0261
 -15.500  -0.8365   0.05862   0.05483  -0.0859   1.0000   0.0262
 -15.250  -0.8547   0.05321   0.04929  -0.0891   1.0000   0.0263
 -15.000  -0.8652   0.04919   0.04521  -0.0910   1.0000   0.0265
 -14.750  -0.8753   0.04551   0.04145  -0.0926   1.0000   0.0267
 -14.500  -0.8865   0.04205   0.03789  -0.0937   1.0000   0.0268
 -14.250  -0.8941   0.03944   0.03522  -0.0939   1.0000   0.0271
 -14.000  -0.9051   0.03702   0.03270  -0.0932   1.0000   0.0273
 -13.750  -0.9178   0.03508   0.03069  -0.0912   1.0000   0.0275
 -13.500  -0.9351   0.03354   0.02906  -0.0877   1.0000   0.0276
 -13.250  -0.9577   0.03259   0.02804  -0.0818   1.0000   0.0278
 -13.000  -0.9789   0.03180   0.02717  -0.0754   1.0000   0.0279
 -12.750  -0.9649   0.03053   0.02577  -0.0751   0.9980   0.0285
 -12.500  -0.9382   0.02917   0.02422  -0.0770   0.9947   0.0292
 -12.250  -0.9124   0.02768   0.02252  -0.0786   0.9915   0.0299
 -12.000  -0.8866   0.02641   0.02126  -0.0796   0.9876   0.0307
 -11.750  -0.8556   0.02553   0.02035  -0.0812   0.9845   0.0314
 -11.500  -0.8221   0.02457   0.01930  -0.0833   0.9822   0.0323
 -11.250  -0.7933   0.02362   0.01820  -0.0843   0.9782   0.0332
 -11.000  -0.7642   0.02282   0.01723  -0.0851   0.9737   0.0339
 -10.750  -0.7342   0.02154   0.01598  -0.0865   0.9709   0.0350
 -10.500  -0.6996   0.02091   0.01533  -0.0882   0.9691   0.0361
 -10.250  -0.6701   0.02027   0.01461  -0.0889   0.9655   0.0373
 -10.000  -0.6427   0.01963   0.01385  -0.0890   0.9603   0.0383
  -9.750  -0.6118   0.01859   0.01279  -0.0902   0.9576   0.0394
  -9.500  -0.5770   0.01799   0.01220  -0.0918   0.9558   0.0407
  -9.250  -0.5409   0.01742   0.01158  -0.0936   0.9544   0.0422
  -9.000  -0.5136   0.01695   0.01102  -0.0934   0.9493   0.0434
  -8.750  -0.4843   0.01613   0.01020  -0.0940   0.9449   0.0448
  -8.500  -0.4493   0.01562   0.00970  -0.0955   0.9423   0.0464
  -8.250  -0.4131   0.01515   0.00918  -0.0971   0.9398   0.0483
  -8.000  -0.3849   0.01460   0.00858  -0.0971   0.9338   0.0499
  -7.750  -0.3551   0.01412   0.00812  -0.0975   0.9273   0.0517
  -7.500  -0.3186   0.01371   0.00766  -0.0990   0.9226   0.0542
  -7.250  -0.2945   0.01330   0.00722  -0.0981   0.9131   0.0563
  -7.000  -0.2623   0.01292   0.00684  -0.0989   0.9067   0.0590
  -6.750  -0.2362   0.01267   0.00654  -0.0983   0.8969   0.0617
  -6.500  -0.2063   0.01225   0.00610  -0.0985   0.8889   0.0650
  -6.250  -0.1812   0.01206   0.00588  -0.0977   0.8783   0.0684
  -6.000  -0.1526   0.01172   0.00549  -0.0977   0.8697   0.0724
  -5.750  -0.1283   0.01151   0.00527  -0.0967   0.8587   0.0762
  -5.500  -0.1017   0.01129   0.00498  -0.0962   0.8487   0.0804
  -5.250  -0.0767   0.01102   0.00471  -0.0954   0.8384   0.0851
  -5.000  -0.0509   0.01090   0.00451  -0.0947   0.8276   0.0891
  -4.750  -0.0261   0.01060   0.00419  -0.0939   0.8159   0.0942
  -4.500  -0.0017   0.01045   0.00400  -0.0929   0.8032   0.0989
  -4.250   0.0227   0.01024   0.00378  -0.0920   0.7912   0.1045
  -4.000   0.0482   0.01010   0.00359  -0.0913   0.7799   0.1106
  -3.750   0.0723   0.00992   0.00341  -0.0902   0.7675   0.1183
  -3.500   0.0969   0.00976   0.00325  -0.0893   0.7550   0.1291
  -3.250   0.1208   0.00956   0.00310  -0.0883   0.7414   0.1485
  -3.000   0.1439   0.00934   0.00295  -0.0872   0.7265   0.1826
  -2.750   0.1668   0.00912   0.00285  -0.0860   0.7107   0.2265
  -2.500   0.1900   0.00895   0.00276  -0.0849   0.6949   0.2672
  -2.250   0.2136   0.00883   0.00269  -0.0839   0.6790   0.3016
  -2.000   0.2368   0.00872   0.00262  -0.0827   0.6633   0.3377
  -1.750   0.2595   0.00860   0.00258  -0.0815   0.6479   0.3809
  -1.500   0.2818   0.00849   0.00256  -0.0802   0.6324   0.4323
  -1.250   0.3042   0.00843   0.00257  -0.0789   0.6168   0.4839
  -1.000   0.3266   0.00840   0.00259  -0.0776   0.6007   0.5277
  -0.750   0.3498   0.00838   0.00261  -0.0764   0.5854   0.5637
  -0.500   0.3729   0.00839   0.00264  -0.0752   0.5700   0.5948
  -0.250   0.3955   0.00839   0.00267  -0.0738   0.5539   0.6251
   0.000   0.4173   0.00840   0.00271  -0.0724   0.5366   0.6596
   0.250   0.4381   0.00842   0.00278  -0.0706   0.5169   0.6977
   0.500   0.4581   0.00849   0.00286  -0.0687   0.4944   0.7365
   0.750   0.4779   0.00860   0.00293  -0.0668   0.4689   0.7715
   1.000   0.4966   0.00873   0.00302  -0.0647   0.4402   0.8061
   1.250   0.5156   0.00885   0.00313  -0.0627   0.4117   0.8448
   1.750   0.6117   0.00943   0.00360  -0.0711   0.3653   0.9454
   2.250   0.7051   0.01004   0.00400  -0.0791   0.3425   0.9889
   2.500   0.7459   0.01037   0.00421  -0.0820   0.3342   1.0000
   2.750   0.7651   0.01050   0.00430  -0.0802   0.3295   1.0000
   3.000   0.7845   0.01065   0.00441  -0.0785   0.3245   1.0000
   3.250   0.8034   0.01086   0.00455  -0.0767   0.3197   1.0000
   3.500   0.8223   0.01110   0.00472  -0.0749   0.3150   1.0000
   3.750   0.8439   0.01122   0.00484  -0.0735   0.3116   1.0000
   4.000   0.8649   0.01138   0.00499  -0.0721   0.3075   1.0000
   4.250   0.8851   0.01158   0.00514  -0.0705   0.3034   1.0000
   4.500   0.9042   0.01186   0.00536  -0.0688   0.2991   1.0000
   4.750   0.9254   0.01204   0.00553  -0.0674   0.2960   1.0000
   5.000   0.9469   0.01219   0.00569  -0.0661   0.2928   1.0000
   5.250   0.9678   0.01236   0.00586  -0.0647   0.2892   1.0000
   5.500   0.9870   0.01258   0.00604  -0.0630   0.2854   1.0000
   5.750   1.0048   0.01290   0.00630  -0.0611   0.2813   1.0000
   6.000   1.0247   0.01306   0.00648  -0.0595   0.2786   1.0000
   6.250   1.0448   0.01321   0.00666  -0.0580   0.2755   1.0000
   6.500   1.0645   0.01340   0.00686  -0.0564   0.2721   1.0000
   6.750   1.0833   0.01363   0.00706  -0.0547   0.2684   1.0000
   7.000   1.1014   0.01398   0.00736  -0.0530   0.2643   1.0000
   7.250   1.1219   0.01416   0.00759  -0.0517   0.2613   1.0000
   7.500   1.1422   0.01434   0.00780  -0.0503   0.2579   1.0000
   7.750   1.1619   0.01457   0.00804  -0.0489   0.2542   1.0000
   8.000   1.1801   0.01487   0.00831  -0.0473   0.2501   1.0000
   8.250   1.1987   0.01520   0.00863  -0.0459   0.2461   1.0000
   8.500   1.2191   0.01540   0.00889  -0.0447   0.2424   1.0000
   8.750   1.2384   0.01566   0.00916  -0.0433   0.2381   1.0000
   9.000   1.2556   0.01602   0.00949  -0.0417   0.2336   1.0000
   9.250   1.2741   0.01636   0.00985  -0.0404   0.2293   1.0000
   9.500   1.2937   0.01665   0.01018  -0.0392   0.2253   1.0000
   9.750   1.3116   0.01702   0.01056  -0.0378   0.2211   1.0000
  10.000   1.3269   0.01753   0.01103  -0.0362   0.2167   1.0000
  10.250   1.3459   0.01788   0.01144  -0.0351   0.2130   1.0000
  10.500   1.3641   0.01828   0.01188  -0.0339   0.2087   1.0000
  10.750   1.3799   0.01879   0.01239  -0.0324   0.2046   1.0000
  11.000   1.3942   0.01942   0.01300  -0.0309   0.2005   1.0000
  11.250   1.4126   0.01986   0.01352  -0.0299   0.1972   1.0000
  11.500   1.4289   0.02041   0.01410  -0.0287   0.1934   1.0000
  11.750   1.4427   0.02110   0.01479  -0.0272   0.1894   1.0000
  12.000   1.4562   0.02185   0.01555  -0.0259   0.1856   1.0000
  12.250   1.4729   0.02243   0.01621  -0.0249   0.1822   1.0000
  12.500   1.4869   0.02318   0.01698  -0.0237   0.1781   1.0000
  12.750   1.4984   0.02411   0.01790  -0.0223   0.1745   1.0000
  13.000   1.5109   0.02500   0.01884  -0.0212   0.1712   1.0000
  13.250   1.5256   0.02578   0.01969  -0.0202   0.1682   1.0000
  13.500   1.5381   0.02672   0.02068  -0.0192   0.1650   1.0000
  13.750   1.5478   0.02787   0.02184  -0.0180   0.1618   1.0000
  14.000   1.5558   0.02918   0.02317  -0.0168   0.1586   1.0000
  14.250   1.5696   0.03010   0.02420  -0.0161   0.1558   1.0000
  14.500   1.5803   0.03127   0.02543  -0.0153   0.1527   1.0000
  14.750   1.5872   0.03277   0.02695  -0.0143   0.1487   1.0000
  15.000   1.5922   0.03447   0.02867  -0.0134   0.1452   1.0000
  15.250   1.6037   0.03569   0.03000  -0.0129   0.1414   1.0000
  15.500   1.6099   0.03739   0.03175  -0.0123   0.1376   1.0000
  15.750   1.6099   0.03972   0.03408  -0.0116   0.1332   1.0000
  16.000   1.6188   0.04130   0.03576  -0.0113   0.1293   1.0000
  16.250   1.6210   0.04355   0.03807  -0.0109   0.1247   1.0000
  16.500   1.6189   0.04631   0.04086  -0.0107   0.1203   1.0000
  16.750   1.6214   0.04868   0.04331  -0.0106   0.1149   1.0000
  17.000   1.6135   0.05226   0.04691  -0.0107   0.1097   1.0000
  17.250   1.6116   0.05522   0.04995  -0.0108   0.1043   1.0000
  17.500   1.5975   0.05971   0.05448  -0.0113   0.0985   1.0000
  17.750   1.5877   0.06380   0.05863  -0.0119   0.0926   1.0000
  18.000   1.5698   0.06899   0.06388  -0.0129   0.0883   1.0000
  18.250   1.5535   0.07411   0.06907  -0.0140   0.0834   1.0000
  18.750   1.5118   0.08595   0.08107  -0.0171   0.0770   1.0000
  19.000   1.4921   0.09189   0.08710  -0.0189   0.0747   1.0000
  19.250   1.4691   0.09842   0.09370  -0.0210   0.0727   1.0000
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