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NACA 65(3)-618 (naca653618-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NACA 65(3)-618 (naca653618-il)
Reynolds number: 100,000
Max Cl/Cd: 27.83 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca653618-il-100000.txt
Download as CSV file: xf-naca653618-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 65(3)-618                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3556   0.11886   0.11426  -0.0627   0.9828   0.1634
 -11.000  -0.3290   0.11590   0.11124  -0.0636   0.9779   0.1692
 -10.750  -0.3472   0.11010   0.10550  -0.0708   0.9725   0.1790
 -10.500  -0.3053   0.10734   0.10265  -0.0716   0.9703   0.1859
 -10.250  -0.3205   0.10270   0.09807  -0.0757   0.9628   0.1965
 -10.000  -0.2928   0.09992   0.09524  -0.0773   0.9590   0.2058
  -9.750  -0.2821   0.09541   0.09071  -0.0813   0.9559   0.2160
  -9.500  -0.3064   0.09162   0.08701  -0.0838   0.9464   0.2295
  -9.250  -0.2727   0.08838   0.08370  -0.0852   0.9433   0.2337
  -9.000  -0.5878   0.05911   0.05298  -0.0906   0.9098   0.0979
  -8.750  -0.5752   0.05409   0.04761  -0.0915   0.9062   0.0924
  -8.500  -0.6054   0.05218   0.04484  -0.0844   0.8960   0.0874
  -8.250  -0.5859   0.04999   0.04224  -0.0844   0.8914   0.0870
  -8.000  -0.5562   0.04722   0.03906  -0.0860   0.8885   0.0868
  -7.750  -0.5590   0.04582   0.03752  -0.0818   0.8812   0.0865
  -7.500  -0.5420   0.04383   0.03526  -0.0809   0.8767   0.0863
  -7.250  -0.5144   0.04196   0.03305  -0.0815   0.8734   0.0866
  -7.000  -0.4788   0.03953   0.03049  -0.0836   0.8712   0.0889
  -6.750  -0.4782   0.03904   0.02995  -0.0796   0.8644   0.0899
  -6.500  -0.4586   0.03813   0.02894  -0.0787   0.8597   0.0916
  -6.250  -0.4290   0.03708   0.02779  -0.0791   0.8566   0.0936
  -6.000  -0.3941   0.03614   0.02673  -0.0803   0.8543   0.0966
  -5.750  -0.3812   0.03597   0.02643  -0.0782   0.8500   0.0991
  -5.500  -0.3750   0.03559   0.02611  -0.0751   0.8445   0.1018
  -5.250  -0.3517   0.03496   0.02560  -0.0746   0.8408   0.1061
  -5.000  -0.3226   0.03441   0.02505  -0.0749   0.8380   0.1120
  -4.750  -0.2910   0.03368   0.02446  -0.0759   0.8359   0.1216
  -4.500  -0.3012   0.03412   0.02490  -0.0707   0.8305   0.1263
  -4.250  -0.2892   0.03381   0.02469  -0.0691   0.8262   0.1392
  -4.000  -0.2660   0.03232   0.02379  -0.0699   0.8229   0.2108
  -3.750  -0.2511   0.03211   0.02554  -0.0667   0.8203   0.6193
  -3.500  -0.2262   0.03372   0.02709  -0.0638   0.8181   0.6557
  -3.250  -0.2381   0.03475   0.02809  -0.0583   0.8135   0.6696
  -3.000  -0.2306   0.03580   0.02909  -0.0544   0.8094   0.6867
  -2.750  -0.2198   0.03694   0.03019  -0.0504   0.8065   0.7032
  -2.500  -0.2097   0.03823   0.03147  -0.0458   0.8043   0.7231
  -2.250  -0.2071   0.04000   0.03333  -0.0373   0.8021   0.7466
  -2.000  -0.2144   0.04129   0.03465  -0.0294   0.7990   0.7674
  -1.750  -0.2244   0.04219   0.03557  -0.0224   0.7968   0.7849
  -1.500  -0.2275   0.04296   0.03633  -0.0167   0.7960   0.8019
  -1.250  -0.2209   0.04331   0.03661  -0.0140   0.7941   0.8134
  -1.000  -0.2094   0.04360   0.03682  -0.0124   0.7923   0.8201
  -0.750  -0.1924   0.04397   0.03708  -0.0132   0.7924   0.8269
  -0.500  -0.1837   0.04434   0.03741  -0.0112   0.7928   0.8317
  -0.250  -0.1882   0.04524   0.03831  -0.0091   0.8068   0.8373
   0.000  -0.1511   0.04579   0.03872  -0.0121   0.8030   0.8424
   0.250  -0.1234   0.04648   0.03932  -0.0133   0.8016   0.8466
   0.500  -0.1846   0.04742   0.04043  -0.0048   0.8482   0.8526
   0.750  -0.1585   0.04777   0.04069  -0.0062   0.8409   0.8576
   1.000  -0.1193   0.04909   0.04190  -0.0095   0.8367   0.8619
   1.250  -0.1011   0.04988   0.04264  -0.0093   0.8345   0.8661
   1.500  -0.0929   0.04933   0.04207  -0.0077   0.8246   0.8714
   1.750  -0.0532   0.05065   0.04329  -0.0112   0.8199   0.8764
   2.000  -0.0308   0.05179   0.04441  -0.0116   0.8174   0.8807
   2.250  -0.0249   0.05122   0.04383  -0.0097   0.8068   0.8860
   2.500   0.0151   0.05270   0.04525  -0.0130   0.8023   0.8917
   2.750   0.0184   0.05286   0.04542  -0.0107   0.7968   0.8973
   3.000   0.0433   0.05338   0.04592  -0.0115   0.7881   0.9031
   3.250   0.0895   0.05545   0.04794  -0.0155   0.7841   0.9089
   3.500   0.0808   0.05476   0.04728  -0.0117   0.7743   0.9161
   3.750   0.1218   0.05615   0.04866  -0.0146   0.7681   0.9237
   4.000   0.1236   0.05639   0.04892  -0.0127   0.7602   0.9318
   4.250   0.1617   0.05743   0.04997  -0.0151   0.7519   0.9398
   4.500   0.1716   0.05813   0.05070  -0.0147   0.7441   0.9496
   4.750   0.2390   0.05981   0.05239  -0.0204   0.7329   0.9592
   5.000   0.2375   0.05988   0.05254  -0.0195   0.7213   0.9702
   5.250   0.3300   0.05703   0.04963  -0.0243   0.6717   0.9799
   5.500   0.3695   0.05745   0.05009  -0.0271   0.6618   1.0000
   5.750   0.3989   0.05818   0.05085  -0.0292   0.6532   1.0000
   6.000   0.4257   0.05902   0.05172  -0.0310   0.6429   1.0000
   6.250   0.4672   0.05946   0.05220  -0.0339   0.6356   1.0000
   6.500   0.4870   0.06060   0.05340  -0.0352   0.6246   1.0000
   6.750   0.5341   0.06075   0.05360  -0.0382   0.6185   1.0000
   7.000   0.5504   0.06202   0.05493  -0.0391   0.6064   1.0000
   7.250   0.6023   0.06172   0.05470  -0.0422   0.6014   1.0000
   7.500   0.6154   0.06312   0.05616  -0.0427   0.5886   1.0000
   7.750   0.6700   0.06234   0.05549  -0.0454   0.5845   1.0000
   8.000   0.6813   0.06375   0.05696  -0.0456   0.5711   1.0000
   8.250   0.7382   0.06240   0.05574  -0.0480   0.5678   1.0000
   8.500   0.7499   0.06361   0.05702  -0.0478   0.5539   1.0000
   8.750   0.8078   0.06166   0.05520  -0.0497   0.5511   1.0000
   9.000   0.8201   0.06263   0.05627  -0.0493   0.5371   1.0000
  10.000   1.0522   0.04469   0.03900  -0.0496   0.5046   1.0000
  10.250   1.0823   0.04281   0.03727  -0.0486   0.4892   1.0000
  10.500   1.0952   0.04284   0.03740  -0.0471   0.4680   1.0000
  10.750   1.1210   0.04156   0.03619  -0.0459   0.4395   1.0000
  11.000   1.1398   0.04095   0.03542  -0.0441   0.3879   1.0000
  11.250   1.1412   0.04186   0.03558  -0.0410   0.2980   1.0000
  11.500   1.1194   0.04579   0.03890  -0.0383   0.2258   1.0000
  11.750   1.0964   0.05029   0.04280  -0.0361   0.1664   1.0000
  12.000   1.0815   0.05431   0.04631  -0.0344   0.1290   1.0000
  12.250   1.0804   0.05711   0.04890  -0.0331   0.1082   1.0000
  12.500   1.0864   0.05923   0.05087  -0.0321   0.0961   1.0000
  12.750   1.0975   0.06086   0.05235  -0.0312   0.0872   1.0000
  13.000   1.1132   0.06213   0.05356  -0.0305   0.0804   1.0000
  13.250   1.1391   0.06263   0.05399  -0.0296   0.0750   1.0000
  13.500   1.1620   0.06356   0.05490  -0.0291   0.0704   1.0000
  13.750   1.1969   0.06400   0.05524  -0.0287   0.0661   1.0000
  14.000   1.2248   0.06518   0.05658  -0.0284   0.0634   1.0000
  14.250   1.2544   0.06653   0.05804  -0.0283   0.0612   1.0000
  14.500   1.3111   0.06786   0.05922  -0.0295   0.0581   1.0000
  14.750   1.3133   0.07068   0.06238  -0.0287   0.0574   1.0000
  15.000   1.3150   0.07378   0.06581  -0.0280   0.0565   1.0000
  15.250   1.3164   0.07716   0.06952  -0.0274   0.0559   1.0000
  15.500   1.3152   0.08091   0.07358  -0.0270   0.0557   1.0000
  15.750   1.3095   0.08503   0.07802  -0.0266   0.0556   1.0000
  16.000   1.2993   0.08955   0.08285  -0.0265   0.0556   1.0000
  16.250   1.2855   0.09446   0.08805  -0.0267   0.0558   1.0000
  16.500   1.2687   0.09977   0.09365  -0.0274   0.0561   1.0000
  16.750   1.2501   0.10547   0.09962  -0.0285   0.0564   1.0000
  17.000   1.2299   0.11159   0.10599  -0.0302   0.0568   1.0000
  17.250   1.2096   0.11806   0.11268  -0.0325   0.0572   1.0000
  17.500   1.1904   0.12482   0.11963  -0.0352   0.0576   1.0000
  17.750   1.1773   0.13142   0.12637  -0.0379   0.0581   1.0000
  18.000   0.9885   0.17842   0.17399  -0.0685   0.0686   1.0000
  18.250   1.0081   0.17772   0.17330  -0.0672   0.0679   1.0000
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