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GOE 563 AIRFOIL (goe563-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 563 AIRFOIL (goe563-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.59 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe563-il-1000000-n5.txt
Download as CSV file: xf-goe563-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 563 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0716   0.04259   0.04015  -0.0739   1.0000   0.0056
 -14.500  -1.1093   0.03616   0.03346  -0.0765   1.0000   0.0056
 -14.250  -1.1268   0.03341   0.03054  -0.0735   1.0000   0.0056
 -14.000  -1.1312   0.03093   0.02789  -0.0715   1.0000   0.0057
 -13.750  -1.1280   0.02905   0.02586  -0.0697   1.0000   0.0058
 -13.500  -1.1215   0.02738   0.02403  -0.0678   1.0000   0.0059
 -13.250  -1.1127   0.02591   0.02241  -0.0660   1.0000   0.0061
 -13.000  -1.1019   0.02464   0.02101  -0.0642   1.0000   0.0062
 -12.750  -1.0899   0.02351   0.01975  -0.0624   1.0000   0.0063
 -12.500  -1.0773   0.02250   0.01862  -0.0604   1.0000   0.0065
 -12.250  -1.0643   0.02159   0.01759  -0.0584   1.0000   0.0066
 -12.000  -1.0401   0.02032   0.01618  -0.0589   0.9986   0.0070
 -11.750  -1.0139   0.01923   0.01498  -0.0596   0.9968   0.0074
 -11.500  -0.9869   0.01828   0.01391  -0.0604   0.9949   0.0078
 -11.250  -0.9604   0.01747   0.01301  -0.0608   0.9928   0.0083
 -11.000  -0.9334   0.01676   0.01219  -0.0612   0.9906   0.0087
 -10.750  -0.9053   0.01609   0.01142  -0.0618   0.9885   0.0091
 -10.500  -0.8767   0.01534   0.01060  -0.0626   0.9868   0.0100
 -10.250  -0.8471   0.01470   0.00990  -0.0634   0.9854   0.0108
 -10.000  -0.8195   0.01417   0.00928  -0.0637   0.9828   0.0117
  -9.750  -0.7912   0.01367   0.00872  -0.0641   0.9802   0.0125
  -9.500  -0.7615   0.01325   0.00829  -0.0648   0.9781   0.0141
  -9.250  -0.7311   0.01288   0.00790  -0.0656   0.9762   0.0155
  -9.000  -0.7001   0.01251   0.00748  -0.0665   0.9746   0.0167
  -8.750  -0.6721   0.01227   0.00725  -0.0667   0.9710   0.0180
  -8.500  -0.6429   0.01204   0.00700  -0.0671   0.9677   0.0192
  -8.250  -0.6127   0.01182   0.00674  -0.0677   0.9649   0.0203
  -8.000  -0.5820   0.01160   0.00648  -0.0684   0.9624   0.0211
  -7.750  -0.5547   0.01144   0.00628  -0.0684   0.9579   0.0216
  -7.500  -0.5276   0.01104   0.00583  -0.0683   0.9533   0.0225
  -7.250  -0.4994   0.01072   0.00546  -0.0685   0.9494   0.0234
  -7.000  -0.4722   0.01053   0.00528  -0.0684   0.9448   0.0244
  -6.750  -0.4454   0.01033   0.00505  -0.0682   0.9396   0.0252
  -6.500  -0.4179   0.01012   0.00480  -0.0681   0.9349   0.0260
  -6.250  -0.3912   0.00991   0.00454  -0.0679   0.9299   0.0267
  -6.000  -0.3647   0.00970   0.00429  -0.0676   0.9243   0.0273
  -5.750  -0.3377   0.00950   0.00404  -0.0674   0.9192   0.0278
  -5.500  -0.3112   0.00931   0.00382  -0.0670   0.9133   0.0282
  -5.250  -0.2846   0.00911   0.00357  -0.0667   0.9070   0.0284
  -5.000  -0.2581   0.00890   0.00331  -0.0664   0.9006   0.0285
  -4.750  -0.2321   0.00863   0.00297  -0.0659   0.8931   0.0291
  -4.500  -0.2059   0.00837   0.00265  -0.0655   0.8859   0.0301
  -4.250  -0.1795   0.00816   0.00240  -0.0651   0.8782   0.0312
  -4.000  -0.1528   0.00799   0.00221  -0.0648   0.8713   0.0325
  -3.750  -0.1260   0.00785   0.00204  -0.0645   0.8638   0.0334
  -3.500  -0.0991   0.00772   0.00188  -0.0642   0.8566   0.0344
  -3.250  -0.0721   0.00760   0.00173  -0.0639   0.8487   0.0353
  -3.000  -0.0451   0.00750   0.00160  -0.0637   0.8410   0.0363
  -2.750  -0.0183   0.00742   0.00147  -0.0633   0.8314   0.0372
  -2.500   0.0084   0.00733   0.00135  -0.0629   0.8187   0.0404
  -2.250   0.0347   0.00724   0.00124  -0.0625   0.8041   0.0454
  -2.000   0.0608   0.00714   0.00114  -0.0621   0.7890   0.0589
  -1.750   0.0866   0.00703   0.00107  -0.0616   0.7725   0.0833
  -1.500   0.1127   0.00700   0.00102  -0.0611   0.7539   0.0942
  -1.250   0.1389   0.00701   0.00096  -0.0606   0.7340   0.1004
  -1.000   0.1652   0.00699   0.00092  -0.0602   0.7177   0.1091
  -0.750   0.1917   0.00694   0.00089  -0.0599   0.7041   0.1229
  -0.250   0.2439   0.00679   0.00084  -0.0591   0.6740   0.1884
   0.000   0.2697   0.00670   0.00082  -0.0586   0.6577   0.2278
   0.250   0.2927   0.00645   0.00082  -0.0578   0.6275   0.3493
   0.500   0.3164   0.00645   0.00085  -0.0569   0.5894   0.4120
   0.750   0.3402   0.00636   0.00089  -0.0562   0.5612   0.4900
   1.000   0.3642   0.00625   0.00094  -0.0554   0.5372   0.5708
   1.250   0.3877   0.00618   0.00100  -0.0545   0.5100   0.6460
   1.500   0.4088   0.00612   0.00108  -0.0531   0.4734   0.7417
   1.750   0.4297   0.00614   0.00119  -0.0516   0.4316   0.8172
   2.000   0.4506   0.00628   0.00132  -0.0500   0.3810   0.8824
   2.250   0.4863   0.00662   0.00154  -0.0518   0.3174   0.9529
   2.500   0.5296   0.00689   0.00168  -0.0554   0.2864   0.9753
   2.750   0.5652   0.00709   0.00179  -0.0572   0.2672   0.9845
   3.000   0.5987   0.00728   0.00190  -0.0585   0.2496   0.9907
   3.250   0.6315   0.00749   0.00202  -0.0597   0.2305   0.9967
   3.500   0.6648   0.00771   0.00216  -0.0610   0.2099   0.9999
   3.750   0.6873   0.00801   0.00232  -0.0600   0.1797   1.0000
   4.000   0.7093   0.00831   0.00249  -0.0588   0.1527   1.0000
   4.250   0.7312   0.00862   0.00268  -0.0577   0.1290   1.0000
   4.500   0.7541   0.00886   0.00286  -0.0567   0.1156   1.0000
   4.750   0.7776   0.00907   0.00304  -0.0558   0.1076   1.0000
   5.000   0.8012   0.00927   0.00321  -0.0549   0.0998   1.0000
   5.250   0.8243   0.00952   0.00342  -0.0540   0.0903   1.0000
   5.500   0.8470   0.00980   0.00364  -0.0530   0.0766   1.0000
   5.750   0.8672   0.01031   0.00396  -0.0516   0.0457   1.0000
   6.000   0.8896   0.01065   0.00424  -0.0506   0.0370   1.0000
   6.250   0.9128   0.01092   0.00450  -0.0497   0.0328   1.0000
   6.500   0.9362   0.01117   0.00477  -0.0488   0.0308   1.0000
   6.750   0.9593   0.01146   0.00506  -0.0479   0.0287   1.0000
   7.000   0.9820   0.01178   0.00537  -0.0470   0.0260   1.0000
   7.250   1.0054   0.01204   0.00566  -0.0462   0.0248   1.0000
   7.500   1.0289   0.01229   0.00594  -0.0454   0.0234   1.0000
   7.750   1.0518   0.01258   0.00625  -0.0446   0.0214   1.0000
   8.000   1.0740   0.01295   0.00660  -0.0436   0.0188   1.0000
   8.250   1.0967   0.01326   0.00692  -0.0427   0.0172   1.0000
   8.500   1.1187   0.01362   0.00727  -0.0418   0.0150   1.0000
   8.750   1.1404   0.01400   0.00767  -0.0408   0.0133   1.0000
   9.000   1.1622   0.01437   0.00807  -0.0398   0.0123   1.0000
   9.250   1.1834   0.01478   0.00849  -0.0387   0.0113   1.0000
   9.500   1.2038   0.01525   0.00897  -0.0375   0.0101   1.0000
   9.750   1.2243   0.01569   0.00945  -0.0364   0.0095   1.0000
  10.000   1.2447   0.01611   0.00992  -0.0352   0.0090   1.0000
  10.250   1.2644   0.01658   0.01043  -0.0340   0.0083   1.0000
  10.500   1.2833   0.01708   0.01097  -0.0326   0.0078   1.0000
  10.750   1.3009   0.01767   0.01159  -0.0311   0.0073   1.0000
  11.000   1.3182   0.01824   0.01222  -0.0295   0.0069   1.0000
  11.250   1.3350   0.01876   0.01279  -0.0278   0.0067   1.0000
  11.500   1.3494   0.01932   0.01341  -0.0257   0.0065   1.0000
  11.750   1.3631   0.01988   0.01404  -0.0235   0.0062   1.0000
  12.000   1.3761   0.02051   0.01474  -0.0213   0.0060   1.0000
  12.250   1.3885   0.02118   0.01548  -0.0191   0.0058   1.0000
  12.500   1.4005   0.02189   0.01624  -0.0170   0.0056   1.0000
  12.750   1.4110   0.02271   0.01712  -0.0148   0.0054   1.0000
  13.000   1.4196   0.02368   0.01816  -0.0124   0.0052   1.0000
  13.250   1.4274   0.02471   0.01927  -0.0101   0.0050   1.0000
  13.500   1.4363   0.02569   0.02034  -0.0081   0.0049   1.0000
  13.750   1.4443   0.02676   0.02151  -0.0061   0.0048   1.0000
  14.000   1.4521   0.02788   0.02272  -0.0043   0.0047   1.0000
  14.250   1.4597   0.02905   0.02397  -0.0026   0.0046   1.0000
  14.500   1.4648   0.03047   0.02548  -0.0009   0.0045   1.0000
  14.750   1.4674   0.03217   0.02729   0.0007   0.0044   1.0000
  15.000   1.4713   0.03383   0.02905   0.0020   0.0043   1.0000
  15.250   1.4739   0.03569   0.03101   0.0032   0.0042   1.0000
  15.500   1.4733   0.03797   0.03340   0.0041   0.0041   1.0000
  15.750   1.4744   0.04022   0.03574   0.0048   0.0040   1.0000
  16.000   1.4703   0.04313   0.03877   0.0051   0.0040   1.0000
  16.250   1.4670   0.04617   0.04192   0.0051   0.0040   1.0000
  16.500   1.4600   0.04984   0.04572   0.0046   0.0039   1.0000
  16.750   1.4541   0.05360   0.04959   0.0037   0.0038   1.0000
  17.000   1.4425   0.05844   0.05457   0.0021   0.0038   1.0000
  17.250   1.4303   0.06371   0.05997  -0.0001   0.0038   1.0000
  17.500   1.4090   0.07082   0.06726  -0.0034   0.0038   1.0000
  17.750   1.3933   0.07736   0.07392  -0.0067   0.0038   1.0000
  18.000   1.3709   0.08539   0.08211  -0.0109   0.0038   1.0000
  18.250   1.3395   0.09549   0.09238  -0.0163   0.0037   1.0000
  18.500   1.3112   0.10509   0.10214  -0.0215   0.0038   1.0000
  18.750   1.2769   0.11619   0.11339  -0.0275   0.0038   1.0000
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