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GOE 567 AIRFOIL (goe567-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 567 AIRFOIL (goe567-il)
Reynolds number: 500,000
Max Cl/Cd: 95.83 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe567-il-500000-n5.txt
Download as CSV file: xf-goe567-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 567 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.5932   0.10333   0.10054  -0.0647   1.0000   0.0241
 -15.500  -0.7139   0.07966   0.07656  -0.0781   1.0000   0.0230
 -15.250  -0.7703   0.06824   0.06497  -0.0846   1.0000   0.0223
 -15.000  -0.8125   0.05990   0.05648  -0.0890   1.0000   0.0220
 -14.750  -0.8503   0.05294   0.04941  -0.0921   1.0000   0.0217
 -14.500  -0.8857   0.04690   0.04326  -0.0944   0.9998   0.0215
 -14.250  -0.8923   0.03988   0.03608  -0.1037   0.9939   0.0221
 -14.000  -0.8958   0.03384   0.02990  -0.1122   0.9847   0.0232
 -13.750  -0.8843   0.02888   0.02478  -0.1211   0.9752   0.0246
 -13.500  -0.8568   0.02540   0.02111  -0.1291   0.9703   0.0266
 -13.250  -0.8343   0.02372   0.01933  -0.1317   0.9624   0.0288
 -13.000  -0.8025   0.02239   0.01788  -0.1351   0.9584   0.0309
 -12.750  -0.7764   0.02135   0.01677  -0.1367   0.9509   0.0327
 -12.500  -0.7449   0.02046   0.01578  -0.1389   0.9447   0.0349
 -12.250  -0.7157   0.01965   0.01489  -0.1405   0.9361   0.0366
 -12.000  -0.6833   0.01899   0.01416  -0.1425   0.9275   0.0387
 -11.750  -0.6544   0.01839   0.01343  -0.1435   0.9154   0.0404
 -11.500  -0.6254   0.01780   0.01273  -0.1445   0.9016   0.0418
 -11.250  -0.5972   0.01732   0.01217  -0.1452   0.8857   0.0433
 -11.000  -0.5702   0.01695   0.01168  -0.1455   0.8686   0.0449
 -10.750  -0.5445   0.01660   0.01118  -0.1454   0.8510   0.0464
 -10.500  -0.5194   0.01628   0.01069  -0.1452   0.8346   0.0476
 -10.250  -0.4950   0.01591   0.01021  -0.1450   0.8195   0.0489
 -10.000  -0.4698   0.01565   0.00987  -0.1448   0.8065   0.0503
  -9.500  -0.4179   0.01529   0.00931  -0.1444   0.7849   0.0537
  -9.250  -0.3918   0.01512   0.00901  -0.1442   0.7762   0.0551
  -9.000  -0.3663   0.01475   0.00856  -0.1440   0.7677   0.0564
  -8.750  -0.3408   0.01442   0.00816  -0.1438   0.7601   0.0575
  -8.500  -0.3144   0.01415   0.00783  -0.1437   0.7531   0.0586
  -8.250  -0.2879   0.01391   0.00751  -0.1436   0.7463   0.0597
  -8.000  -0.2612   0.01367   0.00720  -0.1435   0.7405   0.0609
  -7.750  -0.2342   0.01344   0.00690  -0.1434   0.7343   0.0622
  -7.500  -0.2073   0.01325   0.00661  -0.1433   0.7285   0.0634
  -7.250  -0.1801   0.01305   0.00633  -0.1432   0.7234   0.0643
  -7.000  -0.1532   0.01273   0.00596  -0.1431   0.7180   0.0654
  -6.750  -0.1264   0.01244   0.00562  -0.1431   0.7126   0.0669
  -6.500  -0.0991   0.01224   0.00536  -0.1430   0.7076   0.0683
  -6.250  -0.0714   0.01204   0.00514  -0.1430   0.7027   0.0698
  -6.000  -0.0438   0.01188   0.00492  -0.1430   0.6976   0.0714
  -5.750  -0.0163   0.01173   0.00469  -0.1429   0.6926   0.0728
  -5.500   0.0116   0.01156   0.00448  -0.1429   0.6878   0.0740
  -5.250   0.0395   0.01142   0.00429  -0.1429   0.6828   0.0750
  -5.000   0.0670   0.01123   0.00404  -0.1428   0.6778   0.0767
  -4.750   0.0947   0.01102   0.00381  -0.1428   0.6729   0.0790
  -4.500   0.1226   0.01085   0.00362  -0.1428   0.6677   0.0810
  -4.250   0.1505   0.01072   0.00346  -0.1428   0.6625   0.0828
  -4.000   0.1783   0.01063   0.00330  -0.1427   0.6576   0.0846
  -3.750   0.2066   0.01051   0.00316  -0.1428   0.6522   0.0866
  -3.500   0.2345   0.01042   0.00303  -0.1427   0.6463   0.0885
  -3.000   0.2904   0.01018   0.00277  -0.1427   0.6358   0.0958
  -2.750   0.3182   0.01010   0.00266  -0.1426   0.6290   0.0998
  -2.500   0.3458   0.01000   0.00256  -0.1425   0.6214   0.1081
  -2.250   0.3733   0.00987   0.00246  -0.1424   0.6128   0.1254
  -2.000   0.4006   0.00972   0.00238  -0.1424   0.6048   0.1560
  -1.750   0.4281   0.00959   0.00232  -0.1423   0.5972   0.1870
  -1.500   0.4554   0.00951   0.00228  -0.1422   0.5902   0.2134
  -1.250   0.4831   0.00943   0.00226  -0.1422   0.5829   0.2390
  -1.000   0.5104   0.00939   0.00226  -0.1421   0.5765   0.2647
  -0.750   0.5381   0.00935   0.00227  -0.1420   0.5701   0.2900
  -0.500   0.5654   0.00934   0.00229  -0.1418   0.5628   0.3132
  -0.250   0.5927   0.00935   0.00233  -0.1417   0.5566   0.3356
   0.000   0.6202   0.00937   0.00237  -0.1416   0.5497   0.3528
   0.250   0.6472   0.00943   0.00242  -0.1413   0.5438   0.3660
   0.500   0.6746   0.00947   0.00247  -0.1412   0.5367   0.3803
   0.750   0.7012   0.00954   0.00254  -0.1409   0.5287   0.3956
   1.000   0.7282   0.00959   0.00262  -0.1407   0.5218   0.4114
   1.250   0.7553   0.00965   0.00270  -0.1404   0.5156   0.4241
   1.750   0.8091   0.00981   0.00286  -0.1400   0.5045   0.4450
   2.000   0.8357   0.00989   0.00296  -0.1397   0.4980   0.4576
   2.250   0.8619   0.00999   0.00307  -0.1393   0.4910   0.4704
   2.500   0.8879   0.01010   0.00318  -0.1389   0.4815   0.4818
   2.750   0.9135   0.01022   0.00329  -0.1384   0.4720   0.4917
   3.000   0.9389   0.01036   0.00341  -0.1380   0.4628   0.5016
   3.250   0.9649   0.01046   0.00354  -0.1376   0.4560   0.5114
   3.500   0.9903   0.01059   0.00367  -0.1371   0.4478   0.5214
   3.750   1.0154   0.01073   0.00382  -0.1366   0.4390   0.5317
   4.000   1.0393   0.01091   0.00398  -0.1358   0.4272   0.5417
   4.250   1.0629   0.01111   0.00415  -0.1350   0.4131   0.5527
   4.500   1.0857   0.01133   0.00435  -0.1341   0.3978   0.5637
   4.750   1.1078   0.01158   0.00457  -0.1331   0.3814   0.5752
   5.250   1.1500   0.01215   0.00507  -0.1307   0.3478   0.6020
   5.500   1.1693   0.01250   0.00537  -0.1292   0.3265   0.6176
   5.750   1.1863   0.01292   0.00573  -0.1274   0.3029   0.6367
   6.000   1.2003   0.01338   0.00614  -0.1250   0.2764   0.6609
   6.250   1.2117   0.01385   0.00661  -0.1222   0.2514   0.6998
   6.500   1.2220   0.01402   0.00712  -0.1190   0.2257   1.0000
   6.750   1.2307   0.01480   0.00774  -0.1159   0.1962   1.0000
   7.000   1.2250   0.01625   0.00883  -0.1108   0.1358   1.0000
   7.250   1.2363   0.01696   0.00947  -0.1084   0.1232   1.0000
   7.500   1.2518   0.01748   0.00999  -0.1066   0.1187   1.0000
   7.750   1.2668   0.01804   0.01055  -0.1048   0.1147   1.0000
   8.000   1.2806   0.01867   0.01118  -0.1029   0.1104   1.0000
   8.250   1.2957   0.01927   0.01179  -0.1013   0.1074   1.0000
   8.500   1.3113   0.01984   0.01240  -0.0998   0.1049   1.0000
   8.750   1.3263   0.02048   0.01307  -0.0982   0.1026   1.0000
   9.000   1.3392   0.02125   0.01386  -0.0965   0.0989   1.0000
   9.250   1.3503   0.02217   0.01478  -0.0947   0.0948   1.0000
   9.500   1.3647   0.02291   0.01557  -0.0933   0.0906   1.0000
  10.000   1.3762   0.02567   0.01817  -0.0892   0.0615   1.0000
  10.250   1.3827   0.02710   0.01959  -0.0875   0.0573   1.0000
  10.500   1.3921   0.02837   0.02090  -0.0861   0.0550   1.0000
  10.750   1.4018   0.02967   0.02225  -0.0848   0.0538   1.0000
  11.000   1.4108   0.03106   0.02369  -0.0835   0.0526   1.0000
  11.250   1.4188   0.03258   0.02526  -0.0823   0.0515   1.0000
  11.500   1.4263   0.03417   0.02691  -0.0811   0.0506   1.0000
  11.750   1.4321   0.03597   0.02875  -0.0799   0.0492   1.0000
  12.000   1.4378   0.03781   0.03065  -0.0789   0.0481   1.0000
  12.250   1.4448   0.03960   0.03250  -0.0779   0.0474   1.0000
  12.500   1.4537   0.04123   0.03421  -0.0772   0.0466   1.0000
  12.750   1.4615   0.04300   0.03605  -0.0764   0.0458   1.0000
  13.000   1.4684   0.04491   0.03803  -0.0757   0.0448   1.0000
  13.250   1.4745   0.04694   0.04012  -0.0751   0.0437   1.0000
  13.500   1.4797   0.04912   0.04236  -0.0745   0.0427   1.0000
  13.750   1.4834   0.05149   0.04480  -0.0739   0.0418   1.0000
  14.000   1.4855   0.05413   0.04749  -0.0735   0.0405   1.0000
  14.250   1.4929   0.05620   0.04964  -0.0732   0.0396   1.0000
  14.500   1.5005   0.05829   0.05181  -0.0729   0.0382   1.0000
  14.750   1.5066   0.06059   0.05417  -0.0727   0.0364   1.0000
  15.000   1.5103   0.06320   0.05680  -0.0726   0.0343   1.0000
  15.250   1.5167   0.06555   0.05923  -0.0726   0.0315   1.0000
  15.500   1.5198   0.06832   0.06200  -0.0726   0.0246   1.0000
  16.000   1.5120   0.07587   0.06951  -0.0731   0.0158   1.0000
  16.250   1.5097   0.07957   0.07327  -0.0735   0.0146   1.0000
  16.500   1.5096   0.08301   0.07679  -0.0739   0.0138   1.0000
  16.750   1.5096   0.08648   0.08034  -0.0744   0.0132   1.0000
  17.000   1.5089   0.09010   0.08405  -0.0751   0.0127   1.0000
  17.250   1.5078   0.09381   0.08783  -0.0758   0.0122   1.0000
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