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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 200,000
Max Cl/Cd: 62.25 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe383-il-200000.txt
Download as CSV file: xf-goe383-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.0378   0.10683   0.10291  -0.0769   0.8344   0.0946
 -11.250  -0.0290   0.10462   0.10064  -0.0765   0.8244   0.0962
 -11.000  -0.0722   0.09728   0.09327  -0.0826   0.8213   0.1017
 -10.750  -0.0488   0.09572   0.09168  -0.0809   0.8103   0.1023
 -10.500  -0.0325   0.09411   0.08999  -0.0797   0.8019   0.1035
 -10.250  -0.0224   0.09181   0.08767  -0.0798   0.7939   0.1058
 -10.000  -0.0617   0.08369   0.07956  -0.0859   0.7900   0.1114
  -9.750  -0.4182   0.04515   0.03937  -0.1048   0.8094   0.0708
  -9.500  -0.4034   0.04277   0.03688  -0.1041   0.8020   0.0701
  -9.250  -0.3951   0.03996   0.03386  -0.1031   0.7940   0.0688
  -9.000  -0.4151   0.03492   0.02754  -0.0985   0.7863   0.0649
  -8.750  -0.3961   0.03312   0.02548  -0.0977   0.7803   0.0648
  -8.500  -0.3764   0.03153   0.02369  -0.0969   0.7736   0.0647
  -8.250  -0.3557   0.03013   0.02207  -0.0961   0.7671   0.0647
  -8.000  -0.3339   0.02891   0.02059  -0.0953   0.7617   0.0648
  -7.750  -0.3100   0.02755   0.01907  -0.0948   0.7564   0.0652
  -7.500  -0.2854   0.02639   0.01790  -0.0946   0.7492   0.0658
  -7.250  -0.2602   0.02551   0.01697  -0.0942   0.7425   0.0667
  -7.000  -0.2345   0.02473   0.01606  -0.0938   0.7369   0.0676
  -6.750  -0.2092   0.02399   0.01525  -0.0934   0.7313   0.0685
  -6.500  -0.1834   0.02327   0.01444  -0.0930   0.7259   0.0692
  -6.250  -0.1570   0.02259   0.01365  -0.0927   0.7209   0.0700
  -6.000  -0.1303   0.02201   0.01293  -0.0923   0.7166   0.0708
  -5.750  -0.1038   0.02132   0.01225  -0.0921   0.7124   0.0719
  -5.500  -0.0786   0.02075   0.01178  -0.0917   0.7073   0.0732
  -5.250  -0.0531   0.02028   0.01132  -0.0913   0.7022   0.0747
  -5.000  -0.0271   0.01986   0.01084  -0.0909   0.6977   0.0768
  -4.750  -0.0016   0.01940   0.01037  -0.0904   0.6937   0.0792
  -4.500   0.0229   0.01908   0.01012  -0.0899   0.6894   0.0820
  -4.250   0.0476   0.01878   0.00982  -0.0893   0.6844   0.0851
  -4.000   0.0719   0.01839   0.00949  -0.0887   0.6794   0.0891
  -3.750   0.0976   0.01804   0.00913  -0.0882   0.6749   0.0948
  -3.500   0.1238   0.01779   0.00888  -0.0878   0.6707   0.1048
  -3.250   0.1465   0.01740   0.00871  -0.0870   0.6656   0.1299
  -3.000   0.1676   0.01672   0.00845  -0.0861   0.6605   0.2023
  -2.750   0.1916   0.01632   0.00834  -0.0855   0.6558   0.2802
  -2.500   0.2173   0.01604   0.00820  -0.0851   0.6515   0.3346
  -2.250   0.2412   0.01585   0.00821  -0.0845   0.6467   0.3899
  -2.000   0.2629   0.01556   0.00825  -0.0834   0.6408   0.4601
  -1.750   0.2855   0.01524   0.00826  -0.0823   0.6353   0.5423
  -1.500   0.3099   0.01505   0.00829  -0.0812   0.6306   0.6255
  -1.250   0.3345   0.01510   0.00847  -0.0801   0.6258   0.6851
  -1.000   0.3570   0.01512   0.00865  -0.0787   0.6196   0.7298
  -0.750   0.3814   0.01513   0.00872  -0.0775   0.6140   0.7705
  -0.500   0.4076   0.01516   0.00878  -0.0763   0.6092   0.8063
  -0.250   0.4323   0.01533   0.00895  -0.0751   0.6038   0.8363
   0.000   0.4550   0.01543   0.00911  -0.0736   0.5969   0.8612
   0.250   0.4820   0.01551   0.00914  -0.0728   0.5911   0.8834
   0.500   0.5134   0.01565   0.00916  -0.0727   0.5863   0.9033
   0.750   0.5433   0.01588   0.00941  -0.0728   0.5797   0.9206
   1.000   0.5794   0.01605   0.00954  -0.0741   0.5731   0.9361
   1.250   0.6220   0.01618   0.00954  -0.0765   0.5677   0.9497
   1.500   0.6678   0.01639   0.00966  -0.0801   0.5615   0.9583
   1.750   0.7096   0.01651   0.00975  -0.0831   0.5542   0.9663
   2.000   0.7573   0.01656   0.00969  -0.0871   0.5486   0.9734
   2.250   0.8051   0.01668   0.00968  -0.0912   0.5433   0.9813
   2.500   0.8516   0.01680   0.00984  -0.0953   0.5359   0.9900
   2.750   0.9020   0.01679   0.00973  -0.1001   0.5300   0.9968
   3.000   0.9381   0.01681   0.00961  -0.1021   0.5255   1.0000
   3.250   0.9489   0.01697   0.00983  -0.0997   0.5197   1.0000
   3.500   0.9630   0.01704   0.00989  -0.0976   0.5143   1.0000
   3.750   0.9805   0.01706   0.00982  -0.0960   0.5097   1.0000
   4.000   0.9984   0.01716   0.00983  -0.0944   0.5047   1.0000
   4.250   1.0097   0.01732   0.01002  -0.0917   0.4984   1.0000
   4.500   1.0273   0.01738   0.01003  -0.0899   0.4931   1.0000
   4.750   1.0503   0.01748   0.01000  -0.0891   0.4887   1.0000
   5.000   1.0644   0.01776   0.01031  -0.0869   0.4836   1.0000
   5.250   1.0810   0.01797   0.01053  -0.0850   0.4784   1.0000
   5.500   1.1019   0.01813   0.01063  -0.0839   0.4739   1.0000
   5.750   1.1292   0.01834   0.01069  -0.0839   0.4697   1.0000
   6.000   1.1419   0.01868   0.01113  -0.0814   0.4647   1.0000
   6.250   1.1607   0.01895   0.01141  -0.0800   0.4598   1.0000
   6.500   1.1838   0.01917   0.01156  -0.0794   0.4553   1.0000
   6.750   1.2113   0.01946   0.01175  -0.0795   0.4509   1.0000
   7.000   1.2244   0.01986   0.01225  -0.0773   0.4459   1.0000
   7.250   1.2438   0.02018   0.01258  -0.0761   0.4410   1.0000
   7.500   1.2684   0.02044   0.01279  -0.0757   0.4366   1.0000
   7.750   1.2940   0.02083   0.01312  -0.0757   0.4321   1.0000
   8.000   1.3054   0.02129   0.01368  -0.0733   0.4270   1.0000
   8.250   1.3241   0.02163   0.01403  -0.0720   0.4219   1.0000
   8.500   1.3513   0.02193   0.01423  -0.0722   0.4171   1.0000
   8.750   1.3675   0.02244   0.01480  -0.0707   0.4123   1.0000
   9.000   1.3761   0.02294   0.01538  -0.0679   0.4072   1.0000
   9.250   1.3944   0.02332   0.01574  -0.0667   0.4023   1.0000
   9.500   1.4307   0.02366   0.01595  -0.0685   0.3974   1.0000
   9.750   1.4260   0.02438   0.01684  -0.0637   0.3924   1.0000
  10.000   1.4351   0.02496   0.01748  -0.0614   0.3869   1.0000
  10.250   1.4580   0.02528   0.01771  -0.0610   0.3815   1.0000
  10.500   1.4655   0.02603   0.01853  -0.0586   0.3758   1.0000
  10.750   1.4682   0.02687   0.01946  -0.0557   0.3697   1.0000
  11.000   1.4864   0.02728   0.01982  -0.0548   0.3641   1.0000
  11.250   1.4951   0.02816   0.02074  -0.0529   0.3586   1.0000
  11.500   1.4956   0.02930   0.02199  -0.0503   0.3526   1.0000
  11.750   1.5104   0.02992   0.02258  -0.0492   0.3473   1.0000
  12.000   1.5202   0.03088   0.02357  -0.0478   0.3418   1.0000
  12.250   1.5175   0.03241   0.02522  -0.0454   0.3357   1.0000
  12.500   1.5299   0.03319   0.02597  -0.0443   0.3302   1.0000
  12.750   1.5340   0.03457   0.02740  -0.0427   0.3244   1.0000
  13.000   1.5309   0.03640   0.02933  -0.0409   0.3181   1.0000
  13.250   1.5456   0.03709   0.02992  -0.0401   0.3124   1.0000
  13.500   1.5377   0.03949   0.03247  -0.0383   0.3062   1.0000
  13.750   1.5380   0.04136   0.03439  -0.0371   0.3001   1.0000
  14.000   1.5537   0.04210   0.03504  -0.0366   0.2949   1.0000
  14.250   1.5450   0.04498   0.03809  -0.0353   0.2894   1.0000
  14.500   1.5483   0.04689   0.04005  -0.0346   0.2845   1.0000
  14.750   1.5676   0.04734   0.04038  -0.0342   0.2799   1.0000
  15.000   1.5564   0.05071   0.04396  -0.0333   0.2749   1.0000
  15.250   1.5568   0.05306   0.04637  -0.0327   0.2700   1.0000
  15.500   1.5726   0.05383   0.04707  -0.0324   0.2658   1.0000
  15.750   1.5690   0.05668   0.05005  -0.0319   0.2615   1.0000
  16.000   1.5650   0.05962   0.05310  -0.0315   0.2570   1.0000
  16.250   1.5723   0.06134   0.05482  -0.0312   0.2526   1.0000
  16.500   1.5801   0.06301   0.05649  -0.0309   0.2485   1.0000
  16.750   1.5687   0.06695   0.06060  -0.0307   0.2440   1.0000
  17.000   1.5685   0.06961   0.06332  -0.0306   0.2397   1.0000
  17.250   1.5854   0.07020   0.06382  -0.0304   0.2351   1.0000
  17.500   1.5670   0.07515   0.06899  -0.0306   0.2309   1.0000
  17.750   1.5603   0.07875   0.07269  -0.0308   0.2264   1.0000
  18.000   1.5764   0.07942   0.07326  -0.0306   0.2216   1.0000
  18.250   1.5551   0.08499   0.07905  -0.0312   0.2171   1.0000
  18.500   1.5439   0.08931   0.08347  -0.0318   0.2115   1.0000
  18.750   1.5478   0.09162   0.08575  -0.0321   0.2060   1.0000
  19.000   1.5243   0.09783   0.09217  -0.0333   0.2004   1.0000
  19.250   1.5301   0.09990   0.09416  -0.0337   0.1939   1.0000
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