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NACA 65(3)-618 (naca653618-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 65(3)-618 (naca653618-il)
Reynolds number: 100,000
Max Cl/Cd: 28.98 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca653618-il-100000-n5.txt
Download as CSV file: xf-naca653618-il-100000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.4159   0.08639   0.08113  -0.0932   0.9771   0.0415
 -12.500  -0.4664   0.07274   0.06720  -0.1047   0.9696   0.0407
 -12.250  -0.4947   0.06489   0.05904  -0.1112   0.9610   0.0405
 -12.000  -0.5110   0.05931   0.05316  -0.1156   0.9522   0.0405
 -11.750  -0.5185   0.05491   0.04845  -0.1189   0.9443   0.0409
 -11.500  -0.5258   0.05154   0.04478  -0.1201   0.9335   0.0414
 -11.250  -0.5277   0.04831   0.04117  -0.1212   0.9251   0.0421
 -11.000  -0.5348   0.04603   0.03857  -0.1196   0.9130   0.0427
 -10.750  -0.5351   0.04372   0.03587  -0.1183   0.9040   0.0433
 -10.500  -0.5302   0.04159   0.03332  -0.1170   0.8955   0.0438
 -10.250  -0.5151   0.03947   0.03086  -0.1169   0.8899   0.0443
 -10.000  -0.5001   0.03808   0.02942  -0.1159   0.8818   0.0451
  -9.750  -0.4787   0.03670   0.02791  -0.1160   0.8764   0.0463
  -9.500  -0.4592   0.03542   0.02647  -0.1156   0.8707   0.0475
  -9.250  -0.4420   0.03418   0.02504  -0.1146   0.8637   0.0485
  -9.000  -0.4168   0.03277   0.02339  -0.1147   0.8591   0.0495
  -8.750  -0.3897   0.03148   0.02188  -0.1149   0.8550   0.0506
  -8.500  -0.3698   0.03055   0.02085  -0.1139   0.8479   0.0516
  -8.250  -0.3447   0.02960   0.01993  -0.1139   0.8430   0.0532
  -8.000  -0.3176   0.02871   0.01898  -0.1141   0.8393   0.0551
  -7.750  -0.2984   0.02808   0.01829  -0.1130   0.8333   0.0568
  -7.500  -0.2771   0.02742   0.01754  -0.1120   0.8278   0.0583
  -7.250  -0.2540   0.02665   0.01675  -0.1115   0.8235   0.0599
  -7.000  -0.2348   0.02599   0.01609  -0.1106   0.8190   0.0619
  -6.750  -0.2229   0.02560   0.01570  -0.1084   0.8120   0.0645
  -6.500  -0.2045   0.02510   0.01510  -0.1073   0.8073   0.0679
  -6.250  -0.1852   0.02443   0.01442  -0.1064   0.8038   0.0714
  -6.000  -0.1739   0.02412   0.01409  -0.1042   0.7977   0.0752
  -5.750  -0.1591   0.02368   0.01362  -0.1025   0.7923   0.0806
  -5.500  -0.1398   0.02310   0.01302  -0.1016   0.7884   0.0908
  -5.250  -0.1200   0.02231   0.01235  -0.1010   0.7852   0.1128
  -5.000  -0.1143   0.02179   0.01212  -0.0982   0.7781   0.1577
  -4.750  -0.1057   0.02039   0.01144  -0.0968   0.7734   0.2943
  -4.500  -0.0904   0.01974   0.01181  -0.0947   0.7703   0.4900
  -4.250  -0.0617   0.01991   0.01195  -0.0945   0.7680   0.5509
  -4.000  -0.0468   0.02031   0.01229  -0.0925   0.7616   0.5789
  -3.750  -0.0253   0.02112   0.01314  -0.0903   0.7574   0.6178
  -3.500  -0.0020   0.02220   0.01421  -0.0876   0.7543   0.6509
  -3.250   0.0248   0.02276   0.01469  -0.0862   0.7519   0.6681
  -3.000   0.0451   0.02312   0.01501  -0.0844   0.7480   0.6733
  -2.750   0.0620   0.02331   0.01512  -0.0828   0.7429   0.6796
  -2.500   0.0877   0.02315   0.01482  -0.0832   0.7394   0.6864
  -2.250   0.1151   0.02316   0.01474  -0.0830   0.7367   0.6895
  -2.000   0.1452   0.02306   0.01452  -0.0835   0.7345   0.6932
  -1.750   0.1640   0.02318   0.01459  -0.0825   0.7301   0.6979
  -1.500   0.1835   0.02323   0.01455  -0.0822   0.7253   0.7037
  -1.250   0.2073   0.02332   0.01459  -0.0817   0.7221   0.7064
  -1.000   0.2349   0.02331   0.01452  -0.0818   0.7197   0.7095
  -0.750   0.2657   0.02321   0.01434  -0.0825   0.7177   0.7128
  -0.500   0.2892   0.02330   0.01438  -0.0824   0.7142   0.7170
  -0.250   0.3025   0.02368   0.01473  -0.0811   0.7084   0.7225
   0.000   0.3246   0.02385   0.01490  -0.0803   0.7052   0.7250
   0.250   0.3521   0.02388   0.01490  -0.0805   0.7028   0.7278
   0.500   0.3829   0.02383   0.01481  -0.0812   0.7009   0.7312
   0.750   0.4162   0.02374   0.01467  -0.0825   0.6993   0.7352
   1.000   0.4149   0.02469   0.01567  -0.0791   0.6913   0.7407
   1.250   0.4355   0.02495   0.01595  -0.0782   0.6880   0.7434
   1.500   0.4630   0.02502   0.01602  -0.0783   0.6857   0.7464
   1.750   0.4943   0.02499   0.01599  -0.0791   0.6839   0.7500
   2.000   0.5287   0.02491   0.01589  -0.0806   0.6824   0.7543
   2.500   0.5359   0.02665   0.01777  -0.0744   0.6698   0.7630
   2.750   0.5663   0.02666   0.01780  -0.0750   0.6678   0.7665
   3.000   0.5995   0.02663   0.01779  -0.0762   0.6663   0.7707
   3.250   0.6352   0.02657   0.01775  -0.0779   0.6650   0.7755
   3.750   0.6294   0.02877   0.02012  -0.0697   0.6508   0.7852
   4.000   0.6637   0.02863   0.02003  -0.0709   0.6493   0.7898
   5.000   0.6882   0.03334   0.02504  -0.0624   0.6213   0.8130
   5.250   0.7143   0.03328   0.02507  -0.0620   0.6185   0.8179
   5.500   0.7468   0.03295   0.02482  -0.0625   0.6167   0.8236
   5.750   0.7843   0.03247   0.02441  -0.0638   0.6154   0.8296
   6.250   0.7969   0.03470   0.02686  -0.0595   0.6000   0.8436
   6.500   0.8320   0.03400   0.02627  -0.0599   0.5986   0.8500
   7.250   0.8418   0.03792   0.03053  -0.0531   0.5701   0.8778
   7.500   0.8735   0.03696   0.02970  -0.0527   0.5675   0.8869
   7.750   0.9124   0.03556   0.02844  -0.0529   0.5656   0.8973
   8.250   0.9207   0.03751   0.03066  -0.0483   0.5447   0.9319
   8.750   0.9898   0.03526   0.02871  -0.0491   0.5320   1.0000
   9.250   0.9992   0.03805   0.03165  -0.0468   0.4953   1.0000
   9.500   1.0166   0.03810   0.03173  -0.0460   0.4701   1.0000
   9.750   1.0362   0.03798   0.03154  -0.0451   0.4359   1.0000
  10.000   1.0647   0.03713   0.03046  -0.0445   0.3910   1.0000
  10.250   1.0821   0.03734   0.03031  -0.0433   0.3406   1.0000
  10.500   1.0840   0.03917   0.03184  -0.0416   0.2954   1.0000
  10.750   1.0807   0.04162   0.03401  -0.0401   0.2528   1.0000
  11.000   1.0765   0.04433   0.03646  -0.0387   0.2131   1.0000
  11.250   1.0730   0.04712   0.03900  -0.0375   0.1749   1.0000
  11.500   1.0706   0.04991   0.04154  -0.0366   0.1384   1.0000
  11.750   1.0691   0.05272   0.04412  -0.0358   0.1071   1.0000
  12.000   1.0702   0.05537   0.04660  -0.0352   0.0853   1.0000
  12.250   1.0728   0.05794   0.04906  -0.0347   0.0722   1.0000
  12.500   1.0769   0.06042   0.05152  -0.0343   0.0638   1.0000
  12.750   1.0822   0.06284   0.05398  -0.0340   0.0578   1.0000
  13.000   1.0862   0.06542   0.05656  -0.0338   0.0537   1.0000
  13.250   1.0921   0.06784   0.05907  -0.0337   0.0501   1.0000
  13.500   1.0960   0.07051   0.06175  -0.0337   0.0475   1.0000
  13.750   1.1027   0.07289   0.06422  -0.0336   0.0449   1.0000
  14.000   1.1092   0.07532   0.06672  -0.0336   0.0430   1.0000
  14.250   1.1149   0.07782   0.06925  -0.0337   0.0414   1.0000
  14.500   1.1224   0.08011   0.07162  -0.0337   0.0398   1.0000
  14.750   1.1314   0.08226   0.07388  -0.0337   0.0381   1.0000
  15.000   1.1397   0.08451   0.07618  -0.0338   0.0366   1.0000
  15.250   1.1486   0.08666   0.07834  -0.0340   0.0355   1.0000
  15.500   1.1597   0.08851   0.08022  -0.0339   0.0345   1.0000
  15.750   1.1716   0.09035   0.08222  -0.0338   0.0336   1.0000
  16.000   1.1832   0.09228   0.08427  -0.0338   0.0327   1.0000
  16.250   1.1933   0.09442   0.08652  -0.0340   0.0318   1.0000
  16.500   1.2026   0.09665   0.08884  -0.0343   0.0310   1.0000
  16.750   1.2128   0.09874   0.09095  -0.0347   0.0303   1.0000
  17.000   1.2216   0.10110   0.09341  -0.0350   0.0296   1.0000
  17.250   1.2240   0.10447   0.09704  -0.0358   0.0289   1.0000
  17.500   1.2260   0.10793   0.10073  -0.0368   0.0284   1.0000
  17.750   1.2268   0.11160   0.10462  -0.0379   0.0280   1.0000
  18.000   1.2262   0.11552   0.10875  -0.0393   0.0276   1.0000
  18.250   1.2234   0.11981   0.11326  -0.0409   0.0274   1.0000
  18.500   1.2185   0.12452   0.11818  -0.0430   0.0271   1.0000
  18.750   1.2113   0.12970   0.12358  -0.0455   0.0269   1.0000
  19.000   1.2014   0.13549   0.12960  -0.0486   0.0268   1.0000
  19.250   1.1879   0.14215   0.13650  -0.0524   0.0267   1.0000
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