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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 500,000
Max Cl/Cd: 88.39 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe383-il-500000.txt
Download as CSV file: xf-goe383-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 383 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.0985   0.11419   0.11105  -0.0663   0.7750   0.0499
 -12.500  -0.6887   0.03824   0.03333  -0.1047   0.8654   0.0398
 -12.250  -0.6886   0.03635   0.03119  -0.1025   0.8478   0.0397
 -12.000  -0.6823   0.03460   0.02921  -0.1007   0.8307   0.0398
 -11.750  -0.6723   0.03300   0.02739  -0.0992   0.8143   0.0399
 -11.500  -0.6590   0.03159   0.02577  -0.0980   0.7983   0.0400
 -11.250  -0.6435   0.03030   0.02431  -0.0969   0.7828   0.0401
 -11.000  -0.6256   0.02916   0.02304  -0.0960   0.7687   0.0403
 -10.750  -0.6066   0.02816   0.02187  -0.0952   0.7559   0.0405
 -10.500  -0.5865   0.02717   0.02078  -0.0944   0.7441   0.0407
 -10.250  -0.5659   0.02633   0.01979  -0.0937   0.7342   0.0409
 -10.000  -0.5443   0.02551   0.01887  -0.0931   0.7254   0.0413
  -9.750  -0.5227   0.02472   0.01793  -0.0924   0.7175   0.0417
  -9.500  -0.5004   0.02390   0.01698  -0.0918   0.7108   0.0420
  -9.250  -0.4773   0.02304   0.01600  -0.0913   0.7044   0.0422
  -9.000  -0.4538   0.02227   0.01509  -0.0908   0.6980   0.0425
  -8.750  -0.4299   0.02159   0.01426  -0.0902   0.6915   0.0428
  -8.500  -0.4051   0.02091   0.01350  -0.0898   0.6860   0.0430
  -8.250  -0.3801   0.02032   0.01280  -0.0894   0.6802   0.0433
  -8.000  -0.3550   0.01983   0.01219  -0.0890   0.6747   0.0436
  -7.750  -0.3295   0.01931   0.01156  -0.0886   0.6694   0.0439
  -7.500  -0.3038   0.01840   0.01069  -0.0884   0.6652   0.0443
  -7.250  -0.2780   0.01782   0.01012  -0.0882   0.6610   0.0448
  -7.000  -0.2521   0.01736   0.00965  -0.0879   0.6569   0.0453
  -6.750  -0.2262   0.01698   0.00922  -0.0875   0.6529   0.0458
  -6.500  -0.2002   0.01664   0.00883  -0.0872   0.6488   0.0464
  -6.250  -0.1737   0.01627   0.00845  -0.0870   0.6461   0.0471
  -6.000  -0.1471   0.01595   0.00811  -0.0868   0.6429   0.0478
  -5.750  -0.1201   0.01570   0.00781  -0.0865   0.6394   0.0485
  -5.500  -0.0953   0.01515   0.00727  -0.0861   0.6359   0.0493
  -5.250  -0.0696   0.01480   0.00692  -0.0857   0.6322   0.0501
  -5.000  -0.0433   0.01457   0.00665  -0.0854   0.6282   0.0510
  -4.750  -0.0165   0.01430   0.00638  -0.0852   0.6254   0.0520
  -4.500   0.0105   0.01405   0.00613  -0.0850   0.6225   0.0531
  -4.250   0.0367   0.01373   0.00581  -0.0847   0.6192   0.0543
  -4.000   0.0631   0.01343   0.00554  -0.0844   0.6158   0.0559
  -3.750   0.0903   0.01323   0.00531  -0.0842   0.6123   0.0577
  -3.500   0.1173   0.01305   0.00509  -0.0840   0.6085   0.0600
  -3.250   0.1444   0.01286   0.00491  -0.0839   0.6048   0.0633
  -3.000   0.1714   0.01260   0.00470  -0.0837   0.6015   0.0679
  -2.750   0.1982   0.01232   0.00450  -0.0834   0.5979   0.0789
  -2.500   0.2234   0.01187   0.00434  -0.0831   0.5942   0.1409
  -2.250   0.2497   0.01159   0.00421  -0.0829   0.5905   0.1820
  -2.000   0.2757   0.01133   0.00415  -0.0827   0.5864   0.2441
  -1.750   0.3024   0.01111   0.00412  -0.0825   0.5828   0.2960
  -1.500   0.3292   0.01089   0.00406  -0.0824   0.5788   0.3373
  -1.250   0.3557   0.01066   0.00400  -0.0822   0.5743   0.3841
  -1.000   0.3812   0.01038   0.00394  -0.0818   0.5698   0.4542
  -0.750   0.4065   0.01017   0.00393  -0.0813   0.5649   0.5330
  -0.500   0.4314   0.00991   0.00398  -0.0807   0.5607   0.6088
  -0.250   0.4575   0.00978   0.00402  -0.0802   0.5557   0.6649
   0.000   0.4841   0.00972   0.00403  -0.0798   0.5505   0.7019
   0.250   0.5106   0.00972   0.00406  -0.0794   0.5451   0.7338
   0.500   0.5368   0.00966   0.00411  -0.0789   0.5395   0.7673
   0.750   0.5629   0.00962   0.00415  -0.0783   0.5330   0.7951
   1.000   0.5889   0.00965   0.00416  -0.0778   0.5266   0.8163
   1.250   0.6152   0.00965   0.00424  -0.0773   0.5201   0.8374
   1.500   0.6409   0.00968   0.00429  -0.0767   0.5128   0.8582
   1.750   0.6659   0.00977   0.00435  -0.0760   0.5060   0.8781
   2.000   0.6913   0.00981   0.00446  -0.0753   0.4984   0.8998
   2.250   0.7158   0.00994   0.00455  -0.0744   0.4910   0.9227
   2.500   0.7431   0.01008   0.00468  -0.0741   0.4842   0.9415
   2.750   0.7742   0.01024   0.00481  -0.0748   0.4769   0.9554
   3.000   0.8070   0.01048   0.00495  -0.0759   0.4694   0.9676
   3.250   0.8425   0.01066   0.00511  -0.0776   0.4614   0.9783
   3.500   0.8843   0.01094   0.00528  -0.0807   0.4530   0.9830
   3.750   0.9257   0.01115   0.00546  -0.0837   0.4467   0.9884
   4.000   0.9659   0.01137   0.00564  -0.0866   0.4407   0.9933
   4.250   1.0085   0.01166   0.00583  -0.0900   0.4350   0.9975
   4.500   1.0414   0.01184   0.00600  -0.0914   0.4305   1.0000
   4.750   1.0546   0.01194   0.00609  -0.0889   0.4265   1.0000
   5.000   1.0680   0.01209   0.00621  -0.0863   0.4224   1.0000
   5.250   1.0818   0.01229   0.00636  -0.0838   0.4183   1.0000
   5.500   1.0977   0.01251   0.00654  -0.0817   0.4145   1.0000
   5.750   1.1151   0.01265   0.00670  -0.0799   0.4113   1.0000
   6.000   1.1332   0.01282   0.00688  -0.0782   0.4077   1.0000
   6.250   1.1500   0.01304   0.00708  -0.0764   0.4038   1.0000
   6.500   1.1668   0.01332   0.00731  -0.0746   0.3999   1.0000
   6.750   1.1861   0.01361   0.00757  -0.0733   0.3961   1.0000
   7.000   1.2055   0.01382   0.00782  -0.0720   0.3929   1.0000
   7.250   1.2254   0.01407   0.00810  -0.0709   0.3894   1.0000
   7.500   1.2449   0.01437   0.00839  -0.0698   0.3857   1.0000
   7.750   1.2642   0.01474   0.00872  -0.0687   0.3818   1.0000
   8.000   1.2842   0.01510   0.00908  -0.0678   0.3780   1.0000
   8.250   1.3035   0.01540   0.00944  -0.0668   0.3741   1.0000
   8.500   1.3221   0.01576   0.00982  -0.0657   0.3696   1.0000
   8.750   1.3394   0.01622   0.01024  -0.0645   0.3649   1.0000
   9.000   1.3571   0.01670   0.01072  -0.0634   0.3603   1.0000
   9.250   1.3756   0.01711   0.01120  -0.0625   0.3559   1.0000
   9.500   1.3929   0.01761   0.01171  -0.0615   0.3511   1.0000
   9.750   1.4083   0.01823   0.01231  -0.0603   0.3464   1.0000
  10.000   1.4252   0.01881   0.01293  -0.0594   0.3419   1.0000
  10.250   1.4421   0.01940   0.01356  -0.0585   0.3366   1.0000
  10.500   1.4553   0.02020   0.01435  -0.0573   0.3308   1.0000
  10.750   1.4692   0.02101   0.01519  -0.0562   0.3248   1.0000
  11.000   1.4823   0.02190   0.01610  -0.0552   0.3174   1.0000
  11.250   1.4915   0.02307   0.01724  -0.0539   0.3102   1.0000
  11.500   1.5036   0.02411   0.01833  -0.0529   0.3020   1.0000
  11.750   1.5106   0.02553   0.01972  -0.0516   0.2942   1.0000
  12.000   1.5203   0.02682   0.02104  -0.0507   0.2860   1.0000
  12.250   1.5253   0.02848   0.02268  -0.0494   0.2787   1.0000
  12.500   1.5339   0.02993   0.02415  -0.0485   0.2714   1.0000
  12.750   1.5365   0.03189   0.02608  -0.0473   0.2647   1.0000
  13.000   1.5453   0.03342   0.02766  -0.0466   0.2585   1.0000
  13.250   1.5484   0.03542   0.02966  -0.0456   0.2525   1.0000
  13.500   1.5541   0.03723   0.03149  -0.0448   0.2472   1.0000
  13.750   1.5593   0.03914   0.03343  -0.0441   0.2418   1.0000
  14.000   1.5603   0.04143   0.03571  -0.0432   0.2366   1.0000
  14.250   1.5667   0.04329   0.03761  -0.0426   0.2319   1.0000
  14.500   1.5702   0.04542   0.03977  -0.0420   0.2269   1.0000
  14.750   1.5707   0.04783   0.04217  -0.0413   0.2223   1.0000
  15.000   1.5761   0.04985   0.04425  -0.0408   0.2184   1.0000
  15.250   1.5810   0.05193   0.04638  -0.0404   0.2143   1.0000
  15.500   1.5814   0.05445   0.04891  -0.0399   0.2101   1.0000
  15.750   1.5832   0.05684   0.05133  -0.0395   0.2063   1.0000
  16.000   1.5882   0.05899   0.05355  -0.0392   0.2023   1.0000
  16.250   1.5887   0.06161   0.05621  -0.0389   0.1982   1.0000
  16.500   1.5865   0.06450   0.05910  -0.0385   0.1942   1.0000
  16.750   1.5909   0.06679   0.06148  -0.0384   0.1904   1.0000
  17.000   1.5916   0.06947   0.06420  -0.0383   0.1859   1.0000
  17.250   1.5849   0.07300   0.06774  -0.0381   0.1811   1.0000
  17.500   1.5875   0.07558   0.07040  -0.0382   0.1760   1.0000
  17.750   1.5804   0.07927   0.07412  -0.0382   0.1704   1.0000
  18.000   1.5763   0.08265   0.07755  -0.0383   0.1640   1.0000
  18.250   1.5652   0.08692   0.08183  -0.0386   0.1567   1.0000
  18.500   1.5534   0.09137   0.08630  -0.0389   0.1468   1.0000
  18.750   1.5343   0.09676   0.09168  -0.0395   0.1333   1.0000
  19.000   1.5023   0.10390   0.09874  -0.0404   0.1124   1.0000
  19.250   1.4611   0.11244   0.10718  -0.0418   0.0915   1.0000
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