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GOE 526 AIRFOIL (goe526-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 526 AIRFOIL (goe526-il)
Reynolds number: 500,000
Max Cl/Cd: 98.44 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe526-il-500000.txt
Download as CSV file: xf-goe526-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 526 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3408   0.10868   0.10616  -0.0441   1.0000   0.0428
 -11.000  -0.3337   0.10682   0.10433  -0.0433   1.0000   0.0431
 -10.750  -0.6753   0.03474   0.03104  -0.0915   0.9825   0.0371
 -10.500  -0.6627   0.03122   0.02728  -0.0926   0.9755   0.0376
 -10.250  -0.6348   0.02959   0.02556  -0.0944   0.9720   0.0381
 -10.000  -0.6042   0.02814   0.02399  -0.0964   0.9698   0.0386
  -9.750  -0.5799   0.02649   0.02216  -0.0971   0.9643   0.0391
  -9.500  -0.5534   0.02477   0.02022  -0.0982   0.9591   0.0398
  -9.250  -0.5246   0.02306   0.01825  -0.0995   0.9552   0.0405
  -9.000  -0.5016   0.02183   0.01677  -0.0992   0.9465   0.0413
  -8.750  -0.4740   0.02069   0.01537  -0.0997   0.9402   0.0419
  -8.500  -0.4524   0.01940   0.01385  -0.0989   0.9306   0.0424
  -8.250  -0.4267   0.01812   0.01247  -0.0989   0.9231   0.0431
  -8.000  -0.4034   0.01750   0.01180  -0.0981   0.9128   0.0437
  -7.750  -0.3764   0.01689   0.01110  -0.0980   0.9049   0.0444
  -7.500  -0.3535   0.01634   0.01045  -0.0970   0.8945   0.0452
  -7.250  -0.3275   0.01581   0.00979  -0.0966   0.8867   0.0461
  -7.000  -0.3036   0.01537   0.00924  -0.0957   0.8772   0.0471
  -6.750  -0.2774   0.01501   0.00871  -0.0952   0.8696   0.0478
  -6.500  -0.2548   0.01411   0.00775  -0.0942   0.8608   0.0489
  -6.250  -0.2289   0.01367   0.00727  -0.0937   0.8539   0.0500
  -6.000  -0.2041   0.01334   0.00691  -0.0930   0.8463   0.0511
  -5.750  -0.1784   0.01302   0.00650  -0.0924   0.8388   0.0524
  -5.500  -0.1527   0.01275   0.00614  -0.0918   0.8312   0.0538
  -5.250  -0.1284   0.01227   0.00561  -0.0910   0.8231   0.0556
  -5.000  -0.1027   0.01199   0.00530  -0.0904   0.8160   0.0574
  -4.750  -0.0775   0.01174   0.00504  -0.0897   0.8083   0.0595
  -4.500  -0.0510   0.01156   0.00475  -0.0891   0.8014   0.0614
  -4.250  -0.0268   0.01116   0.00437  -0.0883   0.7942   0.0643
  -4.000  -0.0009   0.01097   0.00415  -0.0877   0.7870   0.0673
  -3.750   0.0254   0.01080   0.00392  -0.0872   0.7809   0.0708
  -3.500   0.0506   0.01055   0.00372  -0.0865   0.7746   0.0753
  -3.250   0.0772   0.01043   0.00355  -0.0860   0.7688   0.0796
  -3.000   0.1032   0.01023   0.00336  -0.0855   0.7635   0.0858
  -2.750   0.1290   0.01006   0.00322  -0.0849   0.7575   0.0924
  -2.500   0.1555   0.00995   0.00311  -0.0844   0.7517   0.1004
  -2.250   0.1822   0.00984   0.00302  -0.0840   0.7464   0.1102
  -2.000   0.2082   0.00972   0.00295  -0.0835   0.7406   0.1202
  -1.750   0.2349   0.00967   0.00289  -0.0830   0.7347   0.1303
  -1.500   0.2618   0.00961   0.00284  -0.0826   0.7290   0.1414
  -1.250   0.2876   0.00950   0.00278  -0.0821   0.7227   0.1514
  -1.000   0.3142   0.00946   0.00272  -0.0816   0.7164   0.1609
  -0.750   0.3405   0.00937   0.00266  -0.0811   0.7107   0.1719
  -0.500   0.3664   0.00929   0.00261  -0.0805   0.7040   0.1823
  -0.250   0.3925   0.00921   0.00254  -0.0800   0.6973   0.1948
   0.000   0.4179   0.00911   0.00250  -0.0793   0.6896   0.2106
   0.250   0.4429   0.00899   0.00245  -0.0786   0.6807   0.2345
   0.500   0.4668   0.00877   0.00243  -0.0777   0.6720   0.2930
   0.750   0.4836   0.00810   0.00244  -0.0756   0.6629   0.5204
   1.000   0.5296   0.00721   0.00275  -0.0788   0.6525   0.9416
   1.250   0.5759   0.00742   0.00288  -0.0822   0.6414   0.9671
   1.500   0.6301   0.00762   0.00298  -0.0875   0.6264   0.9790
   1.750   0.6845   0.00777   0.00304  -0.0930   0.6091   0.9878
   2.000   0.7397   0.00789   0.00305  -0.0988   0.5890   0.9961
   2.250   0.7803   0.00797   0.00303  -0.1015   0.5656   1.0000
   2.500   0.7997   0.00814   0.00307  -0.0997   0.5432   1.0000
   2.750   0.8190   0.00832   0.00314  -0.0979   0.5211   1.0000
   3.000   0.8380   0.00852   0.00323  -0.0961   0.4996   1.0000
   3.250   0.8568   0.00873   0.00334  -0.0943   0.4807   1.0000
   3.500   0.8758   0.00894   0.00346  -0.0925   0.4650   1.0000
   3.750   0.8949   0.00915   0.00359  -0.0907   0.4519   1.0000
   4.000   0.9134   0.00939   0.00375  -0.0888   0.4394   1.0000
   4.250   0.9333   0.00956   0.00389  -0.0872   0.4289   1.0000
   4.500   0.9523   0.00976   0.00404  -0.0854   0.4196   1.0000
   4.750   0.9711   0.00997   0.00421  -0.0835   0.4092   1.0000
   5.000   0.9903   0.01016   0.00437  -0.0818   0.4000   1.0000
   5.250   1.0087   0.01037   0.00454  -0.0799   0.3910   1.0000
   5.500   1.0280   0.01054   0.00471  -0.0781   0.3826   1.0000
   5.750   1.0462   0.01076   0.00489  -0.0762   0.3741   1.0000
   6.000   1.0653   0.01093   0.00506  -0.0744   0.3658   1.0000
   6.250   1.0827   0.01116   0.00525  -0.0724   0.3563   1.0000
   6.500   1.1015   0.01133   0.00544  -0.0706   0.3470   1.0000
   6.750   1.1179   0.01159   0.00565  -0.0683   0.3373   1.0000
   7.000   1.1363   0.01178   0.00584  -0.0665   0.3268   1.0000
   7.250   1.1530   0.01202   0.00606  -0.0643   0.3155   1.0000
   7.500   1.1682   0.01231   0.00631  -0.0619   0.3025   1.0000
   7.750   1.1810   0.01262   0.00657  -0.0590   0.2864   1.0000
   8.000   1.1916   0.01296   0.00684  -0.0558   0.2668   1.0000
   8.250   1.1995   0.01344   0.00719  -0.0521   0.2425   1.0000
   8.500   1.2073   0.01401   0.00764  -0.0486   0.2167   1.0000
   9.000   1.2253   0.01527   0.00869  -0.0425   0.1841   1.0000
   9.250   1.2374   0.01582   0.00922  -0.0400   0.1750   1.0000
   9.500   1.2478   0.01649   0.00985  -0.0374   0.1668   1.0000
   9.750   1.2624   0.01699   0.01037  -0.0356   0.1601   1.0000
  10.000   1.2733   0.01770   0.01105  -0.0332   0.1530   1.0000
  10.250   1.2884   0.01823   0.01162  -0.0315   0.1467   1.0000
  10.500   1.2999   0.01896   0.01233  -0.0295   0.1390   1.0000
  10.750   1.3146   0.01956   0.01296  -0.0279   0.1310   1.0000
  11.000   1.3259   0.02037   0.01374  -0.0260   0.1221   1.0000
  11.250   1.3376   0.02118   0.01452  -0.0243   0.1118   1.0000
  11.500   1.3483   0.02210   0.01542  -0.0225   0.1022   1.0000
  11.750   1.3575   0.02315   0.01644  -0.0207   0.0953   1.0000
  12.000   1.3647   0.02436   0.01763  -0.0189   0.0891   1.0000
  12.250   1.3735   0.02552   0.01882  -0.0173   0.0845   1.0000
  12.500   1.3801   0.02687   0.02017  -0.0157   0.0804   1.0000
  12.750   1.3846   0.02842   0.02175  -0.0140   0.0770   1.0000
  13.000   1.3944   0.02963   0.02302  -0.0128   0.0739   1.0000
  13.250   1.4005   0.03115   0.02458  -0.0115   0.0712   1.0000
  13.500   1.3996   0.03329   0.02672  -0.0099   0.0683   1.0000
  13.750   1.4100   0.03455   0.02807  -0.0091   0.0662   1.0000
  14.000   1.4167   0.03616   0.02975  -0.0081   0.0639   1.0000
  14.250   1.4204   0.03807   0.03169  -0.0071   0.0620   1.0000
  14.500   1.4178   0.04062   0.03427  -0.0061   0.0599   1.0000
  14.750   1.4264   0.04220   0.03595  -0.0055   0.0581   1.0000
  15.000   1.4316   0.04414   0.03795  -0.0049   0.0565   1.0000
  15.250   1.4346   0.04634   0.04021  -0.0044   0.0547   1.0000
  15.500   1.4333   0.04905   0.04296  -0.0039   0.0533   1.0000
  15.750   1.4307   0.05196   0.04593  -0.0036   0.0519   1.0000
  16.000   1.4358   0.05415   0.04822  -0.0034   0.0505   1.0000
  16.250   1.4382   0.05665   0.05081  -0.0034   0.0491   1.0000
  16.500   1.4391   0.05940   0.05362  -0.0034   0.0479   1.0000
  16.750   1.4362   0.06264   0.05691  -0.0036   0.0468   1.0000
  17.000   1.4286   0.06645   0.06076  -0.0039   0.0455   1.0000
  17.250   1.4306   0.06924   0.06367  -0.0042   0.0446   1.0000
  17.500   1.4313   0.07225   0.06678  -0.0047   0.0434   1.0000
  17.750   1.4292   0.07562   0.07023  -0.0053   0.0425   1.0000
  18.000   1.4267   0.07908   0.07376  -0.0060   0.0415   1.0000
  18.250   1.4211   0.08297   0.07769  -0.0068   0.0406   1.0000
  18.500   1.4131   0.08712   0.08187  -0.0077   0.0395   1.0000
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