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GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.02 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe315-il-1000000-n5.txt
Download as CSV file: xf-goe315-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 315 (HANSA-BRANDENBURG III.5) 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.4160   0.11067   0.10895  -0.0100   1.0000   0.0076
 -10.250  -0.4119   0.10722   0.10551  -0.0113   1.0000   0.0079
 -10.000  -0.4168   0.10136   0.09966  -0.0136   1.0000   0.0087
  -9.750  -0.4115   0.09846   0.09678  -0.0148   1.0000   0.0088
  -9.500  -0.4060   0.09568   0.09401  -0.0159   1.0000   0.0089
  -9.250  -0.3987   0.09340   0.09174  -0.0168   1.0000   0.0091
  -9.000  -0.3945   0.09048   0.08884  -0.0180   1.0000   0.0092
  -8.500  -0.3395   0.07970   0.07799  -0.0361   0.9392   0.0101
  -8.250  -0.3268   0.07238   0.07020  -0.0470   0.8186   0.0111
  -8.000  -0.3232   0.07009   0.06777  -0.0482   0.7842   0.0112
  -7.750  -0.3155   0.06761   0.06521  -0.0500   0.7647   0.0114
  -7.500  -0.3069   0.06466   0.06220  -0.0523   0.7511   0.0115
  -7.250  -0.2960   0.06171   0.05918  -0.0546   0.7400   0.0118
  -7.000  -0.2841   0.05830   0.05569  -0.0571   0.7301   0.0121
  -6.750  -0.2795   0.04943   0.04663  -0.0629   0.7229   0.0137
  -6.500  -0.2612   0.04712   0.04423  -0.0640   0.7143   0.0139
  -6.250  -0.2416   0.04511   0.04213  -0.0648   0.7068   0.0141
  -6.000  -0.2213   0.04302   0.03995  -0.0655   0.6993   0.0143
  -5.750  -0.2008   0.04067   0.03749  -0.0662   0.6922   0.0146
  -5.500  -0.1799   0.03783   0.03450  -0.0669   0.6843   0.0152
  -5.250  -0.1623   0.03017   0.02639  -0.0675   0.6782   0.0170
  -5.000  -0.1391   0.02868   0.02480  -0.0675   0.6693   0.0172
  -4.750  -0.1154   0.02736   0.02335  -0.0673   0.6603   0.0174
  -4.500  -0.0915   0.02601   0.02187  -0.0671   0.6495   0.0177
  -4.250  -0.0673   0.02447   0.02017  -0.0668   0.6377   0.0181
  -3.750  -0.0250   0.01520   0.00981  -0.0642   0.6133   0.0207
  -3.500   0.0005   0.01462   0.00907  -0.0638   0.5957   0.0210
  -3.250   0.0261   0.01408   0.00837  -0.0634   0.5765   0.0212
  -3.000   0.0520   0.01359   0.00773  -0.0630   0.5591   0.0214
  -2.750   0.0779   0.01302   0.00699  -0.0626   0.5449   0.0217
  -2.500   0.1042   0.01251   0.00634  -0.0622   0.5330   0.0219
  -2.250   0.1304   0.01194   0.00563  -0.0618   0.5228   0.0222
  -2.000   0.1571   0.01140   0.00498  -0.0615   0.5142   0.0224
  -1.750   0.1836   0.01094   0.00440  -0.0611   0.5051   0.0227
  -1.500   0.2103   0.01057   0.00395  -0.0607   0.4963   0.0230
  -1.250   0.2371   0.01027   0.00358  -0.0604   0.4894   0.0234
  -1.000   0.2640   0.00992   0.00317  -0.0601   0.4836   0.0237
  -0.750   0.2907   0.00965   0.00286  -0.0597   0.4776   0.0240
  -0.500   0.3177   0.00943   0.00261  -0.0594   0.4728   0.0244
  -0.250   0.3447   0.00926   0.00241  -0.0591   0.4675   0.0246
   0.000   0.3716   0.00917   0.00227  -0.0588   0.4585   0.0249
   0.250   0.3986   0.00905   0.00213  -0.0586   0.4493   0.0250
   0.500   0.4247   0.00877   0.00181  -0.0581   0.4400   0.0256
   0.750   0.4512   0.00868   0.00166  -0.0578   0.4256   0.0260
   1.000   0.4774   0.00868   0.00157  -0.0574   0.4003   0.0264
   1.250   0.5030   0.00879   0.00153  -0.0570   0.3663   0.0267
   1.500   0.5287   0.00893   0.00155  -0.0566   0.3350   0.0274
   1.750   0.5543   0.00909   0.00159  -0.0561   0.3057   0.0282
   2.000   0.5796   0.00929   0.00165  -0.0557   0.2727   0.0288
   2.250   0.6054   0.00944   0.00170  -0.0553   0.2499   0.0295
   2.500   0.6315   0.00958   0.00176  -0.0549   0.2332   0.0302
   2.750   0.6578   0.00969   0.00183  -0.0546   0.2206   0.0308
   3.000   0.6840   0.00982   0.00190  -0.0543   0.2079   0.0316
   3.250   0.7102   0.00995   0.00198  -0.0539   0.1956   0.0333
   3.500   0.7361   0.01012   0.00209  -0.0536   0.1799   0.0355
   4.000   0.7698   0.00952   0.00280  -0.0501   0.0903   0.8182
   4.750   0.8736   0.01034   0.00366  -0.0551   0.0326   1.0000
   5.000   0.8984   0.01055   0.00386  -0.0545   0.0314   1.0000
   5.250   0.9231   0.01077   0.00407  -0.0539   0.0304   1.0000
   5.500   0.9477   0.01100   0.00430  -0.0533   0.0295   1.0000
   5.750   0.9723   0.01124   0.00455  -0.0527   0.0288   1.0000
   6.000   0.9966   0.01151   0.00482  -0.0521   0.0280   1.0000
   6.250   1.0210   0.01177   0.00508  -0.0515   0.0275   1.0000
   6.500   1.0453   0.01202   0.00535  -0.0509   0.0272   1.0000
   6.750   1.0695   0.01229   0.00564  -0.0503   0.0269   1.0000
   7.000   1.0934   0.01258   0.00595  -0.0497   0.0265   1.0000
   7.250   1.1171   0.01288   0.00628  -0.0491   0.0261   1.0000
   7.500   1.1406   0.01320   0.00662  -0.0484   0.0257   1.0000
   7.750   1.1638   0.01353   0.00698  -0.0477   0.0251   1.0000
   8.000   1.1868   0.01388   0.00735  -0.0470   0.0247   1.0000
   8.250   1.2094   0.01426   0.00775  -0.0462   0.0241   1.0000
   8.500   1.2314   0.01466   0.00819  -0.0454   0.0235   1.0000
   8.750   1.2525   0.01515   0.00870  -0.0445   0.0229   1.0000
   9.000   1.2717   0.01578   0.00939  -0.0432   0.0221   1.0000
   9.250   1.2942   0.01609   0.00972  -0.0425   0.0219   1.0000
   9.500   1.3163   0.01641   0.01008  -0.0418   0.0215   1.0000
   9.750   1.3377   0.01677   0.01048  -0.0409   0.0210   1.0000
  10.000   1.3584   0.01717   0.01092  -0.0400   0.0204   1.0000
  10.250   1.3789   0.01757   0.01135  -0.0390   0.0198   1.0000
  10.500   1.3993   0.01795   0.01176  -0.0381   0.0191   1.0000
  10.750   1.4189   0.01836   0.01218  -0.0370   0.0185   1.0000
  11.000   1.4364   0.01888   0.01273  -0.0357   0.0178   1.0000
  11.250   1.4534   0.01939   0.01329  -0.0343   0.0173   1.0000
  11.500   1.4704   0.01983   0.01378  -0.0329   0.0168   1.0000
  11.750   1.4848   0.02028   0.01427  -0.0310   0.0161   1.0000
  12.000   1.4983   0.02077   0.01479  -0.0290   0.0153   1.0000
  12.250   1.5117   0.02127   0.01531  -0.0272   0.0145   1.0000
  12.500   1.5233   0.02192   0.01598  -0.0252   0.0138   1.0000
  12.750   1.5330   0.02270   0.01684  -0.0232   0.0134   1.0000
  13.000   1.5424   0.02356   0.01775  -0.0214   0.0127   1.0000
  13.250   1.5513   0.02452   0.01876  -0.0197   0.0120   1.0000
  13.500   1.5593   0.02563   0.01991  -0.0183   0.0114   1.0000
  13.750   1.5660   0.02695   0.02128  -0.0170   0.0106   1.0000
  14.000   1.5713   0.02851   0.02292  -0.0160   0.0104   1.0000
  14.250   1.5762   0.03024   0.02474  -0.0152   0.0097   1.0000
  14.500   1.5800   0.03219   0.02676  -0.0146   0.0093   1.0000
  14.750   1.5827   0.03434   0.02899  -0.0142   0.0090   1.0000
  15.000   1.5838   0.03676   0.03148  -0.0140   0.0086   1.0000
  15.250   1.5829   0.03947   0.03427  -0.0140   0.0082   1.0000
  15.500   1.5815   0.04233   0.03723  -0.0141   0.0080   1.0000
  15.750   1.5794   0.04539   0.04039  -0.0144   0.0078   1.0000
  16.000   1.5757   0.04874   0.04385  -0.0149   0.0077   1.0000
  16.250   1.5701   0.05240   0.04761  -0.0157   0.0075   1.0000
  16.500   1.5639   0.05624   0.05155  -0.0165   0.0072   1.0000
  16.750   1.5562   0.06035   0.05576  -0.0176   0.0071   1.0000
  17.000   1.5477   0.06471   0.06023  -0.0188   0.0070   1.0000
  17.250   1.5374   0.06944   0.06506  -0.0203   0.0069   1.0000
  17.500   1.5268   0.07435   0.07007  -0.0219   0.0067   1.0000
  17.750   1.5148   0.07962   0.07544  -0.0238   0.0065   1.0000
  18.000   1.5028   0.08501   0.08095  -0.0259   0.0066   1.0000
  18.250   1.4891   0.09087   0.08691  -0.0282   0.0064   1.0000
  18.500   1.4759   0.09679   0.09294  -0.0308   0.0063   1.0000
  18.750   1.4628   0.10281   0.09905  -0.0334   0.0062   1.0000
  19.000   1.4493   0.10905   0.10540  -0.0363   0.0061   1.0000
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