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GOE 602 AIRFOIL (goe602-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 602 AIRFOIL (goe602-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.86 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe602-il-1000000-n5.txt
Download as CSV file: xf-goe602-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 602 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.4108   0.13023   0.12850  -0.0288   1.0000   0.0036
 -12.250  -0.4099   0.12624   0.12452  -0.0298   1.0000   0.0037
 -11.750  -0.7901   0.03177   0.02945  -0.0900   0.9891   0.0036
 -11.500  -0.7757   0.02744   0.02476  -0.0932   0.9865   0.0037
 -11.250  -0.7601   0.02487   0.02193  -0.0939   0.9820   0.0038
 -11.000  -0.7375   0.02294   0.01978  -0.0950   0.9793   0.0039
 -10.750  -0.7127   0.02113   0.01773  -0.0963   0.9775   0.0040
 -10.500  -0.6888   0.01976   0.01618  -0.0968   0.9744   0.0042
 -10.250  -0.6635   0.01877   0.01504  -0.0972   0.9707   0.0043
 -10.000  -0.6358   0.01759   0.01366  -0.0982   0.9681   0.0044
  -9.750  -0.6076   0.01629   0.01217  -0.0994   0.9660   0.0047
  -9.500  -0.5828   0.01541   0.01118  -0.0994   0.9614   0.0049
  -9.250  -0.5553   0.01466   0.01032  -0.0999   0.9573   0.0051
  -9.000  -0.5256   0.01402   0.00957  -0.1008   0.9542   0.0054
  -8.750  -0.4980   0.01338   0.00882  -0.1011   0.9500   0.0057
  -8.500  -0.4712   0.01282   0.00816  -0.1012   0.9448   0.0060
  -8.250  -0.4423   0.01229   0.00753  -0.1017   0.9403   0.0063
  -8.000  -0.4150   0.01184   0.00698  -0.1019   0.9352   0.0065
  -7.750  -0.3890   0.01126   0.00628  -0.1017   0.9294   0.0071
  -7.250  -0.3352   0.01047   0.00536  -0.1016   0.9184   0.0083
  -7.000  -0.3083   0.01016   0.00497  -0.1016   0.9127   0.0091
  -6.750  -0.2817   0.00982   0.00458  -0.1014   0.9071   0.0103
  -6.500  -0.2554   0.00955   0.00428  -0.1011   0.9007   0.0117
  -6.250  -0.2283   0.00932   0.00401  -0.1010   0.8948   0.0132
  -6.000  -0.2020   0.00911   0.00377  -0.1007   0.8880   0.0152
  -5.500  -0.1479   0.00891   0.00354  -0.1004   0.8731   0.0193
  -5.250  -0.1208   0.00886   0.00344  -0.1002   0.8651   0.0200
  -5.000  -0.0947   0.00861   0.00312  -0.0999   0.8565   0.0213
  -4.750  -0.0683   0.00842   0.00288  -0.0996   0.8485   0.0231
  -4.500  -0.0418   0.00829   0.00271  -0.0993   0.8396   0.0244
  -4.250  -0.0151   0.00816   0.00254  -0.0991   0.8303   0.0257
  -4.000   0.0114   0.00804   0.00235  -0.0987   0.8202   0.0270
  -3.750   0.0378   0.00794   0.00219  -0.0984   0.8091   0.0282
  -3.500   0.0641   0.00784   0.00203  -0.0980   0.7968   0.0289
  -3.250   0.0903   0.00778   0.00190  -0.0977   0.7829   0.0295
  -3.000   0.1163   0.00772   0.00176  -0.0972   0.7684   0.0298
  -2.750   0.1421   0.00760   0.00154  -0.0967   0.7540   0.0313
  -2.500   0.1679   0.00754   0.00140  -0.0963   0.7389   0.0328
  -2.250   0.1939   0.00750   0.00128  -0.0958   0.7239   0.0341
  -1.750   0.2459   0.00746   0.00112  -0.0950   0.6945   0.0376
  -1.500   0.2719   0.00745   0.00106  -0.0946   0.6796   0.0404
  -1.250   0.2978   0.00742   0.00101  -0.0942   0.6651   0.0529
  -1.000   0.3233   0.00730   0.00097  -0.0938   0.6505   0.0959
  -0.750   0.3487   0.00720   0.00095  -0.0933   0.6350   0.1386
  -0.500   0.3727   0.00692   0.00093  -0.0928   0.6180   0.2539
   0.000   0.4212   0.00702   0.00098  -0.0914   0.5612   0.3240
   0.250   0.4456   0.00709   0.00102  -0.0908   0.5331   0.3558
   0.500   0.4699   0.00707   0.00106  -0.0902   0.5084   0.4164
   0.750   0.4940   0.00698   0.00112  -0.0896   0.4892   0.5018
   1.000   0.5181   0.00689   0.00120  -0.0889   0.4717   0.5863
   1.250   0.5407   0.00668   0.00129  -0.0879   0.4578   0.7104
   1.500   0.5584   0.00635   0.00142  -0.0856   0.4452   0.8709
   1.750   0.5878   0.00636   0.00152  -0.0858   0.4302   0.9456
   2.000   0.6277   0.00651   0.00161  -0.0886   0.4135   0.9704
   2.250   0.6655   0.00667   0.00169  -0.0910   0.3981   0.9868
   2.500   0.6991   0.00683   0.00179  -0.0924   0.3844   0.9995
   2.750   0.7232   0.00699   0.00189  -0.0917   0.3686   1.0000
   3.000   0.7471   0.00716   0.00199  -0.0909   0.3543   1.0000
   3.250   0.7707   0.00735   0.00210  -0.0901   0.3361   1.0000
   3.500   0.7939   0.00759   0.00225  -0.0893   0.3153   1.0000
   3.750   0.8175   0.00780   0.00239  -0.0885   0.2967   1.0000
   4.000   0.8384   0.00822   0.00260  -0.0873   0.2574   1.0000
   4.250   0.8605   0.00857   0.00282  -0.0862   0.2282   1.0000
   4.500   0.8800   0.00911   0.00312  -0.0848   0.1808   1.0000
   4.750   0.8961   0.00994   0.00358  -0.0828   0.1087   1.0000
   5.000   0.9179   0.01033   0.00386  -0.0818   0.0890   1.0000
   5.250   0.9411   0.01062   0.00411  -0.0810   0.0792   1.0000
   5.500   0.9645   0.01088   0.00436  -0.0803   0.0700   1.0000
   5.750   0.9824   0.01157   0.00483  -0.0786   0.0266   1.0000
   6.000   1.0046   0.01192   0.00517  -0.0776   0.0172   1.0000
   6.250   1.0274   0.01222   0.00547  -0.0768   0.0144   1.0000
   6.500   1.0494   0.01257   0.00582  -0.0758   0.0114   1.0000
   6.750   1.0718   0.01287   0.00615  -0.0749   0.0103   1.0000
   7.000   1.0939   0.01319   0.00649  -0.0740   0.0093   1.0000
   7.250   1.1153   0.01355   0.00686  -0.0729   0.0084   1.0000
   7.500   1.1352   0.01401   0.00734  -0.0716   0.0073   1.0000
   7.750   1.1564   0.01434   0.00770  -0.0705   0.0069   1.0000
   8.000   1.1769   0.01471   0.00812  -0.0693   0.0063   1.0000
   8.250   1.1965   0.01512   0.00855  -0.0680   0.0059   1.0000
   8.500   1.2150   0.01555   0.00901  -0.0665   0.0055   1.0000
   8.750   1.2305   0.01607   0.00957  -0.0644   0.0052   1.0000
   9.000   1.2452   0.01662   0.01017  -0.0622   0.0049   1.0000
   9.250   1.2608   0.01711   0.01071  -0.0602   0.0047   1.0000
   9.500   1.2761   0.01761   0.01127  -0.0582   0.0045   1.0000
   9.750   1.2906   0.01817   0.01187  -0.0562   0.0043   1.0000
  10.000   1.3038   0.01880   0.01259  -0.0540   0.0041   1.0000
  10.250   1.3188   0.01933   0.01315  -0.0521   0.0038   1.0000
  10.500   1.3321   0.01997   0.01383  -0.0501   0.0037   1.0000
  10.750   1.3439   0.02070   0.01461  -0.0480   0.0035   1.0000
  11.000   1.3501   0.02179   0.01578  -0.0451   0.0033   1.0000
  11.250   1.3590   0.02274   0.01681  -0.0428   0.0032   1.0000
  11.500   1.3687   0.02367   0.01781  -0.0407   0.0032   1.0000
  11.750   1.3777   0.02467   0.01890  -0.0386   0.0031   1.0000
  12.000   1.3841   0.02588   0.02020  -0.0364   0.0030   1.0000
  12.250   1.3910   0.02711   0.02151  -0.0344   0.0030   1.0000
  12.500   1.3964   0.02850   0.02299  -0.0324   0.0029   1.0000
  12.750   1.4008   0.03003   0.02462  -0.0305   0.0028   1.0000
  13.000   1.4045   0.03168   0.02639  -0.0288   0.0027   1.0000
  13.250   1.4049   0.03372   0.02853  -0.0270   0.0027   1.0000
  13.500   1.4104   0.03538   0.03028  -0.0259   0.0026   1.0000
  13.750   1.4129   0.03741   0.03240  -0.0248   0.0026   1.0000
  14.000   1.4107   0.04001   0.03512  -0.0237   0.0026   1.0000
  14.250   1.4091   0.04269   0.03792  -0.0230   0.0025   1.0000
  14.500   1.4157   0.04459   0.03987  -0.0227   0.0024   1.0000
  14.750   1.4177   0.04707   0.04244  -0.0224   0.0023   1.0000
  15.000   1.4100   0.05085   0.04636  -0.0224   0.0023   1.0000
  15.250   1.4085   0.05403   0.04964  -0.0227   0.0023   1.0000
  15.500   1.4040   0.05773   0.05346  -0.0232   0.0023   1.0000
  15.750   1.3993   0.06162   0.05746  -0.0240   0.0022   1.0000
  16.000   1.3942   0.06573   0.06167  -0.0250   0.0022   1.0000
  16.250   1.3890   0.06999   0.06602  -0.0263   0.0021   1.0000
  16.500   1.3775   0.07530   0.07148  -0.0280   0.0022   1.0000
  16.750   1.3684   0.08049   0.07677  -0.0300   0.0021   1.0000
  17.000   1.3580   0.08602   0.08243  -0.0321   0.0021   1.0000
  17.250   1.3458   0.09197   0.08852  -0.0345   0.0021   1.0000
  17.500   1.3304   0.09873   0.09541  -0.0376   0.0020   1.0000
  17.750   1.3201   0.10472   0.10153  -0.0404   0.0021   1.0000
  18.000   1.3080   0.11116   0.10809  -0.0435   0.0021   1.0000
  18.250   1.2928   0.11839   0.11545  -0.0471   0.0021   1.0000
  18.500   1.2787   0.12559   0.12278  -0.0509   0.0020   1.0000
  18.750   1.2649   0.13290   0.13021  -0.0548   0.0020   1.0000
  19.000   1.2545   0.13958   0.13700  -0.0585   0.0020   1.0000
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