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GOE 514 AIRFOIL (goe514-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 514 AIRFOIL (goe514-il)
Reynolds number: 200,000
Max Cl/Cd: 57.19 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe514-il-200000.txt
Download as CSV file: xf-goe514-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 514 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4372   0.07106   0.06775  -0.0854   0.9657   0.0389
 -10.500  -0.5336   0.05603   0.05237  -0.0936   0.9501   0.0371
 -10.250  -0.5703   0.04711   0.04270  -0.0945   0.9414   0.0369
 -10.000  -0.5851   0.04405   0.03930  -0.0900   0.9297   0.0371
  -9.750  -0.5732   0.04054   0.03531  -0.0900   0.9261   0.0377
  -9.500  -0.5795   0.03866   0.03315  -0.0850   0.9150   0.0381
  -9.250  -0.5605   0.03615   0.03015  -0.0846   0.9113   0.0390
  -9.000  -0.5568   0.03466   0.02834  -0.0807   0.9020   0.0397
  -8.750  -0.5327   0.03324   0.02694  -0.0806   0.8975   0.0410
  -8.500  -0.5019   0.03224   0.02583  -0.0815   0.8948   0.0433
  -8.250  -0.4925   0.03140   0.02477  -0.0782   0.8860   0.0448
  -8.000  -0.4667   0.03002   0.02327  -0.0779   0.8811   0.0471
  -7.750  -0.4299   0.02891   0.02209  -0.0795   0.8785   0.0501
  -7.500  -0.4149   0.02812   0.02106  -0.0768   0.8699   0.0527
  -7.250  -0.3856   0.02710   0.02013  -0.0770   0.8649   0.0568
  -7.000  -0.3487   0.02591   0.01884  -0.0785   0.8624   0.0634
  -6.750  -0.3103   0.02465   0.01752  -0.0802   0.8607   0.0727
  -6.500  -0.3024   0.02425   0.01701  -0.0763   0.8495   0.0792
  -6.250  -0.2659   0.02302   0.01576  -0.0776   0.8468   0.0909
  -6.000  -0.2254   0.02205   0.01480  -0.0797   0.8451   0.1030
  -5.750  -0.1906   0.02152   0.01432  -0.0806   0.8420   0.1137
  -5.250  -0.1384   0.02096   0.01371  -0.0791   0.8301   0.1322
  -5.000  -0.0964   0.02049   0.01315  -0.0813   0.8286   0.1450
  -4.750  -0.0883   0.02048   0.01320  -0.0773   0.8179   0.1517
  -4.500  -0.0495   0.01980   0.01248  -0.0789   0.8150   0.1650
  -4.250  -0.0068   0.01913   0.01179  -0.0813   0.8130   0.1799
  -4.000   0.0074   0.01905   0.01166  -0.0782   0.8036   0.1897
  -3.750   0.0442   0.01860   0.01125  -0.0795   0.7993   0.2007
  -3.500   0.0912   0.01806   0.01061  -0.0828   0.7962   0.2119
  -3.250   0.1052   0.01801   0.01057  -0.0797   0.7859   0.2175
  -3.000   0.1501   0.01753   0.00991  -0.0826   0.7812   0.2261
  -2.750   0.1757   0.01731   0.00973  -0.0819   0.7720   0.2313
  -2.500   0.2199   0.01693   0.00924  -0.0847   0.7645   0.2387
  -2.250   0.2463   0.01668   0.00888  -0.0842   0.7538   0.2439
  -2.000   0.2965   0.01637   0.00854  -0.0884   0.7449   0.2505
  -1.750   0.3204   0.01623   0.00829  -0.0874   0.7324   0.2557
  -1.500   0.3483   0.01605   0.00798  -0.0871   0.7195   0.2608
  -1.250   0.3800   0.01591   0.00781  -0.0877   0.7060   0.2660
  -1.000   0.4086   0.01586   0.00764  -0.0876   0.6915   0.2730
  -0.750   0.4339   0.01578   0.00743  -0.0869   0.6762   0.2793
  -0.500   0.4537   0.01573   0.00734  -0.0851   0.6601   0.2847
  -0.250   0.4689   0.01570   0.00721  -0.0823   0.6427   0.2905
   0.000   0.4812   0.01566   0.00705  -0.0789   0.6240   0.2964
   0.250   0.4920   0.01564   0.00700  -0.0752   0.6043   0.3018
   0.500   0.5030   0.01571   0.00695  -0.0716   0.5844   0.3094
   0.750   0.5159   0.01577   0.00691  -0.0685   0.5650   0.3166
   1.000   0.5300   0.01590   0.00694  -0.0657   0.5475   0.3252
   1.250   0.5455   0.01602   0.00696  -0.0633   0.5318   0.3341
   1.500   0.5627   0.01619   0.00701  -0.0612   0.5184   0.3441
   1.750   0.5811   0.01631   0.00706  -0.0594   0.5063   0.3528
   2.000   0.5992   0.01649   0.00717  -0.0575   0.4955   0.3629
   2.250   0.6203   0.01661   0.00723  -0.0563   0.4860   0.3725
   2.500   0.6389   0.01675   0.00735  -0.0546   0.4769   0.3824
   2.750   0.6630   0.01692   0.00744  -0.0540   0.4693   0.3937
   3.000   0.6813   0.01701   0.00759  -0.0523   0.4620   0.4034
   3.250   0.7055   0.01716   0.00768  -0.0518   0.4556   0.4155
   3.500   0.7261   0.01729   0.00783  -0.0505   0.4498   0.4278
   3.750   0.7439   0.01739   0.00799  -0.0487   0.4438   0.4425
   4.000   0.7680   0.01745   0.00808  -0.0482   0.4384   0.4729
   4.250   1.0851   0.01907   0.01066  -0.1096   0.4201   1.0000
   4.500   1.1025   0.01936   0.01094  -0.1078   0.4163   1.0000
   4.750   1.1135   0.01959   0.01119  -0.1047   0.4123   1.0000
   5.000   1.1296   0.01985   0.01142  -0.1027   0.4083   1.0000
   5.250   1.1519   0.02019   0.01167  -0.1019   0.4042   1.0000
   5.500   1.1809   0.02065   0.01207  -0.1026   0.4002   1.0000
   5.750   1.1887   0.02088   0.01236  -0.0989   0.3972   1.0000
   6.000   1.2013   0.02115   0.01266  -0.0962   0.3938   1.0000
   6.250   1.2191   0.02147   0.01297  -0.0945   0.3905   1.0000
   6.500   1.2428   0.02183   0.01329  -0.0941   0.3873   1.0000
   6.750   1.2820   0.02246   0.01382  -0.0969   0.3837   1.0000
   7.000   1.2828   0.02268   0.01415  -0.0918   0.3810   1.0000
   7.250   1.2895   0.02296   0.01451  -0.0880   0.3779   1.0000
   7.500   1.3031   0.02329   0.01487  -0.0856   0.3748   1.0000
   7.750   1.3217   0.02363   0.01520  -0.0842   0.3717   1.0000
   8.000   1.3507   0.02407   0.01558  -0.0848   0.3686   1.0000
   8.250   1.3690   0.02457   0.01611  -0.0835   0.3653   1.0000
   8.500   1.3667   0.02484   0.01649  -0.0780   0.3622   1.0000
   8.750   1.3736   0.02517   0.01689  -0.0745   0.3588   1.0000
   9.000   1.3876   0.02550   0.01723  -0.0723   0.3555   1.0000
   9.250   1.4101   0.02584   0.01753  -0.0717   0.3523   1.0000
   9.500   1.4374   0.02639   0.01805  -0.0722   0.3490   1.0000
   9.750   1.4321   0.02679   0.01861  -0.0665   0.3461   1.0000
  10.000   1.4357   0.02721   0.01914  -0.0626   0.3427   1.0000
  10.250   1.4465   0.02760   0.01957  -0.0601   0.3394   1.0000
  10.500   1.4654   0.02794   0.01990  -0.0590   0.3364   1.0000
  10.750   1.4996   0.02839   0.02028  -0.0606   0.3332   1.0000
  11.000   1.4972   0.02903   0.02109  -0.0560   0.3307   1.0000
  11.250   1.4955   0.02967   0.02188  -0.0516   0.3276   1.0000
  11.500   1.5007   0.03020   0.02250  -0.0485   0.3241   1.0000
  11.750   1.5133   0.03050   0.02280  -0.0465   0.3204   1.0000
  12.000   1.5380   0.03073   0.02292  -0.0465   0.3160   1.0000
  12.250   1.5275   0.03166   0.02407  -0.0412   0.3129   1.0000
  12.500   1.5250   0.03245   0.02499  -0.0374   0.3091   1.0000
  12.750   1.5316   0.03290   0.02546  -0.0349   0.3047   1.0000
  13.000   1.5549   0.03305   0.02551  -0.0346   0.3005   1.0000
  13.250   1.5472   0.03429   0.02694  -0.0306   0.2975   1.0000
  13.500   1.5410   0.03548   0.02830  -0.0269   0.2934   1.0000
  13.750   1.5456   0.03630   0.02918  -0.0247   0.2894   1.0000
  14.000   1.5615   0.03660   0.02941  -0.0236   0.2851   1.0000
  14.250   1.5531   0.03822   0.03121  -0.0203   0.2812   1.0000
  14.500   1.5455   0.03987   0.03302  -0.0174   0.2767   1.0000
  14.750   1.5479   0.04098   0.03416  -0.0155   0.2720   1.0000
  15.000   1.5554   0.04197   0.03516  -0.0141   0.2676   1.0000
  15.250   1.5429   0.04444   0.03784  -0.0116   0.2630   1.0000
  15.500   1.5397   0.04634   0.03984  -0.0099   0.2581   1.0000
  15.750   1.5464   0.04750   0.04096  -0.0089   0.2529   1.0000
  16.000   1.5331   0.05063   0.04432  -0.0072   0.2482   1.0000
  16.250   1.5264   0.05325   0.04702  -0.0060   0.2423   1.0000
  16.500   1.5215   0.05581   0.04964  -0.0051   0.2362   1.0000
  16.750   1.5089   0.05940   0.05340  -0.0043   0.2304   1.0000
  17.000   1.5076   0.06180   0.05578  -0.0038   0.2246   1.0000
  17.250   1.4907   0.06620   0.06039  -0.0034   0.2184   1.0000
  17.500   1.4802   0.06991   0.06414  -0.0033   0.2114   1.0000
  17.750   1.4663   0.07423   0.06858  -0.0033   0.2058   1.0000
  18.000   1.4477   0.07924   0.07365  -0.0037   0.1979   1.0000
  18.250   1.4323   0.08400   0.07851  -0.0042   0.1921   1.0000
  18.500   1.4116   0.08957   0.08414  -0.0050   0.1844   1.0000
  18.750   1.3962   0.09449   0.08914  -0.0058   0.1788   1.0000
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