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GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 13K AIRFOIL (goe13k-il)
Reynolds number: 200,000
Max Cl/Cd: 42.92 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe13k-il-200000-n5.txt
Download as CSV file: xf-goe13k-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 13K 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.1073   0.11154   0.10686  -0.1332   0.9196   0.0461
 -11.750  -0.1225   0.10955   0.10490  -0.1300   0.9130   0.0464
 -11.500  -0.1346   0.10410   0.09945  -0.1325   0.9103   0.0482
 -11.250  -0.1219   0.10228   0.09762  -0.1332   0.9089   0.0487
 -11.000  -0.1130   0.09947   0.09480  -0.1348   0.9076   0.0492
 -10.750  -0.1069   0.09588   0.09119  -0.1371   0.9065   0.0495
 -10.500  -0.0992   0.09244   0.08774  -0.1395   0.9055   0.0503
 -10.250  -0.1134   0.09064   0.08597  -0.1364   0.8992   0.0508
 -10.000  -0.1190   0.08768   0.08302  -0.1364   0.8954   0.0518
  -9.750  -0.1243   0.08324   0.07857  -0.1385   0.8930   0.0521
  -9.500  -0.1337   0.07763   0.07296  -0.1420   0.8911   0.0526
  -9.250  -0.1514   0.07023   0.06554  -0.1477   0.8892   0.0529
  -9.000  -0.2039   0.06765   0.06302  -0.1420   0.8772   0.0526
  -8.750  -0.2870   0.05461   0.04960  -0.1414   0.8723   0.0533
  -8.500  -0.3382   0.05366   0.04860  -0.1295   0.8598   0.0534
  -8.250  -0.3822   0.04462   0.03882  -0.1240   0.8564   0.0542
  -8.000  -0.4193   0.04363   0.03763  -0.1132   0.8456   0.0544
  -7.750  -0.4252   0.04048   0.03398  -0.1089   0.8427   0.0548
  -7.500  -0.4155   0.03841   0.03169  -0.1067   0.8412   0.0554
  -7.250  -0.3970   0.03723   0.03044  -0.1057   0.8402   0.0560
  -7.000  -0.4158   0.03724   0.03034  -0.0974   0.8318   0.0561
  -6.750  -0.4056   0.03635   0.02933  -0.0946   0.8288   0.0565
  -6.500  -0.3903   0.03520   0.02800  -0.0927   0.8269   0.0570
  -6.250  -0.3732   0.03396   0.02656  -0.0911   0.8255   0.0574
  -6.000  -0.3539   0.03281   0.02522  -0.0898   0.8244   0.0579
  -5.750  -0.3334   0.03173   0.02393  -0.0886   0.8235   0.0584
  -5.500  -0.3522   0.03230   0.02443  -0.0801   0.8148   0.0587
  -5.250  -0.3376   0.03156   0.02351  -0.0777   0.8125   0.0592
  -5.000  -0.3190   0.03084   0.02261  -0.0761   0.8109   0.0598
  -4.750  -0.2981   0.03017   0.02176  -0.0748   0.8097   0.0607
  -4.500  -0.2757   0.02948   0.02089  -0.0738   0.8087   0.0614
  -4.250  -0.2516   0.02880   0.02004  -0.0731   0.8079   0.0619
  -4.000  -0.2623   0.02934   0.02050  -0.0660   0.8003   0.0622
  -3.750  -0.2464   0.02907   0.02010  -0.0639   0.7978   0.0626
  -3.500  -0.2261   0.02870   0.01961  -0.0625   0.7961   0.0629
  -3.250  -0.2034   0.02836   0.01916  -0.0615   0.7948   0.0633
  -3.000  -0.1794   0.02782   0.01858  -0.0609   0.7938   0.0640
  -2.750  -0.1543   0.02739   0.01811  -0.0605   0.7929   0.0645
  -2.500  -0.1287   0.02704   0.01776  -0.0602   0.7922   0.0655
  -2.250  -0.1368   0.02777   0.01848  -0.0538   0.7856   0.0658
  -2.000  -0.1215   0.02780   0.01850  -0.0517   0.7827   0.0666
  -1.750  -0.1002   0.02773   0.01843  -0.0506   0.7809   0.0679
  -1.500  -0.0759   0.02753   0.01821  -0.0499   0.7795   0.0688
  -1.250  -0.0476   0.02717   0.01783  -0.0500   0.7782   0.0698
  -1.000  -0.0171   0.02675   0.01738  -0.0504   0.7771   0.0710
  -0.750   0.0122   0.02642   0.01704  -0.0506   0.7763   0.0720
  -0.500   0.0012   0.02743   0.01803  -0.0440   0.7686   0.0723
  -0.250   0.0238   0.02734   0.01793  -0.0430   0.7659   0.0732
   0.250   0.0787   0.02680   0.01747  -0.0429   0.7627   0.0770
   0.500   0.1082   0.02657   0.01725  -0.0432   0.7616   0.0793
   0.750   0.1382   0.02635   0.01704  -0.0436   0.7607   0.0828
   1.000   0.1689   0.02611   0.01684  -0.0442   0.7600   0.0865
   2.000   0.2459   0.02675   0.01777  -0.0389   0.7458   0.1300
   2.250   0.2790   0.02644   0.01761  -0.0400   0.7448   0.1670
   2.500   0.3131   0.02610   0.01750  -0.0415   0.7441   0.2196
   3.000   0.6071   0.02645   0.02020  -0.0960   0.7479   1.0000
   3.250   0.6364   0.02621   0.01993  -0.0961   0.7464   1.0000
   3.500   0.6673   0.02587   0.01957  -0.0965   0.7451   1.0000
   3.750   0.7003   0.02536   0.01905  -0.0972   0.7441   1.0000
   4.250   0.7214   0.02648   0.02018  -0.0914   0.7305   1.0000
   4.750   0.7534   0.02704   0.02077  -0.0874   0.7179   1.0000
   5.000   0.7814   0.02667   0.02041  -0.0872   0.7148   1.0000
   5.250   0.8135   0.02608   0.01984  -0.0876   0.7126   1.0000
   6.250   0.8652   0.02737   0.02122  -0.0773   0.6635   1.0000
   6.500   0.8768   0.02758   0.02139  -0.0743   0.6271   1.0000
   6.750   0.9699   0.02260   0.01542  -0.0821   0.5060   1.0000
   7.000   0.9745   0.02348   0.01602  -0.0782   0.4711   1.0000
   7.250   0.9846   0.02421   0.01661  -0.0755   0.4515   1.0000
   7.500   0.9961   0.02491   0.01721  -0.0730   0.4350   1.0000
   7.750   1.0082   0.02560   0.01783  -0.0707   0.4201   1.0000
   8.000   1.0220   0.02624   0.01843  -0.0687   0.4066   1.0000
   8.250   1.0356   0.02688   0.01904  -0.0667   0.3925   1.0000
   8.500   1.0486   0.02757   0.01970  -0.0646   0.3776   1.0000
   8.750   1.0614   0.02829   0.02040  -0.0626   0.3628   1.0000
   9.000   1.0732   0.02906   0.02114  -0.0604   0.3451   1.0000
   9.250   1.0841   0.02990   0.02194  -0.0582   0.3226   1.0000
   9.500   1.0918   0.03094   0.02287  -0.0556   0.2950   1.0000
   9.750   1.0968   0.03216   0.02392  -0.0527   0.2615   1.0000
  10.000   1.1007   0.03350   0.02506  -0.0498   0.2268   1.0000
  10.250   1.1056   0.03483   0.02621  -0.0471   0.1967   1.0000
  10.500   1.1136   0.03599   0.02725  -0.0449   0.1742   1.0000
  10.750   1.1227   0.03710   0.02828  -0.0429   0.1571   1.0000
  11.000   1.1329   0.03816   0.02930  -0.0410   0.1456   1.0000
  11.250   1.1422   0.03930   0.03039  -0.0390   0.1347   1.0000
  11.500   1.1538   0.04030   0.03140  -0.0374   0.1269   1.0000
  11.750   1.1631   0.04147   0.03255  -0.0356   0.1200   1.0000
  12.000   1.1749   0.04248   0.03361  -0.0340   0.1153   1.0000
  12.250   1.1847   0.04363   0.03477  -0.0324   0.1102   1.0000
  12.500   1.1939   0.04485   0.03600  -0.0306   0.1058   1.0000
  12.750   1.2053   0.04591   0.03713  -0.0292   0.1017   1.0000
  13.000   1.2145   0.04716   0.03839  -0.0276   0.0975   1.0000
  13.250   1.2223   0.04854   0.03977  -0.0259   0.0942   1.0000
  13.500   1.2334   0.04967   0.04100  -0.0246   0.0908   1.0000
  13.750   1.2436   0.05087   0.04227  -0.0232   0.0880   1.0000
  14.000   1.2511   0.05232   0.04373  -0.0217   0.0846   1.0000
  14.250   1.2583   0.05381   0.04525  -0.0202   0.0824   1.0000
  14.500   1.2682   0.05508   0.04663  -0.0190   0.0800   1.0000
  14.750   1.2771   0.05646   0.04809  -0.0177   0.0769   1.0000
  15.000   1.2839   0.05806   0.04973  -0.0164   0.0746   1.0000
  15.250   1.2888   0.05983   0.05152  -0.0150   0.0723   1.0000
  15.500   1.2970   0.06133   0.05315  -0.0139   0.0704   1.0000
  15.750   1.3046   0.06290   0.05483  -0.0128   0.0678   1.0000
  16.000   1.3098   0.06473   0.05671  -0.0117   0.0654   1.0000
  16.250   1.3124   0.06683   0.05883  -0.0105   0.0635   1.0000
  16.500   1.3193   0.06854   0.06069  -0.0096   0.0610   1.0000
  16.750   1.3239   0.07052   0.06278  -0.0087   0.0593   1.0000
  17.000   1.3270   0.07271   0.06504  -0.0079   0.0568   1.0000
  17.250   1.3278   0.07514   0.06752  -0.0070   0.0553   1.0000
  17.500   1.3319   0.07728   0.06980  -0.0064   0.0530   1.0000
  17.750   1.3348   0.07959   0.07223  -0.0058   0.0507   1.0000
  18.000   1.3348   0.08227   0.07500  -0.0053   0.0491   1.0000
  18.250   1.3337   0.08515   0.07793  -0.0050   0.0475   1.0000
  18.500   1.3353   0.08771   0.08065  -0.0047   0.0455   1.0000
  18.750   1.3346   0.09065   0.08370  -0.0046   0.0436   1.0000
  19.000   1.3324   0.09383   0.08697  -0.0047   0.0422   1.0000
  19.250   1.3289   0.09721   0.09042  -0.0049   0.0410   1.0000
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