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GOE 584 AIRFOIL (goe584-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 584 AIRFOIL (goe584-il)
Reynolds number: 500,000
Max Cl/Cd: 106 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe584-il-500000-n5.txt
Download as CSV file: xf-goe584-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 584 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.3912   0.14800   0.14543  -0.0316   1.0000   0.0133
 -15.000  -0.3846   0.14526   0.14269  -0.0327   1.0000   0.0135
 -13.500  -0.9028   0.03169   0.02829  -0.0995   0.9864   0.0184
 -13.250  -0.8865   0.02859   0.02491  -0.1020   0.9761   0.0190
 -13.000  -0.8634   0.02630   0.02243  -0.1043   0.9668   0.0199
 -12.750  -0.8366   0.02451   0.02048  -0.1064   0.9568   0.0210
 -12.500  -0.8074   0.02299   0.01875  -0.1084   0.9457   0.0223
 -12.250  -0.7771   0.02183   0.01747  -0.1102   0.9326   0.0236
 -12.000  -0.7484   0.02097   0.01648  -0.1112   0.9174   0.0252
 -11.750  -0.7237   0.02013   0.01545  -0.1113   0.9007   0.0267
 -11.500  -0.6984   0.01976   0.01501  -0.1111   0.8857   0.0280
 -11.250  -0.6740   0.01943   0.01458  -0.1107   0.8721   0.0294
 -11.000  -0.6514   0.01891   0.01389  -0.1099   0.8592   0.0310
 -10.750  -0.6280   0.01852   0.01338  -0.1093   0.8483   0.0323
 -10.500  -0.6021   0.01853   0.01333  -0.1089   0.8387   0.0333
 -10.250  -0.5767   0.01844   0.01318  -0.1084   0.8292   0.0345
 -10.000  -0.5525   0.01814   0.01274  -0.1078   0.8209   0.0358
  -9.750  -0.5285   0.01771   0.01215  -0.1072   0.8127   0.0370
  -9.500  -0.5044   0.01736   0.01165  -0.1065   0.8052   0.0380
  -9.250  -0.4787   0.01727   0.01155  -0.1061   0.7974   0.0388
  -9.000  -0.4528   0.01724   0.01146  -0.1057   0.7902   0.0396
  -8.750  -0.4269   0.01715   0.01131  -0.1053   0.7835   0.0405
  -8.500  -0.4014   0.01697   0.01104  -0.1048   0.7763   0.0415
  -8.250  -0.3762   0.01671   0.01066  -0.1043   0.7696   0.0426
  -8.000  -0.3508   0.01638   0.01021  -0.1039   0.7626   0.0436
  -7.750  -0.3251   0.01618   0.00987  -0.1034   0.7561   0.0443
  -7.500  -0.3006   0.01563   0.00922  -0.1029   0.7495   0.0452
  -7.250  -0.2754   0.01528   0.00882  -0.1024   0.7425   0.0461
  -7.000  -0.2495   0.01507   0.00856  -0.1020   0.7360   0.0468
  -6.750  -0.2234   0.01484   0.00828  -0.1016   0.7295   0.0477
  -6.500  -0.1976   0.01455   0.00791  -0.1012   0.7229   0.0484
  -6.250  -0.1715   0.01424   0.00752  -0.1008   0.7164   0.0492
  -6.000  -0.1454   0.01396   0.00715  -0.1004   0.7093   0.0501
  -5.750  -0.1194   0.01365   0.00675  -0.1000   0.7032   0.0508
  -5.500  -0.0931   0.01333   0.00635  -0.0996   0.6968   0.0514
  -5.250  -0.0668   0.01306   0.00599  -0.0992   0.6902   0.0519
  -5.000  -0.0404   0.01282   0.00568  -0.0988   0.6840   0.0525
  -4.750  -0.0137   0.01262   0.00542  -0.0985   0.6773   0.0529
  -4.500   0.0125   0.01236   0.00507  -0.0980   0.6715   0.0533
  -4.250   0.0382   0.01190   0.00458  -0.0976   0.6657   0.0542
  -4.000   0.0642   0.01159   0.00423  -0.0972   0.6594   0.0550
  -3.750   0.0904   0.01138   0.00396  -0.0967   0.6536   0.0558
  -3.500   0.1171   0.01118   0.00375  -0.0964   0.6478   0.0565
  -3.250   0.1437   0.01102   0.00355  -0.0961   0.6421   0.0573
  -3.000   0.1703   0.01089   0.00337  -0.0957   0.6366   0.0581
  -2.750   0.1972   0.01075   0.00321  -0.0954   0.6309   0.0591
  -2.500   0.2240   0.01063   0.00307  -0.0951   0.6252   0.0601
  -2.250   0.2506   0.01053   0.00292  -0.0947   0.6200   0.0610
  -2.000   0.2777   0.01042   0.00279  -0.0945   0.6144   0.0618
  -1.750   0.3045   0.01033   0.00267  -0.0941   0.6088   0.0626
  -1.500   0.3312   0.01028   0.00257  -0.0938   0.6034   0.0632
  -1.250   0.3582   0.01018   0.00247  -0.0935   0.5974   0.0642
  -1.000   0.3847   0.01009   0.00235  -0.0931   0.5910   0.0663
  -0.750   0.4113   0.01004   0.00228  -0.0928   0.5848   0.0685
  -0.500   0.4383   0.00998   0.00223  -0.0925   0.5785   0.0710
  -0.250   0.4649   0.00996   0.00219  -0.0921   0.5726   0.0744
   0.000   0.4917   0.00992   0.00216  -0.0919   0.5674   0.0803
   0.250   0.5184   0.00986   0.00214  -0.0916   0.5616   0.0922
   0.500   0.5442   0.00975   0.00215  -0.0911   0.5559   0.1350
   0.750   0.5704   0.00965   0.00218  -0.0908   0.5505   0.1782
   1.000   0.5967   0.00959   0.00221  -0.0905   0.5446   0.2111
   1.250   0.6224   0.00954   0.00225  -0.0900   0.5387   0.2532
   1.500   0.6476   0.00935   0.00232  -0.0896   0.5335   0.3439
   1.750   0.6710   0.00904   0.00238  -0.0889   0.5271   0.4785
   2.000   0.6825   0.00815   0.00254  -0.0853   0.5218   0.8356
   2.500   0.8073   0.00828   0.00278  -0.1002   0.5058   1.0000
   2.750   0.8315   0.00838   0.00285  -0.0994   0.4993   1.0000
   3.000   0.8552   0.00849   0.00293  -0.0985   0.4921   1.0000
   3.250   0.8789   0.00862   0.00302  -0.0976   0.4854   1.0000
   3.500   0.9028   0.00873   0.00311  -0.0968   0.4775   1.0000
   3.750   0.9261   0.00888   0.00322  -0.0959   0.4702   1.0000
   4.000   0.9498   0.00901   0.00333  -0.0950   0.4615   1.0000
   4.250   0.9725   0.00918   0.00345  -0.0940   0.4508   1.0000
   4.500   0.9943   0.00938   0.00359  -0.0928   0.4378   1.0000
   4.750   1.0156   0.00961   0.00374  -0.0915   0.4220   1.0000
   5.000   1.0366   0.00985   0.00392  -0.0902   0.4059   1.0000
   5.250   1.0570   0.01013   0.00412  -0.0889   0.3889   1.0000
   5.500   1.0775   0.01040   0.00433  -0.0875   0.3743   1.0000
   5.750   1.0986   0.01066   0.00454  -0.0863   0.3623   1.0000
   6.000   1.1192   0.01093   0.00477  -0.0850   0.3499   1.0000
   6.250   1.1392   0.01123   0.00502  -0.0836   0.3379   1.0000
   6.500   1.1583   0.01156   0.00530  -0.0821   0.3257   1.0000
   6.750   1.1779   0.01186   0.00557  -0.0806   0.3143   1.0000
   7.000   1.1972   0.01216   0.00585  -0.0792   0.3045   1.0000
   7.250   1.2151   0.01251   0.00617  -0.0775   0.2946   1.0000
   7.500   1.2336   0.01281   0.00647  -0.0759   0.2847   1.0000
   7.750   1.2490   0.01316   0.00680  -0.0737   0.2756   1.0000
   8.000   1.2634   0.01354   0.00714  -0.0714   0.2652   1.0000
   8.250   1.2774   0.01395   0.00753  -0.0691   0.2534   1.0000
   8.500   1.2882   0.01451   0.00802  -0.0664   0.2366   1.0000
   8.750   1.2982   0.01515   0.00857  -0.0637   0.2196   1.0000
   9.000   1.3084   0.01581   0.00916  -0.0611   0.2038   1.0000
   9.250   1.3196   0.01647   0.00978  -0.0588   0.1903   1.0000
   9.500   1.3299   0.01721   0.01048  -0.0566   0.1763   1.0000
   9.750   1.3397   0.01802   0.01125  -0.0544   0.1630   1.0000
  10.000   1.3494   0.01889   0.01208  -0.0523   0.1517   1.0000
  10.250   1.3569   0.01993   0.01306  -0.0501   0.1389   1.0000
  10.500   1.3663   0.02092   0.01404  -0.0483   0.1292   1.0000
  10.750   1.3759   0.02195   0.01507  -0.0466   0.1221   1.0000
  11.000   1.3857   0.02302   0.01613  -0.0451   0.1150   1.0000
  11.250   1.3941   0.02422   0.01733  -0.0435   0.1090   1.0000
  11.500   1.4041   0.02535   0.01849  -0.0422   0.1029   1.0000
  11.750   1.4116   0.02669   0.01984  -0.0408   0.0971   1.0000
  12.000   1.4205   0.02798   0.02115  -0.0395   0.0912   1.0000
  12.250   1.4259   0.02957   0.02273  -0.0382   0.0842   1.0000
  12.500   1.4296   0.03134   0.02447  -0.0369   0.0739   1.0000
  13.000   1.4168   0.03681   0.02973  -0.0337   0.0366   1.0000
  13.250   1.4137   0.03942   0.03234  -0.0325   0.0299   1.0000
  13.500   1.4161   0.04162   0.03459  -0.0317   0.0269   1.0000
  13.750   1.4178   0.04393   0.03696  -0.0310   0.0246   1.0000
  14.000   1.4201   0.04625   0.03934  -0.0304   0.0230   1.0000
  14.250   1.4235   0.04850   0.04166  -0.0299   0.0214   1.0000
  14.500   1.4257   0.05095   0.04418  -0.0295   0.0204   1.0000
  14.750   1.4263   0.05360   0.04690  -0.0292   0.0194   1.0000
  15.000   1.4277   0.05624   0.04961  -0.0289   0.0186   1.0000
  15.250   1.4298   0.05885   0.05231  -0.0288   0.0179   1.0000
  15.500   1.4303   0.06167   0.05521  -0.0288   0.0171   1.0000
  15.750   1.4297   0.06469   0.05831  -0.0288   0.0165   1.0000
  16.000   1.4272   0.06801   0.06170  -0.0290   0.0159   1.0000
  16.250   1.4247   0.07140   0.06517  -0.0293   0.0155   1.0000
  16.500   1.4235   0.07467   0.06854  -0.0296   0.0151   1.0000
  16.750   1.4212   0.07813   0.07209  -0.0301   0.0146   1.0000
  17.000   1.4187   0.08169   0.07574  -0.0307   0.0142   1.0000
  17.250   1.4152   0.08544   0.07959  -0.0314   0.0138   1.0000
  17.500   1.4104   0.08945   0.08368  -0.0323   0.0134   1.0000
  17.750   1.4038   0.09377   0.08808  -0.0333   0.0131   1.0000
  18.000   1.3969   0.09822   0.09264  -0.0345   0.0129   1.0000
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