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GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 648 AIRFOIL (goe648-il)
Reynolds number: 200,000
Max Cl/Cd: 57.57 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe648-il-200000-n5.txt
Download as CSV file: xf-goe648-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 648 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.7041   0.05715   0.05243  -0.0812   1.0000   0.0319
 -13.250  -0.7419   0.04974   0.04479  -0.0857   1.0000   0.0318
 -13.000  -0.7678   0.04522   0.04010  -0.0871   1.0000   0.0320
 -12.750  -0.7924   0.04201   0.03675  -0.0862   1.0000   0.0321
 -12.500  -0.8174   0.03992   0.03454  -0.0830   1.0000   0.0323
 -12.250  -0.8447   0.03863   0.03315  -0.0772   1.0000   0.0324
 -12.000  -0.8474   0.03655   0.03082  -0.0758   0.9971   0.0331
 -11.750  -0.8297   0.03420   0.02817  -0.0775   0.9917   0.0340
 -11.500  -0.8061   0.03306   0.02702  -0.0785   0.9868   0.0346
 -11.250  -0.7795   0.03196   0.02585  -0.0800   0.9827   0.0356
 -11.000  -0.7578   0.03064   0.02436  -0.0805   0.9771   0.0366
 -10.750  -0.7337   0.02915   0.02259  -0.0813   0.9719   0.0379
 -10.500  -0.7053   0.02797   0.02132  -0.0826   0.9678   0.0389
 -10.250  -0.6814   0.02717   0.02049  -0.0827   0.9608   0.0399
 -10.000  -0.6513   0.02624   0.01945  -0.0839   0.9568   0.0412
  -9.750  -0.6265   0.02525   0.01827  -0.0839   0.9510   0.0427
  -9.500  -0.6007   0.02433   0.01725  -0.0841   0.9452   0.0439
  -9.250  -0.5694   0.02361   0.01651  -0.0852   0.9417   0.0451
  -9.000  -0.5424   0.02292   0.01575  -0.0854   0.9365   0.0466
  -8.750  -0.5167   0.02217   0.01484  -0.0852   0.9302   0.0484
  -8.500  -0.4851   0.02144   0.01407  -0.0862   0.9265   0.0499
  -8.250  -0.4501   0.02081   0.01341  -0.0878   0.9238   0.0516
  -8.000  -0.4289   0.02030   0.01283  -0.0866   0.9151   0.0535
  -7.750  -0.3973   0.01964   0.01209  -0.0874   0.9105   0.0556
  -7.500  -0.3629   0.01908   0.01152  -0.0888   0.9072   0.0577
  -7.250  -0.3399   0.01863   0.01101  -0.0878   0.8985   0.0599
  -7.000  -0.3084   0.01807   0.01039  -0.0885   0.8931   0.0627
  -6.750  -0.2759   0.01759   0.00990  -0.0894   0.8880   0.0656
  -6.500  -0.2497   0.01719   0.00942  -0.0889   0.8787   0.0688
  -6.250  -0.2146   0.01661   0.00881  -0.0903   0.8723   0.0721
  -6.000  -0.1895   0.01625   0.00842  -0.0896   0.8611   0.0757
  -5.750  -0.1573   0.01580   0.00790  -0.0902   0.8523   0.0800
  -5.500  -0.1309   0.01543   0.00751  -0.0898   0.8412   0.0839
  -5.250  -0.1022   0.01511   0.00711  -0.0898   0.8311   0.0883
  -5.000  -0.0748   0.01473   0.00672  -0.0895   0.8202   0.0930
  -4.750  -0.0489   0.01447   0.00641  -0.0889   0.8088   0.0982
  -4.500  -0.0212   0.01417   0.00608  -0.0887   0.7977   0.1039
  -4.250   0.0038   0.01394   0.00581  -0.0879   0.7844   0.1108
  -4.000   0.0286   0.01369   0.00556  -0.0871   0.7703   0.1189
  -3.750   0.0539   0.01347   0.00532  -0.0863   0.7558   0.1293
  -3.500   0.0790   0.01325   0.00508  -0.0855   0.7414   0.1436
  -3.250   0.1035   0.01302   0.00489  -0.0847   0.7276   0.1627
  -3.000   0.1276   0.01281   0.00471  -0.0837   0.7131   0.1881
  -2.750   0.1516   0.01260   0.00457  -0.0828   0.6980   0.2185
  -2.500   0.1757   0.01243   0.00443  -0.0819   0.6822   0.2508
  -2.250   0.1996   0.01229   0.00431  -0.0809   0.6663   0.2837
  -2.000   0.2234   0.01217   0.00421  -0.0799   0.6510   0.3161
  -1.750   0.2468   0.01206   0.00413  -0.0788   0.6361   0.3503
  -1.500   0.2695   0.01194   0.00408  -0.0776   0.6210   0.3926
  -1.250   0.2918   0.01183   0.00407  -0.0763   0.6055   0.4422
  -1.000   0.3141   0.01177   0.00408  -0.0749   0.5897   0.4905
  -0.750   0.3362   0.01174   0.00411  -0.0735   0.5736   0.5363
  -0.500   0.3582   0.01173   0.00414  -0.0721   0.5574   0.5783
  -0.250   0.3798   0.01172   0.00417  -0.0705   0.5413   0.6172
   0.000   0.4009   0.01172   0.00423  -0.0688   0.5247   0.6572
   0.250   0.4216   0.01174   0.00431  -0.0670   0.5070   0.6997
   0.500   0.4423   0.01179   0.00439  -0.0652   0.4877   0.7407
   0.750   0.4633   0.01186   0.00446  -0.0635   0.4667   0.7821
   1.000   0.4858   0.01197   0.00454  -0.0621   0.4444   0.8188
   1.250   0.5140   0.01213   0.00465  -0.0620   0.4225   0.8561
   1.500   0.5541   0.01239   0.00483  -0.0644   0.4014   0.8961
   1.750   0.6044   0.01273   0.00503  -0.0691   0.3821   0.9339
   2.250   0.6912   0.01342   0.00545  -0.0758   0.3564   1.0000
   2.750   0.7277   0.01388   0.00572  -0.0721   0.3424   1.0000
   3.000   0.7465   0.01412   0.00587  -0.0704   0.3360   1.0000
   3.250   0.7651   0.01441   0.00605  -0.0686   0.3305   1.0000
   3.500   0.7859   0.01461   0.00623  -0.0672   0.3253   1.0000
   3.750   0.8061   0.01485   0.00641  -0.0657   0.3201   1.0000
   4.000   0.8257   0.01514   0.00662  -0.0642   0.3154   1.0000
   4.250   0.8461   0.01542   0.00684  -0.0628   0.3113   1.0000
   4.500   0.8676   0.01564   0.00706  -0.0615   0.3069   1.0000
   4.750   0.8884   0.01590   0.00729  -0.0602   0.3027   1.0000
   5.000   0.9086   0.01620   0.00754  -0.0588   0.2985   1.0000
   5.250   0.9286   0.01655   0.00781  -0.0574   0.2946   1.0000
   5.500   0.9501   0.01678   0.00807  -0.0563   0.2910   1.0000
   5.750   0.9706   0.01703   0.00834  -0.0549   0.2872   1.0000
   6.000   0.9899   0.01731   0.00861  -0.0534   0.2832   1.0000
   6.250   1.0087   0.01764   0.00889  -0.0518   0.2795   1.0000
   6.500   1.0280   0.01799   0.00920  -0.0503   0.2760   1.0000
   6.750   1.0478   0.01825   0.00952  -0.0489   0.2724   1.0000
   7.000   1.0673   0.01854   0.00984  -0.0475   0.2687   1.0000
   7.250   1.0859   0.01887   0.01017  -0.0460   0.2650   1.0000
   7.500   1.1037   0.01924   0.01051  -0.0444   0.2614   1.0000
   7.750   1.1225   0.01960   0.01089  -0.0430   0.2579   1.0000
   8.000   1.1415   0.01993   0.01128  -0.0416   0.2540   1.0000
   8.250   1.1596   0.02029   0.01168  -0.0402   0.2502   1.0000
   8.500   1.1770   0.02069   0.01209  -0.0386   0.2467   1.0000
   8.750   1.1939   0.02114   0.01251  -0.0371   0.2436   1.0000
   9.000   1.2121   0.02155   0.01300  -0.0358   0.2401   1.0000
   9.250   1.2294   0.02196   0.01349  -0.0343   0.2361   1.0000
   9.500   1.2453   0.02243   0.01398  -0.0328   0.2322   1.0000
   9.750   1.2594   0.02295   0.01448  -0.0310   0.2283   1.0000
  10.000   1.2754   0.02346   0.01506  -0.0296   0.2242   1.0000
  10.250   1.2908   0.02399   0.01566  -0.0281   0.2198   1.0000
  10.500   1.3046   0.02458   0.01628  -0.0266   0.2158   1.0000
  10.750   1.3171   0.02526   0.01695  -0.0249   0.2124   1.0000
  11.000   1.3321   0.02589   0.01768  -0.0236   0.2083   1.0000
  11.250   1.3458   0.02658   0.01844  -0.0222   0.2042   1.0000
  11.500   1.3574   0.02737   0.01926  -0.0207   0.2003   1.0000
  11.750   1.3677   0.02825   0.02015  -0.0191   0.1968   1.0000
  12.000   1.3812   0.02906   0.02107  -0.0179   0.1929   1.0000
  12.250   1.3923   0.02998   0.02206  -0.0166   0.1890   1.0000
  12.500   1.4021   0.03101   0.02313  -0.0153   0.1857   1.0000
  12.750   1.4104   0.03217   0.02430  -0.0140   0.1826   1.0000
  13.000   1.4216   0.03322   0.02547  -0.0129   0.1791   1.0000
  13.250   1.4306   0.03442   0.02676  -0.0118   0.1755   1.0000
  13.500   1.4374   0.03580   0.02818  -0.0107   0.1720   1.0000
  13.750   1.4421   0.03736   0.02975  -0.0096   0.1688   1.0000
  14.000   1.4505   0.03877   0.03130  -0.0088   0.1652   1.0000
  14.250   1.4565   0.04037   0.03300  -0.0080   0.1617   1.0000
  14.500   1.4605   0.04219   0.03488  -0.0073   0.1586   1.0000
  14.750   1.4626   0.04422   0.03693  -0.0067   0.1558   1.0000
  15.000   1.4676   0.04611   0.03897  -0.0062   0.1529   1.0000
  15.250   1.4711   0.04821   0.04119  -0.0059   0.1496   1.0000
  15.500   1.4723   0.05058   0.04365  -0.0056   0.1465   1.0000
  15.750   1.4711   0.05325   0.04637  -0.0055   0.1436   1.0000
  16.000   1.4706   0.05596   0.04917  -0.0056   0.1408   1.0000
  16.250   1.4698   0.05883   0.05220  -0.0058   0.1373   1.0000
  16.500   1.4663   0.06206   0.05554  -0.0062   0.1340   1.0000
  16.750   1.4596   0.06572   0.05926  -0.0068   0.1308   1.0000
  17.000   1.4538   0.06943   0.06309  -0.0076   0.1276   1.0000
  17.250   1.4459   0.07354   0.06734  -0.0086   0.1239   1.0000
  17.500   1.4343   0.07822   0.07212  -0.0100   0.1203   1.0000
  17.750   1.4211   0.08320   0.07716  -0.0115   0.1171   1.0000
  18.000   1.4081   0.08839   0.08251  -0.0133   0.1133   1.0000
  18.250   1.3922   0.09406   0.08829  -0.0154   0.1096   1.0000
  18.500   1.3739   0.10018   0.09447  -0.0178   0.1061   1.0000
  18.750   1.3563   0.10639   0.10083  -0.0203   0.1023   1.0000
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