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GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 683 AIRFOIL (goe683-il)
Reynolds number: 100,000
Max Cl/Cd: 41.47 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe683-il-100000-n5.txt
Download as CSV file: xf-goe683-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 683 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6867   0.07271   0.06593  -0.0800   1.0000   0.0736
 -14.750  -0.7395   0.06386   0.05676  -0.0845   1.0000   0.0737
 -14.500  -0.7713   0.05856   0.05121  -0.0858   1.0000   0.0740
 -14.250  -0.7955   0.05462   0.04703  -0.0855   1.0000   0.0744
 -14.000  -0.8165   0.05141   0.04359  -0.0841   1.0000   0.0750
 -13.750  -0.8349   0.04882   0.04076  -0.0818   1.0000   0.0755
 -13.500  -0.8398   0.04691   0.03876  -0.0796   1.0000   0.0762
 -13.250  -0.8324   0.04561   0.03751  -0.0780   1.0000   0.0771
 -13.000  -0.8304   0.04429   0.03619  -0.0758   1.0000   0.0781
 -12.750  -0.8317   0.04298   0.03485  -0.0730   1.0000   0.0790
 -12.500  -0.8348   0.04174   0.03355  -0.0698   1.0000   0.0798
 -12.250  -0.8405   0.04064   0.03238  -0.0660   1.0000   0.0808
 -12.000  -0.8499   0.03978   0.03145  -0.0613   1.0000   0.0815
 -11.750  -0.8276   0.03798   0.02943  -0.0625   0.9867   0.0831
 -11.500  -0.8039   0.03644   0.02775  -0.0635   0.9721   0.0848
 -11.250  -0.7756   0.03521   0.02657  -0.0649   0.9590   0.0866
 -11.000  -0.7471   0.03397   0.02530  -0.0664   0.9471   0.0886
 -10.750  -0.7171   0.03269   0.02390  -0.0680   0.9355   0.0908
 -10.500  -0.6846   0.03142   0.02242  -0.0700   0.9247   0.0933
 -10.250  -0.6481   0.03023   0.02128  -0.0727   0.9153   0.0957
 -10.000  -0.6160   0.02922   0.02022  -0.0745   0.9027   0.0986
  -9.750  -0.5818   0.02821   0.01907  -0.0766   0.8909   0.1018
  -9.500  -0.5496   0.02728   0.01809  -0.0782   0.8783   0.1050
  -9.250  -0.5245   0.02657   0.01733  -0.0783   0.8636   0.1084
  -9.000  -0.4992   0.02590   0.01653  -0.0784   0.8499   0.1125
  -8.750  -0.4748   0.02527   0.01584  -0.0782   0.8375   0.1164
  -8.500  -0.4567   0.02479   0.01531  -0.0767   0.8233   0.1211
  -8.250  -0.4365   0.02429   0.01474  -0.0756   0.8111   0.1268
  -8.000  -0.4167   0.02383   0.01422  -0.0743   0.7996   0.1332
  -7.750  -0.3999   0.02342   0.01378  -0.0724   0.7875   0.1405
  -7.500  -0.3789   0.02300   0.01325  -0.0712   0.7779   0.1500
  -7.250  -0.3653   0.02266   0.01294  -0.0687   0.7664   0.1590
  -7.000  -0.3457   0.02230   0.01251  -0.0672   0.7575   0.1702
  -6.750  -0.3305   0.02206   0.01222  -0.0649   0.7466   0.1808
  -6.250  -0.2952   0.02158   0.01165  -0.0610   0.7283   0.2013
  -6.000  -0.2768   0.02135   0.01138  -0.0591   0.7202   0.2112
  -5.750  -0.2591   0.02117   0.01117  -0.0572   0.7110   0.2208
  -5.500  -0.2400   0.02098   0.01093  -0.0554   0.7027   0.2305
  -5.250  -0.2202   0.02080   0.01070  -0.0538   0.6946   0.2398
  -5.000  -0.2015   0.02064   0.01051  -0.0520   0.6859   0.2504
  -4.750  -0.1795   0.02042   0.01024  -0.0508   0.6792   0.2611
  -4.500  -0.1612   0.02032   0.01012  -0.0489   0.6703   0.2727
  -4.250  -0.1401   0.02010   0.00991  -0.0475   0.6629   0.2838
  -4.000  -0.1179   0.01994   0.00970  -0.0464   0.6554   0.2953
  -3.750  -0.0977   0.01976   0.00956  -0.0449   0.6472   0.3087
  -3.500  -0.0747   0.01953   0.00933  -0.0438   0.6407   0.3251
  -3.250  -0.0546   0.01938   0.00925  -0.0423   0.6328   0.3425
  -3.000  -0.0330   0.01917   0.00911  -0.0411   0.6253   0.3635
  -2.750  -0.0088   0.01894   0.00892  -0.0403   0.6191   0.3893
  -2.500   0.0109   0.01879   0.00892  -0.0387   0.6108   0.4183
  -2.250   0.0349   0.01858   0.00882  -0.0379   0.6039   0.4545
  -2.000   0.0617   0.01837   0.00872  -0.0376   0.5977   0.4971
  -1.750   0.0894   0.01819   0.00876  -0.0375   0.5897   0.5448
  -1.500   0.1258   0.01797   0.00873  -0.0390   0.5828   0.6033
  -1.250   0.1745   0.01793   0.00890  -0.0428   0.5753   0.6672
  -1.000   0.2389   0.01823   0.00936  -0.0494   0.5668   0.7248
  -0.750   0.3026   0.01877   0.00988  -0.0555   0.5601   0.7661
  -0.500   0.3451   0.01931   0.01046  -0.0577   0.5516   0.7947
  -0.250   0.3759   0.01968   0.01075  -0.0577   0.5452   0.8218
   0.000   0.4073   0.02011   0.01108  -0.0578   0.5395   0.8442
   0.250   0.4349   0.02056   0.01151  -0.0574   0.5325   0.8648
   0.500   0.4647   0.02093   0.01179  -0.0574   0.5264   0.8826
   0.750   0.4954   0.02127   0.01201  -0.0577   0.5210   0.8975
   1.000   0.5230   0.02166   0.01239  -0.0576   0.5142   0.9115
   1.250   0.5537   0.02198   0.01264  -0.0580   0.5083   0.9243
   1.500   0.5977   0.02226   0.01278  -0.0611   0.5033   0.9349
   1.750   0.6373   0.02261   0.01316  -0.0634   0.4962   0.9475
   2.000   0.6762   0.02281   0.01328  -0.0657   0.4902   0.9580
   2.250   0.7115   0.02293   0.01329  -0.0674   0.4856   0.9665
   2.500   0.7475   0.02300   0.01338  -0.0694   0.4796   0.9728
   2.750   0.7790   0.02315   0.01351  -0.0705   0.4739   0.9803
   3.000   0.8182   0.02303   0.01330  -0.0731   0.4689   0.9857
   3.250   0.8535   0.02309   0.01332  -0.0750   0.4641   0.9921
   3.500   0.8912   0.02302   0.01329  -0.0776   0.4583   0.9982
   3.750   0.9153   0.02313   0.01336  -0.0773   0.4535   1.0000
   4.000   0.9340   0.02330   0.01346  -0.0759   0.4497   1.0000
   4.250   0.9510   0.02355   0.01370  -0.0742   0.4457   1.0000
   4.500   0.9653   0.02389   0.01411  -0.0721   0.4410   1.0000
   4.750   0.9815   0.02418   0.01440  -0.0702   0.4367   1.0000
   5.000   0.9996   0.02441   0.01460  -0.0687   0.4328   1.0000
   5.250   1.0202   0.02463   0.01474  -0.0675   0.4296   1.0000
   5.500   1.0319   0.02508   0.01529  -0.0650   0.4251   1.0000
   5.750   1.0453   0.02549   0.01576  -0.0627   0.4207   1.0000
   6.000   1.0612   0.02580   0.01607  -0.0608   0.4165   1.0000
   6.250   1.0801   0.02605   0.01628  -0.0593   0.4129   1.0000
   6.500   1.0956   0.02642   0.01665  -0.0574   0.4090   1.0000
   6.750   1.1033   0.02697   0.01732  -0.0542   0.4042   1.0000
   7.000   1.1152   0.02736   0.01774  -0.0517   0.3994   1.0000
   7.250   1.1317   0.02763   0.01798  -0.0498   0.3955   1.0000
   7.500   1.1499   0.02791   0.01822  -0.0483   0.3919   1.0000
   7.750   1.1513   0.02863   0.01909  -0.0442   0.3875   1.0000
   8.000   1.1571   0.02920   0.01973  -0.0408   0.3833   1.0000
   8.250   1.1680   0.02962   0.02017  -0.0381   0.3795   1.0000
   8.500   1.1846   0.02992   0.02046  -0.0364   0.3763   1.0000
   8.750   1.1921   0.03045   0.02102  -0.0333   0.3728   1.0000
   9.000   1.1796   0.03129   0.02200  -0.0270   0.3688   1.0000
   9.250   1.1734   0.03199   0.02277  -0.0219   0.3650   1.0000
   9.500   1.1781   0.03252   0.02333  -0.0185   0.3615   1.0000
   9.750   1.1933   0.03281   0.02361  -0.0166   0.3584   1.0000
  10.000   1.1950   0.03357   0.02442  -0.0131   0.3553   1.0000
  10.250   1.1724   0.03523   0.02624  -0.0070   0.3514   1.0000
  10.500   1.1622   0.03666   0.02777  -0.0029   0.3474   1.0000
  10.750   1.1681   0.03742   0.02856  -0.0004   0.3435   1.0000
  11.000   1.1899   0.03746   0.02856   0.0005   0.3403   1.0000
  11.250   1.1592   0.04027   0.03155   0.0055   0.3356   1.0000
  11.500   1.1292   0.04354   0.03497   0.0096   0.3302   1.0000
  11.750   1.1362   0.04452   0.03597   0.0113   0.3262   1.0000
  12.000   1.1658   0.04390   0.03529   0.0118   0.3231   1.0000
  12.250   1.0591   0.05450   0.04621   0.0167   0.3134   1.0000
  12.500   1.0756   0.05473   0.04644   0.0178   0.3094   1.0000
  12.750   1.1107   0.05326   0.04494   0.0185   0.3069   1.0000
  13.000   0.9876   0.06859   0.06052   0.0196   0.2927   1.0000
  13.250   1.0209   0.06687   0.05879   0.0207   0.2911   1.0000
  13.500   1.0585   0.06473   0.05665   0.0218   0.2897   1.0000
  13.750   0.9669   0.07836   0.07044   0.0208   0.2747   1.0000
  14.000   0.9993   0.07654   0.06863   0.0221   0.2735   1.0000
  14.500   0.9639   0.08629   0.07852   0.0217   0.2576   1.0000
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