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EPPLER 584 AIRFOIL (e584-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 584 AIRFOIL (e584-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.78 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e584-il-1000000-n5.txt
Download as CSV file: xf-e584-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 584 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3334   0.03772   0.03386  -0.1394   0.6522   0.0040
 -11.000  -0.3753   0.03288   0.02872  -0.1352   0.6514   0.0040
 -10.750  -0.3853   0.03082   0.02651  -0.1320   0.6506   0.0040
 -10.500  -0.3976   0.02861   0.02411  -0.1279   0.6498   0.0040
 -10.250  -0.4048   0.02691   0.02224  -0.1237   0.6490   0.0039
 -10.000  -0.4165   0.02490   0.01997  -0.1184   0.6482   0.0039
  -9.750  -0.4101   0.02360   0.01850  -0.1157   0.6474   0.0039
  -9.500  -0.4014   0.02226   0.01698  -0.1133   0.6466   0.0039
  -9.250  -0.3897   0.02105   0.01558  -0.1112   0.6457   0.0039
  -9.000  -0.3765   0.01981   0.01416  -0.1092   0.6448   0.0039
  -8.750  -0.3600   0.01886   0.01305  -0.1077   0.6440   0.0039
  -8.500  -0.3421   0.01797   0.01201  -0.1064   0.6431   0.0039
  -8.250  -0.3230   0.01717   0.01107  -0.1052   0.6421   0.0039
  -8.000  -0.3026   0.01649   0.01028  -0.1042   0.6411   0.0039
  -7.750  -0.2818   0.01582   0.00949  -0.1032   0.6399   0.0040
  -7.500  -0.2601   0.01524   0.00881  -0.1024   0.6386   0.0040
  -7.250  -0.2376   0.01472   0.00823  -0.1017   0.6377   0.0040
  -7.000  -0.2149   0.01420   0.00763  -0.1009   0.6370   0.0040
  -6.750  -0.1918   0.01373   0.00711  -0.1003   0.6362   0.0040
  -6.500  -0.1682   0.01332   0.00665  -0.0997   0.6353   0.0040
  -6.250  -0.1446   0.01291   0.00620  -0.0991   0.6343   0.0041
  -6.000  -0.1205   0.01255   0.00580  -0.0986   0.6333   0.0041
  -5.750  -0.0969   0.01215   0.00535  -0.0980   0.6321   0.0041
  -5.500  -0.0728   0.01178   0.00495  -0.0975   0.6308   0.0042
  -5.250  -0.0486   0.01144   0.00457  -0.0970   0.6295   0.0044
  -5.000  -0.0235   0.01120   0.00429  -0.0966   0.6284   0.0045
  -4.750   0.0018   0.01097   0.00404  -0.0963   0.6271   0.0048
  -4.500   0.0274   0.01079   0.00382  -0.0960   0.6257   0.0050
  -4.250   0.0533   0.01064   0.00364  -0.0958   0.6242   0.0055
  -4.000   0.0794   0.01045   0.00345  -0.0956   0.6231   0.0059
  -3.750   0.1055   0.01026   0.00326  -0.0954   0.6218   0.0068
  -3.500   0.1318   0.01009   0.00310  -0.0953   0.6202   0.0085
  -3.250   0.1581   0.00992   0.00295  -0.0952   0.6186   0.0122
  -3.000   0.1842   0.00974   0.00281  -0.0950   0.6169   0.0212
  -2.750   0.2105   0.00957   0.00269  -0.0949   0.6152   0.0326
  -2.500   0.2367   0.00940   0.00258  -0.0948   0.6135   0.0487
  -2.250   0.2620   0.00915   0.00248  -0.0946   0.6118   0.0869
  -2.000   0.2863   0.00882   0.00238  -0.0943   0.6101   0.1557
  -1.750   0.3113   0.00846   0.00229  -0.0941   0.6084   0.2346
  -1.500   0.3368   0.00814   0.00220  -0.0941   0.6064   0.3110
  -1.250   0.3620   0.00773   0.00211  -0.0940   0.6041   0.4118
  -1.000   0.3860   0.00705   0.00196  -0.0940   0.6017   0.5803
  -0.750   0.4101   0.00653   0.00203  -0.0936   0.5993   0.7574
  -0.500   0.4380   0.00660   0.00210  -0.0936   0.5971   0.7838
  -0.250   0.4665   0.00666   0.00214  -0.0938   0.5947   0.7951
   0.000   0.4957   0.00673   0.00219  -0.0942   0.5919   0.8065
   0.250   0.5227   0.00688   0.00236  -0.0940   0.5888   0.8178
   0.500   0.5491   0.00705   0.00253  -0.0936   0.5856   0.8277
   0.750   0.5756   0.00717   0.00264  -0.0933   0.5824   0.8328
   1.000   0.6040   0.00719   0.00264  -0.0937   0.5792   0.8339
   1.250   0.6325   0.00721   0.00263  -0.0940   0.5756   0.8347
   1.500   0.6605   0.00724   0.00263  -0.0943   0.5717   0.8355
   1.750   0.6879   0.00728   0.00263  -0.0944   0.5678   0.8363
   2.000   0.7159   0.00731   0.00264  -0.0947   0.5642   0.8368
   2.250   0.7439   0.00735   0.00267  -0.0950   0.5602   0.8373
   2.500   0.7713   0.00740   0.00269  -0.0952   0.5558   0.8378
   3.000   0.8258   0.00753   0.00277  -0.0955   0.5469   0.8390
   3.250   0.8528   0.00759   0.00282  -0.0956   0.5415   0.8394
   3.500   0.8784   0.00768   0.00288  -0.0954   0.5360   0.8399
   3.750   0.9056   0.00772   0.00293  -0.0956   0.5311   0.8405
   4.000   0.9318   0.00779   0.00299  -0.0955   0.5250   0.8410
   4.500   0.9830   0.00796   0.00315  -0.0953   0.5119   0.8420
   4.750   1.0069   0.00808   0.00324  -0.0948   0.5038   0.8425
   5.000   1.0317   0.00819   0.00334  -0.0945   0.4950   0.8430
   5.250   1.0547   0.00833   0.00346  -0.0938   0.4860   0.8436
   5.500   1.0768   0.00850   0.00360  -0.0930   0.4751   0.8442
   5.750   1.0979   0.00866   0.00374  -0.0920   0.4646   0.8450
   6.000   1.1164   0.00885   0.00391  -0.0904   0.4533   0.8458
   6.500   1.1532   0.00929   0.00429  -0.0874   0.4306   0.8472
   6.750   1.1711   0.00955   0.00452  -0.0858   0.4191   0.8480
   7.000   1.1875   0.00985   0.00478  -0.0840   0.4068   0.8487
   7.250   1.2030   0.01018   0.00508  -0.0821   0.3938   0.8495
   7.500   1.2172   0.01056   0.00541  -0.0799   0.3788   0.8504
   7.750   1.2294   0.01099   0.00578  -0.0775   0.3625   0.8512
   8.000   1.2430   0.01140   0.00616  -0.0753   0.3488   0.8520
   8.250   1.2539   0.01190   0.00661  -0.0728   0.3333   0.8529
   8.500   1.2641   0.01244   0.00711  -0.0702   0.3185   0.8537
   8.750   1.2734   0.01304   0.00766  -0.0676   0.3041   0.8545
   9.000   1.2814   0.01372   0.00830  -0.0649   0.2895   0.8552
   9.250   1.2882   0.01450   0.00902  -0.0622   0.2747   0.8559
   9.500   1.2931   0.01538   0.00987  -0.0593   0.2592   0.8572
   9.750   1.2987   0.01630   0.01076  -0.0567   0.2455   0.8585
  10.000   1.3038   0.01731   0.01174  -0.0541   0.2325   0.8596
  10.250   1.3076   0.01846   0.01286  -0.0516   0.2183   0.8607
  10.500   1.3128   0.01962   0.01399  -0.0494   0.2067   0.8617
  10.750   1.3179   0.02083   0.01518  -0.0473   0.1945   0.8627
  11.000   1.3224   0.02214   0.01646  -0.0452   0.1820   0.8637
  11.250   1.3239   0.02368   0.01796  -0.0430   0.1674   0.8648
  11.500   1.3250   0.02532   0.01954  -0.0409   0.1528   0.8658
  11.750   1.3276   0.02693   0.02111  -0.0391   0.1399   0.8668
  12.000   1.3319   0.02848   0.02264  -0.0376   0.1293   0.8678
  12.250   1.3358   0.03012   0.02425  -0.0361   0.1191   0.8687
  12.500   1.3390   0.03187   0.02598  -0.0347   0.1088   0.8696
  12.750   1.3447   0.03350   0.02760  -0.0337   0.1003   0.8704
  13.000   1.3504   0.03516   0.02925  -0.0326   0.0926   0.8712
  13.500   1.3538   0.03919   0.03322  -0.0303   0.0721   0.8731
  13.750   1.3573   0.04111   0.03513  -0.0293   0.0646   0.8741
  14.000   1.3614   0.04302   0.03705  -0.0285   0.0577   0.8752
  14.250   1.3579   0.04566   0.03961  -0.0274   0.0447   0.8762
  14.500   1.3601   0.04789   0.04183  -0.0267   0.0384   0.8772
  14.750   1.3676   0.04966   0.04364  -0.0262   0.0358   0.8783
  15.000   1.3655   0.05239   0.04635  -0.0256   0.0278   0.8793
  15.250   1.3722   0.05433   0.04834  -0.0253   0.0256   0.8805
  15.500   1.3753   0.05671   0.05073  -0.0250   0.0219   0.8817
  16.000   1.3822   0.06152   0.05561  -0.0248   0.0164   0.8841
  16.250   1.3862   0.06394   0.05806  -0.0248   0.0143   0.8852
  16.500   1.3899   0.06646   0.06063  -0.0249   0.0127   0.8863
  16.750   1.3927   0.06914   0.06335  -0.0251   0.0110   0.8872
  17.000   1.3968   0.07167   0.06594  -0.0253   0.0100   0.8885
  17.250   1.3999   0.07435   0.06869  -0.0256   0.0091   0.8898
  17.500   1.4031   0.07706   0.07147  -0.0260   0.0084   0.8911
  17.750   1.4043   0.08009   0.07456  -0.0265   0.0072   0.8925
  18.000   1.4069   0.08297   0.07751  -0.0270   0.0066   0.8939
  18.250   1.4082   0.08609   0.08071  -0.0277   0.0058   0.8953
  18.500   1.4102   0.08914   0.08382  -0.0284   0.0054   0.8968
  18.750   1.4098   0.09256   0.08732  -0.0293   0.0046   0.8983
  19.000   1.4096   0.09602   0.09085  -0.0303   0.0040   0.8997
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