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GOE 602 MOD. AIRFOIL (goe602m-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 602 MOD. AIRFOIL (goe602m-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.89 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe602m-il-1000000-n5.txt
Download as CSV file: xf-goe602m-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 602 MOD. 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4101   0.12550   0.12379  -0.0294   1.0000   0.0034
 -12.000  -0.4046   0.12303   0.12133  -0.0301   1.0000   0.0036
 -11.500  -0.7518   0.02909   0.02663  -0.0984   0.9874   0.0035
 -11.250  -0.7342   0.02563   0.02287  -0.1014   0.9837   0.0035
 -11.000  -0.7126   0.02328   0.02029  -0.1032   0.9803   0.0037
 -10.750  -0.6869   0.02144   0.01825  -0.1050   0.9782   0.0038
 -10.500  -0.6588   0.01994   0.01656  -0.1067   0.9767   0.0039
 -10.250  -0.6353   0.01879   0.01526  -0.1070   0.9722   0.0040
 -10.000  -0.6077   0.01766   0.01395  -0.1080   0.9692   0.0042
  -9.750  -0.5785   0.01661   0.01274  -0.1093   0.9668   0.0044
  -9.500  -0.5501   0.01568   0.01166  -0.1101   0.9639   0.0045
  -9.250  -0.5244   0.01487   0.01072  -0.1103   0.9589   0.0047
  -9.000  -0.4952   0.01414   0.00985  -0.1111   0.9553   0.0049
  -8.750  -0.4654   0.01345   0.00903  -0.1120   0.9520   0.0051
  -8.500  -0.4400   0.01269   0.00817  -0.1119   0.9461   0.0055
  -8.250  -0.4115   0.01213   0.00752  -0.1124   0.9413   0.0059
  -8.000  -0.3832   0.01166   0.00697  -0.1127   0.9367   0.0064
  -7.750  -0.3565   0.01123   0.00643  -0.1127   0.9307   0.0068
  -7.500  -0.3285   0.01082   0.00591  -0.1128   0.9253   0.0072
  -7.250  -0.3021   0.01040   0.00540  -0.1127   0.9196   0.0078
  -7.000  -0.2753   0.01000   0.00494  -0.1125   0.9136   0.0087
  -6.750  -0.2482   0.00969   0.00457  -0.1125   0.9080   0.0097
  -6.500  -0.2217   0.00941   0.00422  -0.1122   0.9016   0.0106
  -6.000  -0.1678   0.00897   0.00375  -0.1119   0.8888   0.0152
  -5.750  -0.1407   0.00879   0.00353  -0.1118   0.8816   0.0172
  -5.500  -0.1137   0.00869   0.00343  -0.1116   0.8734   0.0196
  -5.250  -0.0864   0.00862   0.00332  -0.1114   0.8655   0.0219
  -5.000  -0.0592   0.00856   0.00322  -0.1112   0.8569   0.0234
  -4.750  -0.0319   0.00851   0.00313  -0.1110   0.8490   0.0242
  -4.500  -0.0047   0.00849   0.00306  -0.1108   0.8401   0.0246
  -4.250   0.0217   0.00824   0.00274  -0.1105   0.8307   0.0257
  -4.000   0.0479   0.00799   0.00240  -0.1102   0.8208   0.0271
  -3.750   0.0743   0.00783   0.00216  -0.1098   0.8092   0.0283
  -3.250   0.1271   0.00760   0.00177  -0.1091   0.7828   0.0294
  -3.000   0.1534   0.00752   0.00161  -0.1087   0.7684   0.0298
  -2.750   0.1797   0.00747   0.00148  -0.1083   0.7535   0.0307
  -2.500   0.2058   0.00742   0.00135  -0.1079   0.7381   0.0313
  -2.250   0.2321   0.00739   0.00124  -0.1075   0.7232   0.0320
  -2.000   0.2584   0.00737   0.00115  -0.1071   0.7078   0.0333
  -1.750   0.2847   0.00737   0.00108  -0.1067   0.6931   0.0348
  -1.500   0.3110   0.00735   0.00101  -0.1063   0.6780   0.0424
  -1.250   0.3367   0.00721   0.00096  -0.1059   0.6628   0.0875
  -1.000   0.3628   0.00719   0.00094  -0.1055   0.6475   0.1059
  -0.750   0.3889   0.00717   0.00091  -0.1052   0.6324   0.1248
  -0.500   0.4138   0.00692   0.00089  -0.1048   0.6167   0.2250
  -0.250   0.4395   0.00692   0.00092  -0.1043   0.5985   0.2660
   0.000   0.4645   0.00702   0.00095  -0.1038   0.5714   0.2861
   0.250   0.4888   0.00719   0.00100  -0.1030   0.5363   0.2977
   0.500   0.5139   0.00733   0.00105  -0.1025   0.5085   0.3085
   0.750   0.5395   0.00742   0.00110  -0.1021   0.4876   0.3257
   1.000   0.5653   0.00747   0.00115  -0.1017   0.4714   0.3510
   1.250   0.5903   0.00734   0.00124  -0.1013   0.4570   0.4459
   1.500   0.6155   0.00732   0.00135  -0.1008   0.4426   0.5174
   1.750   0.6413   0.00738   0.00143  -0.1004   0.4288   0.5512
   2.000   0.6672   0.00748   0.00152  -0.1000   0.4147   0.5704
   2.250   0.6930   0.00755   0.00161  -0.0997   0.4023   0.5941
   2.500   0.7184   0.00761   0.00170  -0.0992   0.3885   0.6244
   2.750   0.7425   0.00757   0.00182  -0.0985   0.3744   0.6923
   3.000   0.7609   0.00718   0.00198  -0.0964   0.3621   0.9045
   3.250   0.8069   0.00741   0.00215  -0.1007   0.3345   1.0000
   3.500   0.8291   0.00782   0.00235  -0.0997   0.2918   1.0000
   3.750   0.8521   0.00817   0.00255  -0.0988   0.2596   1.0000
   4.000   0.8743   0.00859   0.00279  -0.0978   0.2225   1.0000
   4.250   0.8965   0.00902   0.00304  -0.0969   0.1884   1.0000
   4.500   0.9151   0.00975   0.00344  -0.0953   0.1240   1.0000
   4.750   0.9352   0.01037   0.00385  -0.0940   0.0836   1.0000
   5.000   0.9594   0.01063   0.00408  -0.0934   0.0739   1.0000
   5.250   0.9777   0.01139   0.00458  -0.0918   0.0229   1.0000
   5.500   1.0012   0.01171   0.00488  -0.0910   0.0150   1.0000
   5.750   1.0247   0.01201   0.00520  -0.0902   0.0120   1.0000
   6.000   1.0482   0.01230   0.00551  -0.0895   0.0103   1.0000
   6.250   1.0716   0.01259   0.00582  -0.0887   0.0093   1.0000
   6.500   1.0943   0.01292   0.00616  -0.0879   0.0083   1.0000
   6.750   1.1160   0.01333   0.00660  -0.0868   0.0073   1.0000
   7.000   1.1379   0.01371   0.00703  -0.0858   0.0068   1.0000
   7.250   1.1600   0.01405   0.00739  -0.0849   0.0063   1.0000
   7.500   1.1815   0.01442   0.00778  -0.0838   0.0058   1.0000
   7.750   1.2025   0.01481   0.00819  -0.0827   0.0053   1.0000
   8.000   1.2218   0.01532   0.00873  -0.0813   0.0049   1.0000
   8.250   1.2403   0.01587   0.00933  -0.0798   0.0046   1.0000
   8.500   1.2593   0.01635   0.00985  -0.0783   0.0044   1.0000
   8.750   1.2769   0.01684   0.01042  -0.0767   0.0042   1.0000
   9.000   1.2922   0.01739   0.01103  -0.0746   0.0040   1.0000
   9.250   1.3080   0.01787   0.01154  -0.0726   0.0038   1.0000
   9.500   1.3212   0.01850   0.01224  -0.0702   0.0037   1.0000
   9.750   1.3351   0.01910   0.01288  -0.0681   0.0036   1.0000
  10.000   1.3487   0.01972   0.01354  -0.0659   0.0034   1.0000
  10.250   1.3604   0.02045   0.01433  -0.0636   0.0033   1.0000
  10.500   1.3666   0.02153   0.01549  -0.0605   0.0030   1.0000
  10.750   1.3781   0.02231   0.01634  -0.0583   0.0030   1.0000
  11.000   1.3874   0.02324   0.01735  -0.0560   0.0029   1.0000
  11.250   1.3951   0.02431   0.01851  -0.0535   0.0028   1.0000
  11.500   1.4039   0.02533   0.01964  -0.0514   0.0027   1.0000
  11.750   1.4109   0.02652   0.02091  -0.0492   0.0026   1.0000
  12.000   1.4164   0.02787   0.02236  -0.0470   0.0026   1.0000
  12.250   1.4206   0.02938   0.02396  -0.0448   0.0025   1.0000
  12.500   1.4256   0.03089   0.02557  -0.0430   0.0024   1.0000
  12.750   1.4294   0.03258   0.02735  -0.0412   0.0024   1.0000
  13.000   1.4298   0.03465   0.02953  -0.0394   0.0024   1.0000
  13.250   1.4287   0.03699   0.03199  -0.0379   0.0023   1.0000
  13.500   1.4338   0.03881   0.03389  -0.0369   0.0023   1.0000
  13.750   1.4329   0.04136   0.03655  -0.0359   0.0022   1.0000
  14.000   1.4351   0.04369   0.03897  -0.0353   0.0022   1.0000
  14.250   1.4354   0.04632   0.04170  -0.0348   0.0021   1.0000
  14.500   1.4346   0.04920   0.04469  -0.0346   0.0021   1.0000
  14.750   1.4325   0.05241   0.04802  -0.0347   0.0021   1.0000
  15.000   1.4246   0.05648   0.05223  -0.0350   0.0021   1.0000
  15.250   1.4151   0.06099   0.05689  -0.0356   0.0021   1.0000
  15.500   1.4217   0.06347   0.05941  -0.0364   0.0020   1.0000
  15.750   1.4101   0.06859   0.06468  -0.0376   0.0020   1.0000
  16.000   1.4019   0.07342   0.06963  -0.0391   0.0020   1.0000
  16.250   1.3957   0.07816   0.07448  -0.0408   0.0019   1.0000
  16.500   1.3836   0.08397   0.08043  -0.0429   0.0019   1.0000
  16.750   1.3708   0.09005   0.08665  -0.0453   0.0019   1.0000
  17.000   1.3616   0.09578   0.09249  -0.0479   0.0019   1.0000
  17.250   1.3481   0.10238   0.09923  -0.0508   0.0019   1.0000
  17.500   1.3362   0.10890   0.10587  -0.0540   0.0019   1.0000
  17.750   1.3227   0.11587   0.11298  -0.0575   0.0019   1.0000
  18.000   1.3087   0.12315   0.12038  -0.0613   0.0019   1.0000
  18.250   1.2960   0.13033   0.12770  -0.0651   0.0019   1.0000
  18.500   1.2837   0.13757   0.13505  -0.0691   0.0019   1.0000
  18.750   1.2696   0.14540   0.14301  -0.0736   0.0019   1.0000
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