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GOE 567 AIRFOIL (goe567-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 567 AIRFOIL (goe567-il)
Reynolds number: 500,000
Max Cl/Cd: 115.17 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe567-il-500000.txt
Download as CSV file: xf-goe567-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7041   0.08328   0.08032  -0.0770   1.0000   0.0296
 -15.500  -0.7434   0.07385   0.07075  -0.0825   1.0000   0.0299
 -15.250  -0.7733   0.06647   0.06324  -0.0867   1.0000   0.0301
 -15.000  -0.7998   0.06018   0.05684  -0.0900   1.0000   0.0303
 -14.750  -0.8246   0.05475   0.05133  -0.0925   1.0000   0.0305
 -14.500  -0.8490   0.04981   0.04628  -0.0943   1.0000   0.0308
 -14.250  -0.8735   0.04557   0.04195  -0.0950   1.0000   0.0310
 -14.000  -0.9022   0.04188   0.03821  -0.0943   1.0000   0.0310
 -13.750  -0.9406   0.03883   0.03514  -0.0914   1.0000   0.0309
 -13.500  -0.9265   0.03308   0.02930  -0.1028   0.9939   0.0322
 -13.250  -0.8954   0.02937   0.02547  -0.1120   0.9886   0.0339
 -13.000  -0.8602   0.02692   0.02276  -0.1189   0.9846   0.0359
 -12.750  -0.8248   0.02521   0.02105  -0.1240   0.9821   0.0379
 -12.500  -0.7954   0.02431   0.02007  -0.1262   0.9763   0.0398
 -12.250  -0.7609   0.02323   0.01880  -0.1294   0.9727   0.0418
 -12.000  -0.7237   0.02252   0.01813  -0.1326   0.9703   0.0438
 -11.750  -0.6881   0.02208   0.01763  -0.1350   0.9669   0.0458
 -11.500  -0.6563   0.02147   0.01685  -0.1367   0.9611   0.0475
 -11.250  -0.6207   0.02050   0.01584  -0.1395   0.9575   0.0494
 -11.000  -0.5817   0.02023   0.01557  -0.1422   0.9545   0.0510
 -10.750  -0.5532   0.01992   0.01520  -0.1428   0.9445   0.0527
 -10.500  -0.5170   0.01945   0.01456  -0.1450   0.9383   0.0545
 -10.250  -0.4896   0.01858   0.01358  -0.1457   0.9259   0.0562
 -10.000  -0.4602   0.01820   0.01318  -0.1464   0.9132   0.0577
  -9.750  -0.4306   0.01797   0.01289  -0.1470   0.8995   0.0592
  -9.500  -0.4024   0.01770   0.01249  -0.1473   0.8849   0.0609
  -9.250  -0.3752   0.01749   0.01211  -0.1474   0.8702   0.0626
  -9.000  -0.3495   0.01707   0.01151  -0.1473   0.8563   0.0641
  -8.750  -0.3255   0.01635   0.01074  -0.1470   0.8431   0.0659
  -8.500  -0.2996   0.01611   0.01043  -0.1468   0.8316   0.0675
  -8.250  -0.2736   0.01584   0.01005  -0.1466   0.8215   0.0691
  -8.000  -0.2478   0.01550   0.00961  -0.1464   0.8117   0.0706
  -7.750  -0.2213   0.01526   0.00924  -0.1462   0.8034   0.0721
  -7.500  -0.1945   0.01512   0.00898  -0.1460   0.7950   0.0731
  -7.250  -0.1703   0.01416   0.00792  -0.1457   0.7879   0.0752
  -7.000  -0.1444   0.01371   0.00746  -0.1456   0.7806   0.0768
  -6.750  -0.1176   0.01344   0.00712  -0.1454   0.7740   0.0786
  -6.500  -0.0907   0.01319   0.00682  -0.1453   0.7676   0.0805
  -6.250  -0.0637   0.01295   0.00650  -0.1451   0.7610   0.0823
  -6.000  -0.0362   0.01277   0.00620  -0.1451   0.7553   0.0837
  -5.750  -0.0091   0.01249   0.00588  -0.1449   0.7494   0.0849
  -5.500   0.0168   0.01192   0.00529  -0.1448   0.7434   0.0879
  -5.250   0.0443   0.01170   0.00500  -0.1447   0.7379   0.0902
  -5.000   0.0716   0.01147   0.00476  -0.1446   0.7324   0.0924
  -4.750   0.0992   0.01128   0.00452  -0.1445   0.7267   0.0946
  -4.500   0.1272   0.01118   0.00432  -0.1445   0.7213   0.0965
  -4.250   0.1544   0.01088   0.00401  -0.1444   0.7158   0.0997
  -4.000   0.1820   0.01064   0.00378  -0.1444   0.7102   0.1032
  -3.750   0.2101   0.01052   0.00359  -0.1444   0.7049   0.1067
  -3.500   0.2380   0.01040   0.00344  -0.1443   0.6994   0.1103
  -3.250   0.2656   0.01018   0.00325  -0.1442   0.6935   0.1175
  -3.000   0.2937   0.01005   0.00309  -0.1442   0.6882   0.1271
  -2.750   0.3214   0.00980   0.00296  -0.1443   0.6828   0.1552
  -2.500   0.3488   0.00947   0.00284  -0.1443   0.6768   0.2130
  -2.250   0.3765   0.00932   0.00277  -0.1443   0.6712   0.2572
  -2.000   0.4043   0.00922   0.00276  -0.1443   0.6653   0.2902
  -1.750   0.4320   0.00914   0.00274  -0.1442   0.6588   0.3159
  -1.500   0.4599   0.00915   0.00272  -0.1440   0.6525   0.3372
  -1.250   0.4874   0.00910   0.00272  -0.1439   0.6451   0.3557
  -1.000   0.5149   0.00911   0.00270  -0.1437   0.6381   0.3728
  -0.750   0.5426   0.00911   0.00273  -0.1435   0.6316   0.3888
  -0.500   0.5703   0.00912   0.00276  -0.1434   0.6250   0.4041
  -0.250   0.5978   0.00917   0.00278  -0.1432   0.6190   0.4174
   0.000   0.6253   0.00917   0.00281  -0.1430   0.6115   0.4305
   0.250   0.6525   0.00923   0.00283  -0.1428   0.6043   0.4432
   0.500   0.6799   0.00925   0.00288  -0.1426   0.5973   0.4549
   0.750   0.7072   0.00930   0.00293  -0.1424   0.5907   0.4666
   1.000   0.7344   0.00939   0.00298  -0.1421   0.5845   0.4790
   1.250   0.7616   0.00941   0.00306  -0.1419   0.5776   0.4905
   1.500   0.7885   0.00950   0.00312  -0.1416   0.5714   0.5020
   2.000   0.8426   0.00963   0.00330  -0.1412   0.5589   0.5256
   2.250   0.8692   0.00974   0.00338  -0.1408   0.5528   0.5360
   2.500   0.8962   0.00979   0.00347  -0.1406   0.5462   0.5475
   2.750   0.9221   0.00988   0.00356  -0.1402   0.5388   0.5585
   3.000   0.9482   0.00994   0.00365  -0.1398   0.5304   0.5702
   3.500   1.0001   0.01013   0.00388  -0.1389   0.5166   0.5957
   3.750   1.0257   0.01020   0.00399  -0.1385   0.5089   0.6097
   4.000   1.0508   0.01030   0.00411  -0.1379   0.5012   0.6255
   4.250   1.0761   0.01036   0.00424  -0.1374   0.4934   0.6441
   4.500   1.1006   0.01046   0.00439  -0.1368   0.4862   0.6680
   4.750   1.1254   0.01045   0.00454  -0.1362   0.4789   0.7066
   5.000   1.1477   0.01011   0.00468  -0.1349   0.4717   1.0000
   5.250   1.1733   0.01025   0.00482  -0.1344   0.4643   1.0000
   5.500   1.1971   0.01046   0.00498  -0.1337   0.4560   1.0000
   5.750   1.2218   0.01063   0.00515  -0.1331   0.4474   1.0000
   6.000   1.2450   0.01085   0.00533  -0.1323   0.4395   1.0000
   6.250   1.2692   0.01102   0.00552  -0.1316   0.4314   1.0000
   6.500   1.2911   0.01128   0.00574  -0.1305   0.4225   1.0000
   6.750   1.3138   0.01148   0.00595  -0.1296   0.4117   1.0000
   7.000   1.3350   0.01175   0.00619  -0.1284   0.4012   1.0000
   7.250   1.3544   0.01205   0.00646  -0.1269   0.3890   1.0000
   7.500   1.3724   0.01236   0.00673  -0.1252   0.3755   1.0000
   7.750   1.3884   0.01271   0.00704  -0.1230   0.3605   1.0000
   8.000   1.4027   0.01313   0.00741  -0.1207   0.3442   1.0000
   8.250   1.4146   0.01366   0.00786  -0.1180   0.3234   1.0000
   8.500   1.4217   0.01440   0.00846  -0.1146   0.2960   1.0000
   8.750   1.4256   0.01533   0.00922  -0.1109   0.2652   1.0000
   9.000   1.4264   0.01646   0.01016  -0.1069   0.2327   1.0000
   9.250   1.4252   0.01777   0.01129  -0.1029   0.1994   1.0000
   9.500   1.4182   0.01949   0.01277  -0.0985   0.1580   1.0000
   9.750   1.4169   0.02104   0.01418  -0.0952   0.1354   1.0000
  10.000   1.4228   0.02226   0.01537  -0.0928   0.1263   1.0000
  10.250   1.4282   0.02359   0.01668  -0.0906   0.1188   1.0000
  10.500   1.4384   0.02466   0.01780  -0.0889   0.1143   1.0000
  10.750   1.4454   0.02601   0.01916  -0.0871   0.1095   1.0000
  11.000   1.4522   0.02743   0.02062  -0.0854   0.1044   1.0000
  11.250   1.4630   0.02861   0.02184  -0.0841   0.0993   1.0000
  11.500   1.4686   0.03023   0.02347  -0.0826   0.0934   1.0000
  11.750   1.4786   0.03155   0.02483  -0.0814   0.0865   1.0000
  12.000   1.4829   0.03337   0.02662  -0.0800   0.0748   1.0000
  12.250   1.4859   0.03537   0.02857  -0.0787   0.0684   1.0000
  12.500   1.4884   0.03748   0.03068  -0.0774   0.0646   1.0000
  12.750   1.4916   0.03960   0.03282  -0.0763   0.0619   1.0000
  13.000   1.4956   0.04170   0.03499  -0.0753   0.0602   1.0000
  13.250   1.4985   0.04395   0.03731  -0.0744   0.0587   1.0000
  13.500   1.5000   0.04642   0.03985  -0.0736   0.0571   1.0000
  13.750   1.5003   0.04911   0.04260  -0.0729   0.0558   1.0000
  14.000   1.4992   0.05202   0.04556  -0.0723   0.0543   1.0000
  14.500   1.5032   0.05738   0.05108  -0.0715   0.0517   1.0000
  14.750   1.5071   0.05993   0.05372  -0.0713   0.0504   1.0000
  15.000   1.5093   0.06274   0.05661  -0.0711   0.0491   1.0000
  15.250   1.5092   0.06587   0.05981  -0.0711   0.0477   1.0000
  15.500   1.5057   0.06952   0.06351  -0.0712   0.0460   1.0000
  15.750   1.5059   0.07275   0.06683  -0.0714   0.0445   1.0000
  16.000   1.5148   0.07489   0.06907  -0.0715   0.0427   1.0000
  16.250   1.5200   0.07752   0.07176  -0.0717   0.0403   1.0000
  16.500   1.5180   0.08120   0.07547  -0.0722   0.0379   1.0000
  16.750   1.5304   0.08289   0.07722  -0.0724   0.0336   1.0000
  17.000   1.5342   0.08580   0.08016  -0.0728   0.0295   1.0000
  17.250   1.5358   0.08906   0.08342  -0.0734   0.0254   1.0000
  17.500   1.5341   0.09283   0.08720  -0.0741   0.0228   1.0000
  17.750   1.5317   0.09677   0.09119  -0.0750   0.0212   1.0000
  18.000   1.5282   0.10091   0.09537  -0.0760   0.0200   1.0000
  18.250   1.5237   0.10529   0.09982  -0.0772   0.0192   1.0000
  18.500   1.5210   0.10942   0.10405  -0.0784   0.0185   1.0000
  18.750   1.5181   0.11358   0.10830  -0.0797   0.0180   1.0000
  19.000   1.5138   0.11803   0.11283  -0.0812   0.0175   1.0000
  19.250   1.5090   0.12261   0.11749  -0.0828   0.0170   1.0000
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