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NACA 16-018 (naca16018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 16-018 (naca16018-il)
Reynolds number: 1,000,000
Max Cl/Cd: 40.47 at α=11°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca16018-il-1000000-n5.txt
Download as CSV file: xf-naca16018-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 16-018                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2109   0.05796   0.05341  -0.0964   0.9949   0.0092
 -19.500  -1.2101   0.05504   0.05039  -0.0971   0.9946   0.0094
 -19.250  -1.2072   0.05239   0.04766  -0.0976   0.9943   0.0096
 -19.000  -1.2027   0.04996   0.04515  -0.0981   0.9940   0.0098
 -18.750  -1.1987   0.04778   0.04288  -0.0980   0.9932   0.0101
 -18.500  -1.1938   0.04578   0.04080  -0.0977   0.9922   0.0104
 -18.250  -1.1872   0.04393   0.03887  -0.0974   0.9913   0.0106
 -18.000  -1.1796   0.04217   0.03703  -0.0972   0.9905   0.0108
 -17.750  -1.1719   0.04043   0.03522  -0.0969   0.9897   0.0112
 -17.500  -1.1626   0.03883   0.03356  -0.0967   0.9889   0.0116
 -17.250  -1.1518   0.03734   0.03202  -0.0965   0.9882   0.0121
 -17.000  -1.1396   0.03595   0.03058  -0.0964   0.9876   0.0125
 -16.750  -1.1266   0.03467   0.02924  -0.0963   0.9870   0.0129
 -16.500  -1.1127   0.03346   0.02796  -0.0962   0.9865   0.0134
 -16.250  -1.0980   0.03234   0.02677  -0.0962   0.9860   0.0138
 -16.000  -1.0834   0.03122   0.02562  -0.0960   0.9854   0.0144
 -15.750  -1.0675   0.03020   0.02456  -0.0959   0.9849   0.0150
 -15.500  -1.0505   0.02926   0.02358  -0.0959   0.9843   0.0157
 -15.250  -1.0346   0.02838   0.02266  -0.0955   0.9833   0.0164
 -15.000  -1.0216   0.02762   0.02185  -0.0943   0.9813   0.0170
 -14.750  -1.0066   0.02684   0.02102  -0.0935   0.9797   0.0175
 -14.500  -0.9907   0.02604   0.02020  -0.0929   0.9784   0.0183
 -14.250  -0.9729   0.02534   0.01947  -0.0925   0.9771   0.0190
 -14.000  -0.9547   0.02465   0.01875  -0.0922   0.9759   0.0198
 -13.750  -0.9363   0.02399   0.01805  -0.0918   0.9747   0.0204
 -13.500  -0.9169   0.02338   0.01740  -0.0916   0.9737   0.0210
 -13.250  -0.8974   0.02279   0.01675  -0.0913   0.9728   0.0216
 -13.000  -0.8835   0.02218   0.01613  -0.0898   0.9704   0.0224
 -12.750  -0.8672   0.02163   0.01555  -0.0887   0.9681   0.0231
 -12.500  -0.8491   0.02111   0.01501  -0.0879   0.9661   0.0238
 -12.250  -0.8305   0.02060   0.01447  -0.0872   0.9643   0.0245
 -12.000  -0.8113   0.02011   0.01394  -0.0866   0.9628   0.0251
 -11.750  -0.7912   0.01965   0.01344  -0.0861   0.9614   0.0257
 -11.500  -0.7713   0.01924   0.01298  -0.0855   0.9598   0.0261
 -11.250  -0.7552   0.01873   0.01246  -0.0842   0.9572   0.0270
 -11.000  -0.7376   0.01827   0.01198  -0.0831   0.9548   0.0279
 -10.750  -0.7188   0.01784   0.01153  -0.0822   0.9527   0.0287
 -10.500  -0.6990   0.01744   0.01111  -0.0814   0.9508   0.0296
 -10.250  -0.6785   0.01705   0.01069  -0.0808   0.9490   0.0304
 -10.000  -0.6575   0.01667   0.01028  -0.0802   0.9472   0.0311
  -9.750  -0.6378   0.01635   0.00993  -0.0794   0.9449   0.0316
  -9.500  -0.6189   0.01597   0.00953  -0.0783   0.9425   0.0329
  -9.250  -0.5990   0.01562   0.00917  -0.0775   0.9402   0.0341
  -9.000  -0.5786   0.01528   0.00882  -0.0767   0.9379   0.0355
  -8.750  -0.5575   0.01495   0.00848  -0.0760   0.9358   0.0369
  -8.500  -0.5357   0.01464   0.00814  -0.0755   0.9338   0.0380
  -8.250  -0.5149   0.01432   0.00782  -0.0747   0.9319   0.0406
  -8.000  -0.4945   0.01403   0.00754  -0.0739   0.9296   0.0435
  -7.750  -0.4735   0.01375   0.00727  -0.0731   0.9271   0.0469
  -7.500  -0.4530   0.01344   0.00698  -0.0722   0.9245   0.0527
  -7.250  -0.4324   0.01312   0.00669  -0.0713   0.9221   0.0608
  -7.000  -0.4115   0.01279   0.00640  -0.0706   0.9201   0.0708
  -6.750  -0.3897   0.01250   0.00613  -0.0699   0.9180   0.0806
  -6.500  -0.3691   0.01224   0.00591  -0.0690   0.9156   0.0912
  -6.250  -0.3486   0.01197   0.00569  -0.0680   0.9129   0.1038
  -6.000  -0.3283   0.01168   0.00547  -0.0670   0.9103   0.1190
  -5.750  -0.3082   0.01137   0.00523  -0.0660   0.9079   0.1374
  -5.500  -0.2879   0.01105   0.00498  -0.0650   0.9055   0.1586
  -5.250  -0.2676   0.01072   0.00473  -0.0640   0.9032   0.1840
  -5.000  -0.2507   0.01036   0.00452  -0.0623   0.9005   0.2198
  -4.750  -0.2346   0.00998   0.00430  -0.0604   0.8975   0.2607
  -4.500  -0.2213   0.00951   0.00404  -0.0579   0.8943   0.3130
  -4.250  -0.2110   0.00894   0.00372  -0.0548   0.8911   0.3792
  -4.000  -0.2025   0.00833   0.00338  -0.0512   0.8880   0.4518
  -3.750  -0.1985   0.00781   0.00312  -0.0465   0.8843   0.5135
  -3.500  -0.1949   0.00733   0.00285  -0.0416   0.8801   0.5701
  -3.250  -0.1975   0.00679   0.00255  -0.0352   0.8760   0.6325
  -3.000  -0.1906   0.00645   0.00234  -0.0308   0.8727   0.6742
  -2.750  -0.1831   0.00628   0.00227  -0.0264   0.8689   0.7026
  -2.500  -0.1747   0.00612   0.00220  -0.0221   0.8651   0.7288
  -2.250  -0.1624   0.00599   0.00214  -0.0187   0.8619   0.7516
  -2.000  -0.1473   0.00590   0.00210  -0.0159   0.8590   0.7727
  -1.750  -0.1401   0.00588   0.00214  -0.0113   0.8554   0.7906
  -1.500  -0.1323   0.00590   0.00220  -0.0067   0.8514   0.8037
  -1.250  -0.1197   0.00589   0.00217  -0.0033   0.8478   0.8127
  -1.000  -0.0898   0.00589   0.00219  -0.0040   0.8457   0.8177
  -0.750  -0.0644   0.00588   0.00216  -0.0037   0.8433   0.8229
  -0.500  -0.0520   0.00588   0.00216  -0.0003   0.8397   0.8279
  -0.250  -0.0253   0.00589   0.00219  -0.0003   0.8367   0.8307
   0.000   0.0000   0.00589   0.00221   0.0000   0.8336   0.8336
   0.250   0.0253   0.00589   0.00219   0.0003   0.8307   0.8367
   0.500   0.0520   0.00588   0.00216   0.0003   0.8279   0.8397
   0.750   0.0644   0.00588   0.00216   0.0037   0.8229   0.8433
   1.000   0.0899   0.00589   0.00219   0.0040   0.8177   0.8457
   1.250   0.1198   0.00589   0.00217   0.0033   0.8127   0.8479
   1.500   0.1324   0.00590   0.00220   0.0067   0.8037   0.8514
   1.750   0.1402   0.00588   0.00214   0.0112   0.7906   0.8554
   2.000   0.1474   0.00590   0.00210   0.0159   0.7727   0.8590
   2.250   0.1626   0.00599   0.00214   0.0187   0.7517   0.8619
   2.500   0.1750   0.00611   0.00220   0.0220   0.7291   0.8651
   2.750   0.1838   0.00627   0.00227   0.0262   0.7032   0.8689
   3.000   0.1921   0.00644   0.00234   0.0304   0.6762   0.8727
   3.250   0.1963   0.00681   0.00255   0.0355   0.6295   0.8760
   3.500   0.1951   0.00733   0.00285   0.0416   0.5700   0.8801
   3.750   0.1981   0.00783   0.00312   0.0466   0.5118   0.8843
   4.000   0.2028   0.00833   0.00338   0.0511   0.4521   0.8880
   4.250   0.2116   0.00893   0.00372   0.0546   0.3804   0.8910
   4.500   0.2216   0.00951   0.00404   0.0578   0.3128   0.8943
   4.750   0.2352   0.00997   0.00430   0.0602   0.2615   0.8975
   5.000   0.2511   0.01036   0.00452   0.0622   0.2198   0.9004
   5.250   0.2680   0.01072   0.00473   0.0639   0.1838   0.9031
   5.500   0.2884   0.01105   0.00498   0.0649   0.1585   0.9055
   5.750   0.3087   0.01137   0.00523   0.0659   0.1372   0.9079
   6.250   0.3492   0.01196   0.00569   0.0679   0.1037   0.9129
   6.500   0.3697   0.01223   0.00591   0.0689   0.0911   0.9156
   6.750   0.3904   0.01249   0.00612   0.0698   0.0806   0.9180
   7.000   0.4122   0.01279   0.00639   0.0704   0.0708   0.9200
   7.250   0.4331   0.01311   0.00669   0.0712   0.0607   0.9221
   7.500   0.4538   0.01344   0.00698   0.0720   0.0527   0.9244
   7.750   0.4743   0.01375   0.00726   0.0729   0.0468   0.9270
   8.000   0.4954   0.01402   0.00753   0.0737   0.0435   0.9295
   8.250   0.5158   0.01431   0.00781   0.0745   0.0406   0.9319
   8.500   0.5367   0.01463   0.00813   0.0752   0.0381   0.9338
   8.750   0.5585   0.01494   0.00847   0.0758   0.0369   0.9358
   9.000   0.5797   0.01527   0.00881   0.0765   0.0355   0.9379
   9.250   0.6001   0.01561   0.00917   0.0772   0.0342   0.9402
   9.500   0.6200   0.01596   0.00952   0.0781   0.0330   0.9425
   9.750   0.6390   0.01634   0.00992   0.0791   0.0316   0.9449
  10.000   0.6587   0.01667   0.01027   0.0800   0.0311   0.9472
  10.250   0.6797   0.01704   0.01068   0.0805   0.0304   0.9489
  10.500   0.7003   0.01743   0.01110   0.0812   0.0295   0.9507
  10.750   0.7201   0.01783   0.01152   0.0819   0.0287   0.9526
  11.000   0.7390   0.01826   0.01196   0.0828   0.0279   0.9547
  11.250   0.7566   0.01872   0.01245   0.0839   0.0269   0.9572
  11.500   0.7729   0.01922   0.01297   0.0852   0.0261   0.9597
  11.750   0.7927   0.01964   0.01343   0.0858   0.0257   0.9614
  12.000   0.8129   0.02010   0.01393   0.0863   0.0252   0.9628
  12.250   0.8322   0.02059   0.01445   0.0869   0.0245   0.9644
  12.500   0.8509   0.02109   0.01499   0.0876   0.0237   0.9661
  12.750   0.8689   0.02161   0.01553   0.0884   0.0230   0.9682
  13.000   0.8854   0.02216   0.01610   0.0894   0.0223   0.9704
  13.250   0.8992   0.02277   0.01674   0.0909   0.0215   0.9728
  13.500   0.9190   0.02336   0.01737   0.0912   0.0210   0.9738
  13.750   0.9383   0.02396   0.01802   0.0915   0.0204   0.9748
  14.000   0.9569   0.02462   0.01872   0.0918   0.0197   0.9759
  14.250   0.9751   0.02531   0.01944   0.0921   0.0190   0.9772
  14.500   0.9929   0.02601   0.02017   0.0925   0.0183   0.9785
  14.750   1.0088   0.02680   0.02098   0.0931   0.0175   0.9799
  15.000   1.0238   0.02757   0.02180   0.0939   0.0169   0.9815
  15.250   1.0366   0.02833   0.02261   0.0952   0.0164   0.9836
  15.500   1.0531   0.02922   0.02354   0.0954   0.0157   0.9844
  15.750   1.0702   0.03016   0.02451   0.0954   0.0150   0.9850
  16.000   1.0862   0.03118   0.02556   0.0955   0.0143   0.9855
  16.250   1.1009   0.03229   0.02672   0.0956   0.0137   0.9861
  16.500   1.1158   0.03341   0.02791   0.0957   0.0134   0.9866
  16.750   1.1297   0.03462   0.02918   0.0958   0.0129   0.9871
  17.000   1.1429   0.03590   0.03052   0.0959   0.0125   0.9877
  17.250   1.1551   0.03728   0.03195   0.0960   0.0120   0.9884
  17.500   1.1659   0.03876   0.03349   0.0961   0.0115   0.9891
  17.750   1.1752   0.04037   0.03515   0.0964   0.0112   0.9899
  18.000   1.1830   0.04209   0.03695   0.0967   0.0108   0.9907
  18.250   1.1908   0.04383   0.03877   0.0969   0.0106   0.9916
  18.500   1.1973   0.04567   0.04070   0.0972   0.0103   0.9925
  18.750   1.2022   0.04766   0.04276   0.0975   0.0100   0.9935
  19.000   1.2071   0.04986   0.04505   0.0974   0.0098   0.9941
  19.250   1.2115   0.05229   0.04756   0.0969   0.0095   0.9944
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