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GOE 599 AIRFOIL (goe599-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 599 AIRFOIL (goe599-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.16 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe599-il-1000000-n5.txt
Download as CSV file: xf-goe599-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 599 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.9655   0.08113   0.07891  -0.0290   1.0000   0.0036
 -14.750  -1.0193   0.06641   0.06403  -0.0376   1.0000   0.0034
 -14.500  -1.0704   0.05076   0.04812  -0.0497   1.0000   0.0034
 -14.250  -1.0908   0.04243   0.03957  -0.0573   1.0000   0.0034
 -14.000  -1.1027   0.03723   0.03418  -0.0613   1.0000   0.0034
 -13.750  -1.1093   0.03408   0.03087  -0.0621   1.0000   0.0034
 -13.500  -1.1148   0.03187   0.02851  -0.0605   1.0000   0.0034
 -13.250  -1.1147   0.03026   0.02677  -0.0583   1.0000   0.0035
 -13.000  -1.1123   0.02848   0.02484  -0.0563   1.0000   0.0035
 -12.750  -1.1102   0.02668   0.02286  -0.0538   1.0000   0.0036
 -12.500  -1.1028   0.02530   0.02135  -0.0516   1.0000   0.0037
 -12.250  -1.0921   0.02419   0.02013  -0.0496   1.0000   0.0038
 -12.000  -1.0798   0.02320   0.01904  -0.0477   1.0000   0.0039
 -11.750  -1.0661   0.02230   0.01805  -0.0459   1.0000   0.0040
 -11.500  -1.0515   0.02145   0.01709  -0.0442   1.0000   0.0041
 -11.250  -1.0340   0.02061   0.01615  -0.0430   0.9998   0.0042
 -11.000  -1.0087   0.01971   0.01514  -0.0434   0.9989   0.0044
 -10.750  -0.9832   0.01886   0.01418  -0.0438   0.9980   0.0045
 -10.500  -0.9568   0.01806   0.01328  -0.0443   0.9970   0.0047
 -10.250  -0.9293   0.01729   0.01240  -0.0449   0.9960   0.0048
 -10.000  -0.9010   0.01659   0.01159  -0.0456   0.9951   0.0050
  -9.750  -0.8726   0.01595   0.01086  -0.0463   0.9942   0.0051
  -9.500  -0.8461   0.01523   0.01004  -0.0466   0.9927   0.0053
  -9.250  -0.8190   0.01453   0.00926  -0.0470   0.9912   0.0057
  -9.000  -0.7906   0.01399   0.00867  -0.0476   0.9900   0.0060
  -8.750  -0.7613   0.01352   0.00815  -0.0483   0.9889   0.0064
  -8.500  -0.7315   0.01308   0.00766  -0.0491   0.9879   0.0068
  -8.250  -0.7011   0.01265   0.00717  -0.0500   0.9870   0.0072
  -8.000  -0.6701   0.01223   0.00669  -0.0510   0.9862   0.0076
  -7.750  -0.6399   0.01171   0.00613  -0.0519   0.9853   0.0084
  -7.500  -0.6129   0.01134   0.00573  -0.0519   0.9827   0.0091
  -7.250  -0.5839   0.01100   0.00535  -0.0524   0.9806   0.0099
  -7.000  -0.5540   0.01069   0.00500  -0.0531   0.9787   0.0106
  -6.750  -0.5239   0.01032   0.00461  -0.0538   0.9769   0.0124
  -6.500  -0.4936   0.01001   0.00431  -0.0545   0.9751   0.0143
  -6.250  -0.4672   0.00975   0.00403  -0.0543   0.9710   0.0162
  -6.000  -0.4390   0.00948   0.00379  -0.0545   0.9675   0.0197
  -5.750  -0.4095   0.00927   0.00355  -0.0550   0.9644   0.0222
  -5.500  -0.3822   0.00905   0.00332  -0.0549   0.9600   0.0248
  -5.250  -0.3548   0.00882   0.00310  -0.0549   0.9547   0.0278
  -5.000  -0.3261   0.00863   0.00289  -0.0551   0.9502   0.0304
  -4.750  -0.2991   0.00848   0.00270  -0.0550   0.9432   0.0317
  -4.500  -0.2712   0.00828   0.00248  -0.0550   0.9363   0.0354
  -4.250  -0.2440   0.00808   0.00229  -0.0549   0.9270   0.0396
  -4.000  -0.2166   0.00788   0.00209  -0.0548   0.9158   0.0480
  -3.750  -0.1899   0.00756   0.00189  -0.0546   0.9005   0.0820
  -3.500  -0.1627   0.00746   0.00175  -0.0544   0.8815   0.0944
  -3.250  -0.1358   0.00739   0.00161  -0.0542   0.8596   0.1032
  -3.000  -0.1092   0.00740   0.00149  -0.0538   0.8345   0.1075
  -2.750  -0.0825   0.00739   0.00139  -0.0536   0.8110   0.1137
  -2.500  -0.0552   0.00736   0.00131  -0.0535   0.7946   0.1207
  -2.250  -0.0275   0.00721   0.00121  -0.0535   0.7852   0.1421
  -2.000  -0.0005   0.00691   0.00112  -0.0535   0.7771   0.2122
  -1.750   0.0274   0.00675   0.00106  -0.0537   0.7696   0.2457
  -1.500   0.0553   0.00665   0.00101  -0.0538   0.7618   0.2711
  -1.250   0.0829   0.00657   0.00097  -0.0538   0.7472   0.2999
  -1.000   0.1095   0.00645   0.00092  -0.0536   0.7195   0.3491
  -0.750   0.1363   0.00641   0.00088  -0.0535   0.6910   0.3837
  -0.500   0.1625   0.00643   0.00087  -0.0532   0.6498   0.4204
  -0.250   0.1890   0.00647   0.00088  -0.0530   0.6126   0.4552
   0.000   0.2150   0.00655   0.00091  -0.0528   0.5675   0.4969
   0.250   0.2409   0.00673   0.00097  -0.0525   0.5130   0.5263
   0.500   0.2663   0.00702   0.00105  -0.0522   0.4449   0.5499
   0.750   0.2920   0.00729   0.00115  -0.0520   0.3851   0.5717
   1.000   0.3184   0.00749   0.00124  -0.0518   0.3434   0.5920
   1.500   0.3707   0.00791   0.00145  -0.0515   0.2532   0.6372
   1.750   0.3934   0.00855   0.00172  -0.0508   0.1366   0.6611
   2.000   0.4182   0.00894   0.00192  -0.0504   0.0648   0.6872
   2.250   0.4449   0.00898   0.00204  -0.0502   0.0579   0.7258
   2.500   0.4703   0.00889   0.00218  -0.0497   0.0529   0.7996
   2.750   0.4914   0.00870   0.00235  -0.0480   0.0521   0.9064
   3.000   0.5195   0.00874   0.00250  -0.0478   0.0509   0.9722
   3.250   0.5549   0.00889   0.00265  -0.0496   0.0494   0.9904
   3.500   0.5884   0.00907   0.00282  -0.0510   0.0476   0.9986
   3.750   0.6155   0.00925   0.00298  -0.0509   0.0459   1.0000
   4.000   0.6412   0.00944   0.00317  -0.0505   0.0445   1.0000
   4.250   0.6670   0.00965   0.00339  -0.0502   0.0431   1.0000
   4.500   0.6925   0.00991   0.00366  -0.0498   0.0417   1.0000
   4.750   0.7181   0.01017   0.00395  -0.0494   0.0409   1.0000
   5.000   0.7444   0.01034   0.00413  -0.0492   0.0406   1.0000
   5.250   0.7709   0.01048   0.00428  -0.0490   0.0398   1.0000
   5.500   0.7974   0.01063   0.00443  -0.0488   0.0385   1.0000
   5.750   0.8237   0.01081   0.00461  -0.0487   0.0369   1.0000
   6.000   0.8498   0.01101   0.00480  -0.0484   0.0353   1.0000
   6.250   0.8756   0.01124   0.00503  -0.0482   0.0335   1.0000
   6.500   0.9012   0.01149   0.00528  -0.0479   0.0317   1.0000
   6.750   0.9274   0.01167   0.00548  -0.0477   0.0299   1.0000
   7.000   0.9531   0.01189   0.00566  -0.0474   0.0253   1.0000
   7.250   0.9775   0.01225   0.00594  -0.0470   0.0169   1.0000
   7.500   1.0012   0.01269   0.00635  -0.0464   0.0123   1.0000
   7.750   1.0252   0.01308   0.00678  -0.0458   0.0106   1.0000
   8.000   1.0485   0.01355   0.00727  -0.0451   0.0090   1.0000
   8.250   1.0720   0.01398   0.00773  -0.0445   0.0081   1.0000
   8.500   1.0956   0.01438   0.00818  -0.0439   0.0076   1.0000
   8.750   1.1187   0.01483   0.00867  -0.0432   0.0070   1.0000
   9.000   1.1412   0.01533   0.00920  -0.0425   0.0065   1.0000
   9.250   1.1628   0.01591   0.00983  -0.0416   0.0060   1.0000
   9.500   1.1842   0.01649   0.01049  -0.0406   0.0056   1.0000
   9.750   1.2062   0.01699   0.01104  -0.0398   0.0054   1.0000
  10.000   1.2276   0.01752   0.01162  -0.0390   0.0051   1.0000
  10.250   1.2485   0.01808   0.01224  -0.0380   0.0048   1.0000
  10.500   1.2688   0.01868   0.01289  -0.0370   0.0046   1.0000
  10.750   1.2883   0.01933   0.01360  -0.0359   0.0044   1.0000
  11.000   1.3067   0.02005   0.01439  -0.0346   0.0041   1.0000
  11.250   1.3234   0.02091   0.01533  -0.0331   0.0039   1.0000
  11.500   1.3389   0.02183   0.01635  -0.0314   0.0038   1.0000
  11.750   1.3553   0.02257   0.01718  -0.0299   0.0037   1.0000
  12.000   1.3691   0.02335   0.01806  -0.0279   0.0036   1.0000
  12.250   1.3810   0.02421   0.01901  -0.0257   0.0035   1.0000
  12.500   1.3921   0.02513   0.02002  -0.0235   0.0034   1.0000
  12.750   1.4022   0.02612   0.02112  -0.0212   0.0034   1.0000
  13.000   1.4114   0.02721   0.02231  -0.0190   0.0033   1.0000
  13.250   1.4194   0.02840   0.02360  -0.0169   0.0032   1.0000
  13.500   1.4266   0.02967   0.02499  -0.0148   0.0031   1.0000
  13.750   1.4328   0.03107   0.02651  -0.0128   0.0031   1.0000
  14.000   1.4377   0.03262   0.02817  -0.0109   0.0030   1.0000
  14.250   1.4414   0.03434   0.03001  -0.0093   0.0029   1.0000
  14.500   1.4436   0.03628   0.03206  -0.0078   0.0029   1.0000
  14.750   1.4448   0.03844   0.03435  -0.0066   0.0028   1.0000
  15.000   1.4440   0.04090   0.03693  -0.0056   0.0028   1.0000
  15.250   1.4411   0.04372   0.03988  -0.0050   0.0028   1.0000
  15.500   1.4366   0.04689   0.04318  -0.0048   0.0027   1.0000
  15.750   1.4298   0.05054   0.04697  -0.0050   0.0027   1.0000
  16.000   1.4203   0.05480   0.05138  -0.0058   0.0027   1.0000
  16.250   1.4079   0.05973   0.05646  -0.0073   0.0027   1.0000
  16.500   1.3930   0.06547   0.06234  -0.0096   0.0026   1.0000
  16.750   1.3729   0.07252   0.06957  -0.0130   0.0026   1.0000
  17.000   1.3487   0.08082   0.07804  -0.0173   0.0026   1.0000
  17.250   1.3178   0.09094   0.08835  -0.0229   0.0027   1.0000
  17.500   1.2740   0.10409   0.10172  -0.0300   0.0027   1.0000
  17.750   1.1736   0.13130   0.12929  -0.0441   0.0029   1.0000
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