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GOE 591 AIRFOIL (goe591-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 591 AIRFOIL (goe591-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.71 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe591-il-1000000-n5.txt
Download as CSV file: xf-goe591-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 591 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.3538   0.15205   0.15027  -0.0310   1.0000   0.0046
 -14.250  -0.3480   0.14929   0.14752  -0.0319   1.0000   0.0048
 -12.750  -0.7735   0.03006   0.02754  -0.1105   0.9777   0.0074
 -12.500  -0.7577   0.02530   0.02241  -0.1141   0.9747   0.0076
 -12.250  -0.7396   0.02314   0.02003  -0.1147   0.9686   0.0078
 -12.000  -0.7146   0.02138   0.01806  -0.1161   0.9647   0.0081
 -11.750  -0.6897   0.02002   0.01653  -0.1168   0.9598   0.0083
 -11.500  -0.6654   0.01887   0.01521  -0.1172   0.9531   0.0085
 -11.250  -0.6400   0.01768   0.01388  -0.1177   0.9468   0.0091
 -11.000  -0.6161   0.01683   0.01291  -0.1176   0.9380   0.0094
 -10.750  -0.5911   0.01607   0.01203  -0.1175   0.9291   0.0100
 -10.500  -0.5662   0.01541   0.01124  -0.1173   0.9184   0.0106
 -10.250  -0.5421   0.01483   0.01051  -0.1169   0.9054   0.0111
 -10.000  -0.5176   0.01431   0.00990  -0.1164   0.8915   0.0118
  -9.750  -0.4927   0.01397   0.00947  -0.1159   0.8770   0.0126
  -9.500  -0.4680   0.01364   0.00904  -0.1154   0.8634   0.0134
  -9.250  -0.4435   0.01329   0.00856  -0.1148   0.8507   0.0141
  -9.000  -0.4189   0.01295   0.00811  -0.1142   0.8391   0.0147
  -8.750  -0.3933   0.01281   0.00790  -0.1138   0.8286   0.0154
  -8.500  -0.3672   0.01267   0.00772  -0.1134   0.8188   0.0161
  -8.250  -0.3411   0.01254   0.00753  -0.1130   0.8099   0.0168
  -8.000  -0.3152   0.01237   0.00727  -0.1126   0.8005   0.0176
  -7.750  -0.2891   0.01220   0.00702  -0.1122   0.7917   0.0182
  -7.250  -0.2378   0.01165   0.00630  -0.1113   0.7749   0.0192
  -6.750  -0.1846   0.01140   0.00598  -0.1107   0.7603   0.0204
  -6.500  -0.1582   0.01127   0.00579  -0.1104   0.7527   0.0210
  -6.250  -0.1315   0.01108   0.00554  -0.1101   0.7456   0.0217
  -6.000  -0.1052   0.01091   0.00529  -0.1098   0.7378   0.0223
  -5.750  -0.0785   0.01071   0.00503  -0.1095   0.7307   0.0229
  -5.500  -0.0521   0.01054   0.00478  -0.1091   0.7225   0.0233
  -5.250  -0.0253   0.01041   0.00459  -0.1088   0.7146   0.0236
  -5.000   0.0012   0.01027   0.00437  -0.1085   0.7061   0.0238
  -4.750   0.0267   0.00983   0.00385  -0.1080   0.6979   0.0244
  -4.500   0.0522   0.00951   0.00345  -0.1075   0.6888   0.0252
  -4.250   0.0784   0.00928   0.00316  -0.1071   0.6794   0.0257
  -4.000   0.1047   0.00910   0.00292  -0.1067   0.6704   0.0261
  -3.750   0.1310   0.00896   0.00272  -0.1064   0.6609   0.0266
  -3.500   0.1576   0.00882   0.00253  -0.1060   0.6509   0.0272
  -3.250   0.1840   0.00872   0.00236  -0.1057   0.6406   0.0278
  -3.000   0.2104   0.00863   0.00221  -0.1053   0.6302   0.0285
  -2.750   0.2371   0.00854   0.00207  -0.1050   0.6203   0.0290
  -2.500   0.2636   0.00847   0.00194  -0.1046   0.6102   0.0296
  -2.250   0.2900   0.00843   0.00183  -0.1042   0.5991   0.0299
  -2.000   0.3166   0.00838   0.00173  -0.1039   0.5878   0.0303
  -1.750   0.3432   0.00835   0.00165  -0.1036   0.5776   0.0307
  -1.500   0.3697   0.00834   0.00158  -0.1032   0.5671   0.0310
  -1.250   0.3961   0.00832   0.00151  -0.1029   0.5560   0.0320
  -1.000   0.4227   0.00830   0.00145  -0.1026   0.5457   0.0337
  -0.750   0.4490   0.00830   0.00142  -0.1022   0.5357   0.0368
  -0.500   0.4753   0.00827   0.00139  -0.1019   0.5252   0.0469
  -0.250   0.5015   0.00823   0.00140  -0.1015   0.5152   0.0716
   0.000   0.5276   0.00826   0.00141  -0.1012   0.5042   0.0811
   0.250   0.5535   0.00832   0.00142  -0.1008   0.4908   0.0871
   0.500   0.5791   0.00837   0.00145  -0.1003   0.4767   0.0992
   0.750   0.6049   0.00837   0.00148  -0.0999   0.4653   0.1291
   1.000   0.6307   0.00836   0.00153  -0.0996   0.4555   0.1680
   1.250   0.6564   0.00840   0.00159  -0.0992   0.4460   0.1953
   1.500   0.6823   0.00839   0.00165  -0.0988   0.4370   0.2290
   1.750   0.7069   0.00826   0.00173  -0.0983   0.4288   0.3295
   2.000   0.7280   0.00773   0.00185  -0.0973   0.4220   0.5950
   2.500   0.8176   0.00721   0.00218  -0.1049   0.4049   0.9974
   2.750   0.8474   0.00735   0.00227  -0.1054   0.3965   1.0000
   3.000   0.8711   0.00746   0.00234  -0.1046   0.3902   1.0000
   3.250   0.8947   0.00759   0.00243  -0.1037   0.3838   1.0000
   3.500   0.9185   0.00771   0.00252  -0.1029   0.3765   1.0000
   3.750   0.9418   0.00785   0.00262  -0.1020   0.3691   1.0000
   4.000   0.9657   0.00797   0.00272  -0.1013   0.3619   1.0000
   4.250   0.9890   0.00813   0.00285  -0.1004   0.3547   1.0000
   4.500   1.0127   0.00828   0.00296  -0.0996   0.3458   1.0000
   4.750   1.0358   0.00845   0.00310  -0.0987   0.3365   1.0000
   5.000   1.0590   0.00863   0.00325  -0.0979   0.3272   1.0000
   5.250   1.0818   0.00883   0.00340  -0.0970   0.3152   1.0000
   5.500   1.1033   0.00910   0.00359  -0.0959   0.2988   1.0000
   5.750   1.1235   0.00945   0.00383  -0.0945   0.2775   1.0000
   6.000   1.1418   0.00990   0.00413  -0.0929   0.2509   1.0000
   6.250   1.1617   0.01025   0.00439  -0.0915   0.2326   1.0000
   6.500   1.1809   0.01064   0.00468  -0.0901   0.2139   1.0000
   6.750   1.1989   0.01108   0.00501  -0.0884   0.1942   1.0000
   7.000   1.2163   0.01153   0.00536  -0.0867   0.1724   1.0000
   7.250   1.2304   0.01213   0.00579  -0.0844   0.1441   1.0000
   7.500   1.2430   0.01268   0.00622  -0.0817   0.1239   1.0000
   7.750   1.2572   0.01313   0.00661  -0.0794   0.1118   1.0000
   8.000   1.2726   0.01354   0.00699  -0.0773   0.1016   1.0000
   8.250   1.2868   0.01402   0.00741  -0.0751   0.0885   1.0000
   8.500   1.2881   0.01512   0.00828  -0.0708   0.0512   1.0000
   8.750   1.2894   0.01628   0.00928  -0.0667   0.0202   1.0000
   9.000   1.3020   0.01690   0.00989  -0.0645   0.0147   1.0000
   9.250   1.3164   0.01744   0.01047  -0.0627   0.0125   1.0000
   9.500   1.3315   0.01797   0.01103  -0.0610   0.0117   1.0000
   9.750   1.3455   0.01856   0.01166  -0.0592   0.0107   1.0000
  10.000   1.3578   0.01927   0.01240  -0.0573   0.0096   1.0000
  10.250   1.3711   0.01994   0.01311  -0.0556   0.0092   1.0000
  10.500   1.3847   0.02062   0.01383  -0.0540   0.0086   1.0000
  10.750   1.3971   0.02140   0.01465  -0.0523   0.0081   1.0000
  11.000   1.4085   0.02226   0.01555  -0.0507   0.0076   1.0000
  11.250   1.4188   0.02324   0.01657  -0.0490   0.0071   1.0000
  11.500   1.4276   0.02436   0.01774  -0.0473   0.0067   1.0000
  11.750   1.4384   0.02538   0.01881  -0.0459   0.0066   1.0000
  12.000   1.4483   0.02650   0.01999  -0.0445   0.0063   1.0000
  12.250   1.4570   0.02775   0.02130  -0.0432   0.0061   1.0000
  12.500   1.4660   0.02902   0.02263  -0.0419   0.0058   1.0000
  12.750   1.4734   0.03047   0.02414  -0.0407   0.0056   1.0000
  13.000   1.4810   0.03192   0.02564  -0.0396   0.0053   1.0000
  13.250   1.4858   0.03367   0.02744  -0.0384   0.0051   1.0000
  13.500   1.4892   0.03562   0.02946  -0.0373   0.0049   1.0000
  13.750   1.4921   0.03769   0.03160  -0.0364   0.0048   1.0000
  14.000   1.4960   0.03971   0.03371  -0.0356   0.0047   1.0000
  14.250   1.4988   0.04193   0.03600  -0.0349   0.0046   1.0000
  14.500   1.5027   0.04411   0.03826  -0.0344   0.0045   1.0000
  14.750   1.5042   0.04659   0.04083  -0.0339   0.0043   1.0000
  15.000   1.5043   0.04931   0.04363  -0.0336   0.0042   1.0000
  15.250   1.5041   0.05214   0.04655  -0.0334   0.0042   1.0000
  15.500   1.5042   0.05503   0.04952  -0.0334   0.0041   1.0000
  15.750   1.5009   0.05839   0.05297  -0.0335   0.0040   1.0000
  16.000   1.4985   0.06173   0.05639  -0.0337   0.0039   1.0000
  16.250   1.4962   0.06512   0.05987  -0.0340   0.0038   1.0000
  16.500   1.4921   0.06885   0.06369  -0.0346   0.0038   1.0000
  16.750   1.4864   0.07286   0.06779  -0.0352   0.0037   1.0000
  17.000   1.4820   0.07673   0.07174  -0.0360   0.0035   1.0000
  17.250   1.4743   0.08120   0.07631  -0.0370   0.0036   1.0000
  17.500   1.4670   0.08569   0.08090  -0.0381   0.0035   1.0000
  17.750   1.4568   0.09070   0.08601  -0.0395   0.0034   1.0000
  18.000   1.4460   0.09592   0.09133  -0.0411   0.0034   1.0000
  18.250   1.4368   0.10099   0.09651  -0.0427   0.0034   1.0000
  18.500   1.4243   0.10670   0.10233  -0.0448   0.0033   1.0000
  18.750   1.4153   0.11190   0.10763  -0.0467   0.0033   1.0000
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