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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
Reynolds number: 500,000
Max Cl/Cd: 125.49 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k131-il-500000-n5.txt
Download as CSV file: xf-fx62k131-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 62-K-131 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.1910   0.09773   0.09495  -0.0903   0.8852   0.0050
 -10.250  -0.1888   0.09316   0.09034  -0.0925   0.8779   0.0046
 -10.000  -0.1936   0.08583   0.08301  -0.0960   0.8709   0.0041
  -9.750  -0.1918   0.08131   0.07846  -0.0986   0.8649   0.0041
  -9.500  -0.1906   0.07657   0.07372  -0.1015   0.8591   0.0040
  -9.250  -0.1904   0.07136   0.06849  -0.1051   0.8538   0.0040
  -9.000  -0.1914   0.06538   0.06252  -0.1100   0.8491   0.0040
  -8.750  -0.1961   0.05618   0.05328  -0.1199   0.8435   0.0040
  -8.500  -0.2027   0.04977   0.04673  -0.1262   0.8381   0.0039
  -8.250  -0.2083   0.04369   0.04045  -0.1324   0.8328   0.0039
  -8.000  -0.2048   0.03820   0.03468  -0.1363   0.8286   0.0040
  -7.750  -0.1931   0.03396   0.03014  -0.1386   0.8253   0.0042
  -7.500  -0.1762   0.03047   0.02634  -0.1403   0.8225   0.0043
  -7.250  -0.1566   0.02694   0.02249  -0.1417   0.8193   0.0045
  -7.000  -0.1330   0.02517   0.02051  -0.1427   0.8164   0.0048
  -6.750  -0.1082   0.02287   0.01790  -0.1436   0.8139   0.0054
  -6.500  -0.0822   0.02022   0.01485  -0.1444   0.8116   0.0058
  -6.000  -0.0286   0.01622   0.01021  -0.1452   0.8069   0.0059
  -5.750  -0.0016   0.01494   0.00874  -0.1454   0.8044   0.0061
  -5.500   0.0259   0.01396   0.00760  -0.1457   0.8020   0.0063
  -5.250   0.0542   0.01325   0.00677  -0.1462   0.7996   0.0066
  -5.000   0.0839   0.01225   0.00568  -0.1473   0.7974   0.0074
  -4.500   0.1443   0.01144   0.00478  -0.1493   0.7929   0.0094
  -4.250   0.1745   0.01116   0.00444  -0.1502   0.7901   0.0107
  -4.000   0.2069   0.01060   0.00382  -0.1517   0.7872   0.0127
  -3.750   0.2379   0.01033   0.00347  -0.1528   0.7841   0.0151
  -3.500   0.2695   0.01007   0.00315  -0.1539   0.7813   0.0204
  -3.250   0.3011   0.00979   0.00292  -0.1551   0.7781   0.0383
  -3.000   0.3366   0.00922   0.00268  -0.1577   0.7753   0.1394
  -2.750   0.3896   0.00782   0.00235  -0.1654   0.7731   0.4727
  -2.500   0.4282   0.00748   0.00241  -0.1683   0.7708   0.6139
  -2.250   0.4585   0.00751   0.00248  -0.1689   0.7684   0.6549
  -2.000   0.4881   0.00757   0.00253  -0.1693   0.7657   0.6758
  -1.750   0.5172   0.00760   0.00255  -0.1697   0.7626   0.6828
  -1.500   0.5471   0.00763   0.00252  -0.1703   0.7595   0.6892
  -1.250   0.5759   0.00767   0.00254  -0.1706   0.7565   0.6936
  -1.000   0.6055   0.00772   0.00253  -0.1711   0.7538   0.6986
  -0.750   0.6351   0.00775   0.00255  -0.1717   0.7503   0.7037
  -0.500   0.6636   0.00780   0.00260  -0.1720   0.7467   0.7081
  -0.250   0.6928   0.00784   0.00262  -0.1724   0.7433   0.7129
   0.000   0.7225   0.00790   0.00263  -0.1730   0.7401   0.7175
   0.250   0.7504   0.00795   0.00272  -0.1731   0.7360   0.7214
   0.500   0.7790   0.00800   0.00278  -0.1734   0.7315   0.7258
   0.750   0.8082   0.00805   0.00279  -0.1739   0.7267   0.7300
   1.000   0.8362   0.00808   0.00285  -0.1741   0.7198   0.7329
   1.250   0.8638   0.00813   0.00291  -0.1741   0.7134   0.7355
   1.500   0.8920   0.00819   0.00298  -0.1744   0.7074   0.7383
   1.750   0.9204   0.00824   0.00305  -0.1747   0.7014   0.7414
   2.000   0.9493   0.00830   0.00311  -0.1751   0.6949   0.7445
   2.250   0.9769   0.00837   0.00321  -0.1752   0.6872   0.7467
   2.500   1.0041   0.00844   0.00331  -0.1753   0.6791   0.7489
   2.750   1.0312   0.00854   0.00341  -0.1753   0.6706   0.7512
   3.000   1.0586   0.00863   0.00353  -0.1753   0.6606   0.7539
   3.250   1.0860   0.00874   0.00367  -0.1754   0.6498   0.7567
   3.500   1.1131   0.00887   0.00379  -0.1755   0.6360   0.7595
   3.750   1.1365   0.00910   0.00395  -0.1747   0.6109   0.7613
   4.000   1.1563   0.00952   0.00419  -0.1732   0.5699   0.7634
   4.250   1.1758   0.01001   0.00452  -0.1718   0.5320   0.7657
   4.500   1.1968   0.01045   0.00486  -0.1707   0.5004   0.7681
   4.750   1.2150   0.01106   0.00527  -0.1691   0.4549   0.7707
   5.000   1.2313   0.01181   0.00576  -0.1672   0.4029   0.7735
   5.250   1.2424   0.01279   0.00641  -0.1645   0.3384   0.7754
   5.500   1.2522   0.01385   0.00713  -0.1615   0.2730   0.7773
   5.750   1.2585   0.01509   0.00797  -0.1580   0.1996   0.7795
   6.000   1.2659   0.01608   0.00874  -0.1547   0.1514   0.7820
   6.250   1.2718   0.01725   0.00962  -0.1512   0.1017   0.7847
   6.500   1.2828   0.01820   0.01041  -0.1487   0.0699   0.7871
   6.750   1.2924   0.01922   0.01128  -0.1460   0.0424   0.7889
   7.000   1.3028   0.02019   0.01217  -0.1435   0.0234   0.7908
   7.250   1.3159   0.02101   0.01299  -0.1414   0.0151   0.7928
   7.500   1.3278   0.02196   0.01393  -0.1393   0.0067   0.7950
   7.750   1.3403   0.02291   0.01491  -0.1373   0.0041   0.7972
   8.000   1.3539   0.02383   0.01592  -0.1355   0.0034   0.7994
   8.250   1.3667   0.02484   0.01702  -0.1337   0.0030   0.8016
   8.500   1.3789   0.02584   0.01812  -0.1319   0.0029   0.8033
   8.750   1.3909   0.02689   0.01928  -0.1300   0.0027   0.8051
   9.000   1.4022   0.02799   0.02048  -0.1282   0.0025   0.8069
   9.250   1.4132   0.02917   0.02177  -0.1265   0.0024   0.8089
   9.500   1.4234   0.03041   0.02309  -0.1247   0.0021   0.8111
   9.750   1.4326   0.03179   0.02457  -0.1229   0.0020   0.8132
  10.000   1.4402   0.03331   0.02619  -0.1210   0.0019   0.8152
  10.250   1.4466   0.03496   0.02795  -0.1190   0.0018   0.8168
  10.500   1.4514   0.03673   0.02985  -0.1169   0.0017   0.8185
  10.750   1.4534   0.03883   0.03211  -0.1146   0.0016   0.8203
  11.000   1.4524   0.04126   0.03469  -0.1122   0.0015   0.8219
  11.250   1.4572   0.04321   0.03675  -0.1105   0.0015   0.8237
  11.500   1.4611   0.04524   0.03891  -0.1087   0.0015   0.8257
  11.750   1.4661   0.04725   0.04103  -0.1073   0.0014   0.8276
  12.000   1.4689   0.04954   0.04345  -0.1057   0.0014   0.8294
  12.250   1.4706   0.05194   0.04599  -0.1041   0.0014   0.8307
  12.500   1.4717   0.05447   0.04867  -0.1027   0.0013   0.8321
  12.750   1.4720   0.05717   0.05152  -0.1013   0.0013   0.8337
  13.000   1.4714   0.06004   0.05455  -0.1000   0.0012   0.8354
  13.250   1.4702   0.06307   0.05773  -0.0989   0.0012   0.8372
  13.500   1.4682   0.06627   0.06108  -0.0979   0.0012   0.8390
  13.750   1.4652   0.06971   0.06469  -0.0971   0.0011   0.8406
  14.000   1.4612   0.07337   0.06852  -0.0965   0.0011   0.8421
  14.250   1.4563   0.07729   0.07261  -0.0961   0.0011   0.8435
  14.500   1.4508   0.08132   0.07683  -0.0959   0.0011   0.8448
  14.750   1.4439   0.08570   0.08138  -0.0959   0.0010   0.8463
  15.000   1.4357   0.09047   0.08637  -0.0963   0.0010   0.8478
  15.250   1.4266   0.09545   0.09155  -0.0970   0.0010   0.8494
  15.500   1.4168   0.10080   0.09708  -0.0982   0.0010   0.8511
  15.750   1.4060   0.10647   0.10294  -0.0997   0.0010   0.8526
  16.000   1.3943   0.11244   0.10910  -0.1017   0.0010   0.8541
  16.250   1.3820   0.11881   0.11565  -0.1041   0.0010   0.8555
  16.500   1.3686   0.12567   0.12270  -0.1072   0.0010   0.8569
  16.750   1.3557   0.13262   0.12984  -0.1106   0.0010   0.8581
  17.000   1.3413   0.14030   0.13771  -0.1148   0.0010   0.8593
  17.250   1.3274   0.14810   0.14568  -0.1193   0.0010   0.8606
  17.500   1.3134   0.15641   0.15416  -0.1244   0.0010   0.8620
  17.750   1.2982   0.16548   0.16341  -0.1302   0.0010   0.8634
  18.000   1.2841   0.17482   0.17290  -0.1363   0.0010   0.8649
  18.250   1.2697   0.18486   0.18309  -0.1430   0.0010   0.8663
  18.500   1.2519   0.19715   0.19552  -0.1511   0.0011   0.8674
  18.750   1.2320   0.21153   0.21003  -0.1601   0.0011   0.8682
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