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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 200,000
Max Cl/Cd: 60.43 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe383-il-200000-n5.txt
Download as CSV file: xf-goe383-il-200000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5021   0.05702   0.05180  -0.1065   0.9032   0.0391
 -12.750  -0.5369   0.05050   0.04491  -0.1105   0.8847   0.0390
 -12.500  -0.5548   0.04666   0.04078  -0.1113   0.8666   0.0391
 -12.250  -0.5657   0.04381   0.03768  -0.1110   0.8490   0.0391
 -12.000  -0.5717   0.04153   0.03515  -0.1098   0.8323   0.0392
 -11.750  -0.5741   0.03961   0.03299  -0.1081   0.8169   0.0394
 -11.500  -0.5746   0.03802   0.03116  -0.1059   0.8023   0.0395
 -11.250  -0.5703   0.03657   0.02949  -0.1040   0.7889   0.0397
 -11.000  -0.5619   0.03517   0.02785  -0.1024   0.7777   0.0399
 -10.750  -0.5506   0.03384   0.02631  -0.1010   0.7664   0.0401
 -10.500  -0.5374   0.03261   0.02484  -0.0997   0.7570   0.0404
 -10.250  -0.5220   0.03143   0.02347  -0.0986   0.7475   0.0407
 -10.000  -0.5055   0.03036   0.02218  -0.0975   0.7391   0.0410
  -9.750  -0.4877   0.02936   0.02096  -0.0965   0.7317   0.0415
  -9.500  -0.4688   0.02842   0.01980  -0.0956   0.7240   0.0419
  -9.250  -0.4486   0.02756   0.01873  -0.0947   0.7171   0.0423
  -9.000  -0.4259   0.02676   0.01788  -0.0942   0.7109   0.0426
  -8.750  -0.4029   0.02603   0.01711  -0.0938   0.7048   0.0430
  -8.500  -0.3797   0.02534   0.01635  -0.0933   0.6994   0.0434
  -8.250  -0.3563   0.02469   0.01561  -0.0927   0.6947   0.0437
  -8.000  -0.3325   0.02406   0.01491  -0.0922   0.6901   0.0442
  -7.750  -0.3084   0.02345   0.01424  -0.0918   0.6848   0.0446
  -7.500  -0.2843   0.02287   0.01358  -0.0913   0.6791   0.0452
  -7.250  -0.2602   0.02234   0.01294  -0.0907   0.6735   0.0457
  -7.000  -0.2358   0.02184   0.01234  -0.0902   0.6679   0.0462
  -6.750  -0.2112   0.02136   0.01180  -0.0897   0.6616   0.0468
  -6.500  -0.1873   0.02083   0.01128  -0.0891   0.6562   0.0473
  -6.250  -0.1630   0.02039   0.01082  -0.0886   0.6520   0.0481
  -5.750  -0.1133   0.01964   0.01000  -0.0878   0.6442   0.0501
  -5.500  -0.0881   0.01930   0.00963  -0.0873   0.6402   0.0512
  -5.250  -0.0634   0.01891   0.00924  -0.0868   0.6362   0.0522
  -5.000  -0.0387   0.01856   0.00887  -0.0864   0.6323   0.0532
  -4.750  -0.0135   0.01826   0.00852  -0.0859   0.6285   0.0544
  -4.500   0.0122   0.01800   0.00820  -0.0855   0.6249   0.0559
  -4.250   0.0375   0.01771   0.00792  -0.0851   0.6210   0.0574
  -4.000   0.0630   0.01743   0.00765  -0.0848   0.6171   0.0594
  -3.750   0.0890   0.01720   0.00740  -0.0844   0.6132   0.0623
  -3.500   0.1147   0.01693   0.00713  -0.0840   0.6093   0.0659
  -3.250   0.1407   0.01670   0.00688  -0.0837   0.6055   0.0715
  -3.000   0.1663   0.01643   0.00670  -0.0834   0.6016   0.0838
  -2.750   0.1914   0.01613   0.00659  -0.0830   0.5972   0.1170
  -2.500   0.2170   0.01589   0.00647  -0.0826   0.5928   0.1478
  -2.250   0.2426   0.01564   0.00635  -0.0823   0.5887   0.1783
  -2.000   0.2677   0.01535   0.00625  -0.0820   0.5848   0.2280
  -1.750   0.2937   0.01517   0.00618  -0.0817   0.5811   0.2771
  -1.250   0.3436   0.01476   0.00615  -0.0808   0.5713   0.3629
  -1.000   0.3676   0.01447   0.00611  -0.0801   0.5664   0.4268
  -0.750   0.3913   0.01420   0.00608  -0.0794   0.5620   0.5071
  -0.500   0.4138   0.01396   0.00621  -0.0782   0.5574   0.5950
  -0.250   0.4375   0.01386   0.00634  -0.0772   0.5520   0.6621
   0.000   0.4626   0.01384   0.00640  -0.0764   0.5468   0.7028
   0.250   0.4884   0.01383   0.00642  -0.0757   0.5422   0.7343
   0.500   0.5137   0.01385   0.00650  -0.0750   0.5368   0.7615
   0.750   0.5387   0.01388   0.00659  -0.0743   0.5304   0.7875
   1.000   0.5639   0.01391   0.00664  -0.0735   0.5246   0.8140
   1.250   0.5894   0.01398   0.00672  -0.0727   0.5191   0.8400
   1.500   0.6153   0.01407   0.00686  -0.0721   0.5127   0.8638
   1.750   0.6424   0.01418   0.00694  -0.0717   0.5068   0.8853
   2.000   0.6718   0.01430   0.00703  -0.0719   0.5012   0.9029
   2.250   0.7027   0.01446   0.00718  -0.0725   0.4942   0.9208
   2.500   0.7358   0.01462   0.00727  -0.0736   0.4878   0.9378
   2.750   0.7707   0.01481   0.00741  -0.0751   0.4819   0.9530
   3.000   0.8064   0.01501   0.00757  -0.0768   0.4755   0.9668
   3.250   0.8436   0.01522   0.00770  -0.0789   0.4695   0.9794
   3.500   0.8855   0.01545   0.00788  -0.0821   0.4635   0.9886
   3.750   0.9266   0.01569   0.00807  -0.0852   0.4573   0.9967
   4.000   0.9512   0.01588   0.00817  -0.0850   0.4517   1.0000
   4.250   0.9644   0.01606   0.00830  -0.0825   0.4461   1.0000
   4.500   0.9777   0.01625   0.00845  -0.0801   0.4398   1.0000
   4.750   0.9917   0.01648   0.00859  -0.0777   0.4340   1.0000
   5.000   1.0074   0.01672   0.00877  -0.0757   0.4290   1.0000
   5.250   1.0240   0.01696   0.00901  -0.0739   0.4243   1.0000
   5.500   1.0412   0.01723   0.00925  -0.0722   0.4198   1.0000
   5.750   1.0588   0.01752   0.00948  -0.0706   0.4157   1.0000
   6.000   1.0765   0.01782   0.00973  -0.0690   0.4118   1.0000
   6.250   1.0926   0.01813   0.01007  -0.0673   0.4076   1.0000
   6.500   1.1096   0.01846   0.01041  -0.0657   0.4033   1.0000
   6.750   1.1273   0.01883   0.01075  -0.0643   0.3993   1.0000
   7.000   1.1463   0.01921   0.01108  -0.0632   0.3955   1.0000
   7.250   1.1642   0.01962   0.01150  -0.0619   0.3916   1.0000
   7.500   1.1807   0.02006   0.01199  -0.0606   0.3873   1.0000
   7.750   1.1976   0.02052   0.01247  -0.0593   0.3829   1.0000
   8.000   1.2153   0.02100   0.01291  -0.0582   0.3789   1.0000
   8.250   1.2341   0.02148   0.01335  -0.0572   0.3753   1.0000
   8.500   1.2492   0.02205   0.01402  -0.0559   0.3711   1.0000
   8.750   1.2643   0.02265   0.01467  -0.0547   0.3666   1.0000
   9.000   1.2796   0.02327   0.01529  -0.0535   0.3621   1.0000
   9.250   1.2960   0.02388   0.01586  -0.0524   0.3580   1.0000
   9.500   1.3091   0.02465   0.01673  -0.0511   0.3534   1.0000
   9.750   1.3219   0.02546   0.01760  -0.0499   0.3485   1.0000
  10.000   1.3351   0.02627   0.01842  -0.0488   0.3439   1.0000
  10.250   1.3483   0.02711   0.01926  -0.0477   0.3394   1.0000
  10.500   1.3583   0.02819   0.02044  -0.0464   0.3337   1.0000
  10.750   1.3681   0.02929   0.02156  -0.0453   0.3280   1.0000
  11.000   1.3780   0.03041   0.02267  -0.0441   0.3228   1.0000
  11.250   1.3857   0.03178   0.02414  -0.0430   0.3165   1.0000
  11.500   1.3932   0.03315   0.02553  -0.0419   0.3104   1.0000
  11.750   1.4001   0.03463   0.02704  -0.0409   0.3044   1.0000
  12.000   1.4055   0.03630   0.02877  -0.0400   0.2977   1.0000
  12.250   1.4111   0.03794   0.03038  -0.0390   0.2919   1.0000
  12.500   1.4169   0.03972   0.03225  -0.0382   0.2857   1.0000
  12.750   1.4216   0.04159   0.03414  -0.0375   0.2799   1.0000
  13.000   1.4266   0.04345   0.03602  -0.0367   0.2745   1.0000
  13.250   1.4304   0.04552   0.03814  -0.0361   0.2684   1.0000
  13.500   1.4329   0.04766   0.04027  -0.0354   0.2625   1.0000
  13.750   1.4354   0.04994   0.04261  -0.0349   0.2562   1.0000
  14.000   1.4359   0.05240   0.04506  -0.0343   0.2498   1.0000
  14.250   1.4374   0.05480   0.04750  -0.0339   0.2439   1.0000
  14.500   1.4378   0.05739   0.05013  -0.0335   0.2378   1.0000
  14.750   1.4385   0.05990   0.05262  -0.0331   0.2324   1.0000
  15.000   1.4395   0.06255   0.05535  -0.0329   0.2272   1.0000
  15.250   1.4406   0.06514   0.05798  -0.0327   0.2224   1.0000
  15.500   1.4425   0.06762   0.06044  -0.0324   0.2184   1.0000
  15.750   1.4443   0.07028   0.06322  -0.0324   0.2143   1.0000
  16.000   1.4449   0.07306   0.06606  -0.0324   0.2103   1.0000
  16.250   1.4464   0.07569   0.06871  -0.0323   0.2064   1.0000
  16.500   1.4471   0.07849   0.07157  -0.0324   0.2028   1.0000
  16.750   1.4466   0.08152   0.07470  -0.0326   0.1988   1.0000
  17.000   1.4454   0.08463   0.07787  -0.0328   0.1947   1.0000
  17.250   1.4454   0.08753   0.08078  -0.0330   0.1907   1.0000
  17.500   1.4411   0.09120   0.08459  -0.0335   0.1863   1.0000
  17.750   1.4368   0.09481   0.08827  -0.0340   0.1815   1.0000
  18.000   1.4342   0.09817   0.09166  -0.0346   0.1771   1.0000
  18.250   1.4278   0.10223   0.09585  -0.0354   0.1720   1.0000
  18.500   1.4219   0.10615   0.09982  -0.0362   0.1667   1.0000
  18.750   1.4157   0.11019   0.10397  -0.0371   0.1614   1.0000
  19.000   1.4068   0.11462   0.10845  -0.0382   0.1547   1.0000
  19.250   1.3965   0.11935   0.11326  -0.0396   0.1465   1.0000
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