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GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 13K AIRFOIL (goe13k-il)
Reynolds number: 500,000
Max Cl/Cd: 92.87 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe13k-il-500000.txt
Download as CSV file: xf-goe13k-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 13K 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.0036   0.09301   0.08995  -0.1590   0.9308   0.0519
 -10.750   0.0057   0.08930   0.08623  -0.1625   0.9304   0.0535
 -10.250  -0.0372   0.07935   0.07631  -0.1641   0.9202   0.0562
 -10.000  -0.0200   0.07731   0.07427  -0.1655   0.9197   0.0566
  -9.750  -0.0034   0.07516   0.07211  -0.1673   0.9191   0.0572
  -9.500   0.0094   0.07202   0.06896  -0.1704   0.9185   0.0579
  -9.250   0.0205   0.06830   0.06522  -0.1746   0.9179   0.0599
  -9.000  -0.1540   0.05036   0.04691  -0.1750   0.9009   0.0634
  -8.750  -0.1805   0.04982   0.04637  -0.1660   0.8922   0.0635
  -8.500  -0.1576   0.04856   0.04514  -0.1666   0.8914   0.0639
  -8.250  -0.1334   0.04762   0.04420  -0.1674   0.8907   0.0644
  -8.000  -0.1156   0.04561   0.04213  -0.1681   0.8897   0.0649
  -7.750  -0.3275   0.03246   0.02754  -0.1298   0.8652   0.0559
  -7.500  -0.3203   0.03117   0.02602  -0.1263   0.8623   0.0557
  -7.250  -0.3078   0.02880   0.02352  -0.1245   0.8609   0.0564
  -7.000  -0.2374   0.03317   0.02864  -0.1321   0.8618   0.0610
  -6.750  -0.2683   0.02555   0.01988  -0.1225   0.8592   0.0568
  -6.500  -0.2444   0.02419   0.01834  -0.1221   0.8585   0.0571
  -6.250  -0.2779   0.02508   0.01921  -0.1096   0.8474   0.0571
  -6.000  -0.2551   0.02433   0.01841  -0.1089   0.8461   0.0577
  -5.750  -0.2320   0.02338   0.01732  -0.1081   0.8451   0.0580
  -5.500  -0.2060   0.02262   0.01646  -0.1079   0.8444   0.0587
  -5.250  -0.1794   0.02171   0.01542  -0.1078   0.8438   0.0592
  -5.000  -0.1514   0.02084   0.01440  -0.1079   0.8432   0.0597
  -4.750  -0.1896   0.02195   0.01548  -0.0945   0.8318   0.0594
  -4.500  -0.1661   0.02132   0.01474  -0.0937   0.8305   0.0599
  -4.250  -0.1399   0.02068   0.01399  -0.0933   0.8296   0.0604
  -4.000  -0.1119   0.02009   0.01331  -0.0933   0.8289   0.0610
  -3.750  -0.0825   0.01954   0.01268  -0.0936   0.8284   0.0616
  -3.500  -0.0514   0.01906   0.01212  -0.0943   0.8279   0.0623
  -3.250  -0.0873   0.02043   0.01347  -0.0816   0.8166   0.0624
  -3.000  -0.0599   0.02000   0.01298  -0.0814   0.8154   0.0627
  -2.750  -0.0272   0.01903   0.01197  -0.0824   0.8149   0.0635
  -2.500   0.0045   0.01830   0.01125  -0.0832   0.8144   0.0644
  -2.250   0.0370   0.01775   0.01071  -0.0841   0.8138   0.0651
  -2.000   0.0678   0.01732   0.01028  -0.0847   0.8133   0.0662
  -1.750   0.1027   0.01679   0.00975  -0.0861   0.8129   0.0670
  -1.500   0.1332   0.01646   0.00942  -0.0866   0.8123   0.0684
  -1.250   0.1121   0.01751   0.01046  -0.0769   0.8044   0.0685
  -1.000   0.1558   0.01688   0.00983  -0.0800   0.8059   0.0704
  -0.750   0.1984   0.01628   0.00922  -0.0829   0.8068   0.0715
  -0.500   0.2430   0.01547   0.00845  -0.0863   0.8074   0.0738
  -0.250   0.2883   0.01491   0.00792  -0.0900   0.8082   0.0765
   0.000   0.3347   0.01446   0.00747  -0.0939   0.8089   0.0796
   1.000   0.7044   0.01167   0.00766  -0.1538   0.8134   0.9421
   1.250   0.7278   0.01185   0.00779  -0.1526   0.8120   0.9813
   1.500   0.8184   0.01195   0.00788  -0.1667   0.8127   0.9949
   1.750   0.8911   0.01174   0.00765  -0.1768   0.8126   1.0000
   2.000   0.9305   0.01154   0.00742  -0.1795   0.8112   1.0000
   2.250   0.9701   0.01141   0.00727  -0.1823   0.8100   1.0000
   2.500   0.9122   0.01223   0.00814  -0.1638   0.8013   1.0000
   2.750   0.9403   0.01210   0.00799  -0.1639   0.7988   1.0000
   3.000   0.9772   0.01187   0.00774  -0.1659   0.7968   1.0000
   3.250   1.0266   0.01146   0.00729  -0.1706   0.7946   1.0000
   3.500   0.9964   0.01200   0.00787  -0.1580   0.7864   1.0000
   3.750   1.0308   0.01160   0.00744  -0.1593   0.7811   1.0000
   4.000   1.0380   0.01161   0.00744  -0.1547   0.7730   1.0000
   4.250   1.0578   0.01139   0.00717  -0.1527   0.7634   1.0000
   4.500   1.0505   0.01174   0.00754  -0.1452   0.7533   1.0000
   4.750   1.0692   0.01169   0.00744  -0.1432   0.7433   1.0000
   5.000   1.0720   0.01201   0.00778  -0.1379   0.7333   1.0000
   5.250   1.0797   0.01228   0.00805  -0.1337   0.7226   1.0000
   5.500   1.0930   0.01246   0.00820  -0.1307   0.7104   1.0000
   5.750   1.1005   0.01280   0.00852  -0.1266   0.6954   1.0000
   6.000   1.1026   0.01330   0.00898  -0.1214   0.6718   1.0000
   6.250   1.0976   0.01402   0.00949  -0.1149   0.6190   1.0000
   6.500   1.0474   0.01642   0.01129  -0.1001   0.5181   1.0000
   6.750   1.0330   0.01799   0.01259  -0.0926   0.4769   1.0000
   7.000   1.0360   0.01896   0.01344  -0.0885   0.4539   1.0000
   7.250   1.0429   0.01979   0.01419  -0.0851   0.4367   1.0000
   7.500   1.0531   0.02051   0.01485  -0.0823   0.4229   1.0000
   7.750   1.0643   0.02121   0.01549  -0.0798   0.4090   1.0000
   8.000   1.0776   0.02183   0.01609  -0.0776   0.3960   1.0000
   8.250   1.0903   0.02248   0.01671  -0.0754   0.3824   1.0000
   8.500   1.1027   0.02317   0.01736  -0.0731   0.3668   1.0000
   8.750   1.1143   0.02391   0.01804  -0.0708   0.3481   1.0000
   9.000   1.1247   0.02474   0.01879  -0.0683   0.3241   1.0000
   9.250   1.1311   0.02578   0.01966  -0.0654   0.2890   1.0000
   9.500   1.1324   0.02713   0.02074  -0.0618   0.2425   1.0000
   9.750   1.1353   0.02843   0.02177  -0.0585   0.1995   1.0000
  10.000   1.1407   0.02962   0.02272  -0.0556   0.1623   1.0000
  10.250   1.1504   0.03059   0.02357  -0.0534   0.1427   1.0000
  10.500   1.1608   0.03154   0.02443  -0.0513   0.1273   1.0000
  10.750   1.1729   0.03239   0.02523  -0.0495   0.1164   1.0000
  11.000   1.1857   0.03324   0.02605  -0.0477   0.1083   1.0000
  11.250   1.1972   0.03416   0.02694  -0.0459   0.1018   1.0000
  11.500   1.2098   0.03502   0.02782  -0.0442   0.0967   1.0000
  11.750   1.2228   0.03587   0.02867  -0.0426   0.0924   1.0000
  12.000   1.2326   0.03693   0.02970  -0.0407   0.0876   1.0000
  12.250   1.2467   0.03773   0.03056  -0.0394   0.0848   1.0000
  12.500   1.2590   0.03865   0.03150  -0.0378   0.0818   1.0000
  12.750   1.2687   0.03978   0.03261  -0.0360   0.0786   1.0000
  13.000   1.2798   0.04081   0.03368  -0.0344   0.0763   1.0000
  13.250   1.2924   0.04174   0.03467  -0.0330   0.0740   1.0000
  13.500   1.3038   0.04276   0.03572  -0.0316   0.0713   1.0000
  13.750   1.3120   0.04404   0.03699  -0.0298   0.0688   1.0000
  14.000   1.3215   0.04523   0.03824  -0.0283   0.0667   1.0000
  14.250   1.3333   0.04627   0.03934  -0.0270   0.0645   1.0000
  14.500   1.3438   0.04742   0.04051  -0.0256   0.0623   1.0000
  14.750   1.3487   0.04903   0.04213  -0.0238   0.0600   1.0000
  15.000   1.3575   0.05035   0.04352  -0.0224   0.0584   1.0000
  15.250   1.3687   0.05148   0.04473  -0.0213   0.0563   1.0000
  15.500   1.3764   0.05292   0.04620  -0.0199   0.0544   1.0000
  15.750   1.3798   0.05475   0.04803  -0.0182   0.0525   1.0000
  16.000   1.3869   0.05628   0.04965  -0.0169   0.0508   1.0000
  16.250   1.3956   0.05770   0.05114  -0.0158   0.0488   1.0000
  16.500   1.4030   0.05926   0.05274  -0.0147   0.0472   1.0000
  16.750   1.4032   0.06151   0.05500  -0.0132   0.0457   1.0000
  17.000   1.4094   0.06323   0.05682  -0.0121   0.0443   1.0000
  17.250   1.4143   0.06510   0.05877  -0.0111   0.0429   1.0000
  17.500   1.4200   0.06692   0.06064  -0.0102   0.0412   1.0000
  17.750   1.4197   0.06938   0.06313  -0.0091   0.0401   1.0000
  18.000   1.4196   0.07186   0.06569  -0.0081   0.0390   1.0000
  18.250   1.4232   0.07403   0.06796  -0.0074   0.0377   1.0000
  18.500   1.4252   0.07639   0.07040  -0.0067   0.0368   1.0000
  18.750   1.4254   0.07900   0.07307  -0.0062   0.0357   1.0000
  19.000   1.4222   0.08202   0.07613  -0.0057   0.0347   1.0000
  19.250   1.4187   0.08513   0.07932  -0.0053   0.0340   1.0000
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