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GOE 507 AIRFOIL (goe507-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 507 AIRFOIL (goe507-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.16 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe507-il-1000000-n5.txt
Download as CSV file: xf-goe507-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 507 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6451   0.11336   0.11138  -0.0221   1.0000   0.0073
 -13.750  -0.6711   0.10393   0.10192  -0.0269   1.0000   0.0074
 -13.250  -1.0344   0.03277   0.02991  -0.0734   1.0000   0.0056
 -13.000  -1.0337   0.02952   0.02645  -0.0724   1.0000   0.0058
 -12.750  -1.0271   0.02724   0.02399  -0.0710   1.0000   0.0059
 -12.500  -1.0163   0.02555   0.02215  -0.0696   1.0000   0.0060
 -12.250  -1.0047   0.02403   0.02048  -0.0681   1.0000   0.0061
 -12.000  -0.9853   0.02270   0.01901  -0.0678   0.9989   0.0064
 -11.750  -0.9596   0.02135   0.01749  -0.0687   0.9951   0.0066
 -11.500  -0.9341   0.02023   0.01622  -0.0693   0.9907   0.0067
 -11.250  -0.9068   0.01914   0.01500  -0.0701   0.9870   0.0069
 -11.000  -0.8799   0.01797   0.01369  -0.0709   0.9833   0.0073
 -10.750  -0.8514   0.01705   0.01267  -0.0718   0.9794   0.0076
 -10.500  -0.8215   0.01623   0.01174  -0.0729   0.9759   0.0080
 -10.250  -0.7927   0.01552   0.01093  -0.0736   0.9704   0.0084
  -9.750  -0.7343   0.01420   0.00940  -0.0750   0.9591   0.0094
  -9.500  -0.7063   0.01359   0.00870  -0.0754   0.9526   0.0101
  -9.250  -0.6794   0.01308   0.00811  -0.0754   0.9450   0.0108
  -9.000  -0.6531   0.01266   0.00760  -0.0753   0.9373   0.0113
  -8.500  -0.6024   0.01172   0.00651  -0.0745   0.9221   0.0135
  -8.000  -0.5515   0.01093   0.00559  -0.0737   0.9090   0.0167
  -7.750  -0.5260   0.01057   0.00518  -0.0733   0.9024   0.0190
  -7.500  -0.5003   0.01022   0.00479  -0.0729   0.8963   0.0225
  -7.250  -0.4742   0.00996   0.00456  -0.0726   0.8901   0.0275
  -7.000  -0.4472   0.00986   0.00449  -0.0724   0.8848   0.0328
  -6.750  -0.4196   0.00981   0.00446  -0.0722   0.8796   0.0364
  -6.500  -0.3923   0.00975   0.00435  -0.0720   0.8740   0.0383
  -6.250  -0.3651   0.00970   0.00426  -0.0718   0.8680   0.0395
  -6.000  -0.3377   0.00967   0.00419  -0.0716   0.8606   0.0401
  -5.750  -0.3104   0.00967   0.00413  -0.0714   0.8535   0.0405
  -5.500  -0.2843   0.00934   0.00375  -0.0710   0.8466   0.0417
  -5.250  -0.2580   0.00912   0.00347  -0.0706   0.8400   0.0433
  -5.000  -0.2308   0.00900   0.00333  -0.0704   0.8336   0.0447
  -4.750  -0.2036   0.00892   0.00323  -0.0702   0.8268   0.0460
  -4.500  -0.1765   0.00879   0.00306  -0.0700   0.8205   0.0469
  -4.250  -0.1498   0.00860   0.00282  -0.0696   0.8129   0.0473
  -4.000  -0.1230   0.00844   0.00259  -0.0693   0.8061   0.0477
  -3.750  -0.0960   0.00827   0.00239  -0.0691   0.7993   0.0482
  -3.500  -0.0690   0.00813   0.00220  -0.0688   0.7933   0.0488
  -3.250  -0.0417   0.00800   0.00205  -0.0686   0.7874   0.0497
  -3.000  -0.0145   0.00789   0.00190  -0.0683   0.7808   0.0505
  -2.750   0.0127   0.00779   0.00176  -0.0681   0.7747   0.0512
  -2.500   0.0401   0.00769   0.00164  -0.0679   0.7678   0.0518
  -2.250   0.0672   0.00762   0.00154  -0.0676   0.7610   0.0524
  -2.000   0.0947   0.00755   0.00146  -0.0675   0.7538   0.0528
  -1.500   0.1493   0.00743   0.00129  -0.0670   0.7382   0.0535
  -1.250   0.1763   0.00735   0.00117  -0.0667   0.7295   0.0548
  -1.000   0.2035   0.00728   0.00108  -0.0665   0.7193   0.0559
  -0.750   0.2303   0.00725   0.00101  -0.0662   0.7049   0.0570
  -0.500   0.2563   0.00727   0.00095  -0.0657   0.6817   0.0581
  -0.250   0.2812   0.00737   0.00091  -0.0650   0.6396   0.0591
   0.000   0.3054   0.00755   0.00090  -0.0641   0.5882   0.0603
   0.250   0.3304   0.00769   0.00091  -0.0635   0.5511   0.0617
   0.500   0.3563   0.00779   0.00093  -0.0631   0.5274   0.0633
   0.750   0.3824   0.00789   0.00096  -0.0627   0.5046   0.0655
   1.000   0.4080   0.00797   0.00099  -0.0622   0.4805   0.0765
   1.250   0.4333   0.00784   0.00104  -0.0618   0.4639   0.1600
   1.500   0.4594   0.00789   0.00110  -0.0614   0.4450   0.1827
   1.750   0.4852   0.00798   0.00117  -0.0610   0.4223   0.2019
   2.000   0.5109   0.00806   0.00125  -0.0606   0.4003   0.2238
   2.250   0.5363   0.00813   0.00133  -0.0601   0.3769   0.2588
   2.500   0.5586   0.00784   0.00146  -0.0593   0.3533   0.4572
   2.750   0.5682   0.00680   0.00164  -0.0554   0.3307   0.9029
   3.000   0.6281   0.00723   0.00190  -0.0628   0.2727   0.9825
   3.250   0.6643   0.00756   0.00208  -0.0648   0.2402   0.9937
   3.500   0.6985   0.00785   0.00224  -0.0664   0.2138   0.9991
   3.750   0.7249   0.00813   0.00241  -0.0662   0.1902   1.0000
   4.000   0.7459   0.00852   0.00263  -0.0649   0.1516   1.0000
   4.250   0.7630   0.00926   0.00302  -0.0630   0.0796   1.0000
   4.500   0.7858   0.00953   0.00323  -0.0620   0.0687   1.0000
   4.750   0.8092   0.00976   0.00343  -0.0611   0.0641   1.0000
   5.000   0.8326   0.00998   0.00364  -0.0602   0.0593   1.0000
   5.250   0.8565   0.01016   0.00382  -0.0594   0.0568   1.0000
   5.500   0.8801   0.01037   0.00403  -0.0586   0.0543   1.0000
   5.750   0.9036   0.01060   0.00425  -0.0577   0.0515   1.0000
   6.000   0.9268   0.01085   0.00449  -0.0568   0.0484   1.0000
   6.250   0.9506   0.01105   0.00471  -0.0561   0.0471   1.0000
   6.500   0.9747   0.01123   0.00492  -0.0554   0.0460   1.0000
   6.750   0.9984   0.01144   0.00514  -0.0546   0.0435   1.0000
   7.000   1.0214   0.01172   0.00539  -0.0537   0.0365   1.0000
   7.250   1.0437   0.01206   0.00567  -0.0528   0.0288   1.0000
   7.500   1.0656   0.01243   0.00599  -0.0518   0.0230   1.0000
   7.750   1.0871   0.01283   0.00636  -0.0507   0.0191   1.0000
   8.000   1.1091   0.01318   0.00673  -0.0497   0.0169   1.0000
   8.250   1.1301   0.01360   0.00715  -0.0486   0.0148   1.0000
   8.500   1.1519   0.01395   0.00752  -0.0476   0.0135   1.0000
   8.750   1.1727   0.01437   0.00794  -0.0465   0.0122   1.0000
   9.000   1.1932   0.01479   0.00839  -0.0453   0.0113   1.0000
   9.250   1.2138   0.01519   0.00883  -0.0441   0.0104   1.0000
   9.500   1.2337   0.01564   0.00930  -0.0429   0.0098   1.0000
   9.750   1.2522   0.01616   0.00984  -0.0415   0.0090   1.0000
  10.000   1.2715   0.01660   0.01033  -0.0401   0.0087   1.0000
  10.250   1.2898   0.01708   0.01085  -0.0387   0.0083   1.0000
  10.500   1.3073   0.01757   0.01140  -0.0371   0.0079   1.0000
  10.750   1.3223   0.01810   0.01197  -0.0351   0.0075   1.0000
  11.000   1.3354   0.01869   0.01259  -0.0328   0.0071   1.0000
  11.250   1.3488   0.01926   0.01321  -0.0306   0.0068   1.0000
  11.500   1.3618   0.01987   0.01388  -0.0284   0.0066   1.0000
  11.750   1.3750   0.02049   0.01456  -0.0264   0.0063   1.0000
  12.000   1.3873   0.02118   0.01531  -0.0243   0.0061   1.0000
  12.250   1.3992   0.02192   0.01611  -0.0223   0.0059   1.0000
  12.500   1.4102   0.02274   0.01700  -0.0203   0.0057   1.0000
  12.750   1.4203   0.02364   0.01796  -0.0184   0.0055   1.0000
  13.000   1.4280   0.02475   0.01914  -0.0163   0.0054   1.0000
  13.250   1.4357   0.02589   0.02036  -0.0143   0.0052   1.0000
  13.500   1.4447   0.02698   0.02153  -0.0127   0.0051   1.0000
  13.750   1.4519   0.02823   0.02287  -0.0110   0.0051   1.0000
  14.000   1.4590   0.02955   0.02428  -0.0094   0.0049   1.0000
  14.250   1.4646   0.03104   0.02585  -0.0080   0.0048   1.0000
  14.500   1.4705   0.03255   0.02745  -0.0067   0.0047   1.0000
  14.750   1.4739   0.03436   0.02935  -0.0054   0.0046   1.0000
  15.000   1.4782   0.03615   0.03123  -0.0044   0.0045   1.0000
  15.250   1.4821   0.03806   0.03322  -0.0036   0.0044   1.0000
  15.500   1.4820   0.04044   0.03571  -0.0029   0.0043   1.0000
  15.750   1.4836   0.04276   0.03812  -0.0024   0.0042   1.0000
  16.000   1.4814   0.04559   0.04106  -0.0021   0.0042   1.0000
  16.250   1.4763   0.04892   0.04450  -0.0022   0.0041   1.0000
  16.500   1.4743   0.05204   0.04773  -0.0026   0.0040   1.0000
  16.750   1.4639   0.05650   0.05232  -0.0036   0.0039   1.0000
  17.000   1.4543   0.06110   0.05704  -0.0050   0.0039   1.0000
  17.250   1.4424   0.06628   0.06235  -0.0068   0.0039   1.0000
  17.500   1.4314   0.07154   0.06774  -0.0089   0.0038   1.0000
  17.750   1.4177   0.07741   0.07374  -0.0114   0.0038   1.0000
  18.000   1.4021   0.08380   0.08027  -0.0143   0.0038   1.0000
  18.250   1.3861   0.09046   0.08706  -0.0175   0.0038   1.0000
  18.500   1.3622   0.09883   0.09558  -0.0217   0.0038   1.0000
  18.750   1.3421   0.10677   0.10366  -0.0258   0.0038   1.0000
  19.000   1.3231   0.11476   0.11178  -0.0300   0.0038   1.0000
  19.250   1.2968   0.12443   0.12159  -0.0354   0.0038   1.0000
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