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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 100,000
Max Cl/Cd: 40.72 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633018-il-100000.txt
Download as CSV file: xf-naca633018-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-018                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.6636   0.17610   0.17090   0.0163   1.0000   0.1678
 -15.750  -0.9043   0.10105   0.09567  -0.0239   1.0000   0.0958
 -15.500  -0.9445   0.09156   0.08601  -0.0285   1.0000   0.0951
 -15.250  -0.9834   0.08350   0.07774  -0.0320   1.0000   0.0946
 -15.000  -1.0178   0.07683   0.07083  -0.0343   1.0000   0.0943
 -14.750  -1.0481   0.07126   0.06502  -0.0356   1.0000   0.0943
 -14.500  -1.0740   0.06659   0.06008  -0.0360   1.0000   0.0945
 -14.250  -1.0969   0.06260   0.05581  -0.0357   1.0000   0.0949
 -14.000  -1.1165   0.05922   0.05215  -0.0348   1.0000   0.0954
 -13.750  -1.1331   0.05639   0.04902  -0.0332   1.0000   0.0959
 -13.500  -1.1148   0.05286   0.04545  -0.0336   1.0000   0.0983
 -13.250  -1.1034   0.05073   0.04327  -0.0332   1.0000   0.1007
 -13.000  -1.0954   0.04863   0.04103  -0.0325   1.0000   0.1030
 -12.750  -1.0891   0.04645   0.03865  -0.0315   1.0000   0.1049
 -12.500  -1.0830   0.04442   0.03635  -0.0303   1.0000   0.1069
 -12.250  -1.0795   0.04265   0.03431  -0.0288   1.0000   0.1088
 -12.000  -1.0411   0.04037   0.03209  -0.0302   1.0000   0.1130
 -11.750  -1.0151   0.03885   0.03055  -0.0304   1.0000   0.1167
 -11.500  -0.9945   0.03735   0.02890  -0.0301   1.0000   0.1206
 -11.250  -0.9675   0.03583   0.02730  -0.0302   1.0000   0.1254
 -11.000  -0.9384   0.03466   0.02627  -0.0304   1.0000   0.1317
 -10.750  -0.9199   0.03341   0.02487  -0.0299   1.0000   0.1377
 -10.500  -0.8889   0.03232   0.02406  -0.0300   1.0000   0.1466
 -10.250  -0.8693   0.03113   0.02297  -0.0294   1.0000   0.1571
 -10.000  -0.8552   0.02982   0.02183  -0.0286   1.0000   0.1708
  -9.750  -0.8464   0.02833   0.02060  -0.0274   1.0000   0.1881
  -9.500  -0.8453   0.02663   0.01915  -0.0258   1.0000   0.2123
  -9.250  -0.8535   0.02491   0.01782  -0.0232   1.0000   0.2410
  -9.000  -0.8771   0.02410   0.01723  -0.0173   1.0000   0.2606
  -8.750  -0.9132   0.02406   0.01726  -0.0085   1.0000   0.2647
  -8.500  -0.9299   0.02315   0.01666  -0.0036   0.9956   0.2997
  -8.250  -0.9051   0.02224   0.01620  -0.0054   0.9824   0.3818
  -8.000  -0.8704   0.02236   0.01632  -0.0076   0.9717   0.4299
  -7.750  -0.8293   0.02285   0.01674  -0.0102   0.9634   0.4616
  -7.500  -0.7832   0.02359   0.01741  -0.0132   0.9560   0.4856
  -7.250  -0.7376   0.02459   0.01835  -0.0155   0.9486   0.5043
  -7.000  -0.6896   0.02581   0.01953  -0.0177   0.9415   0.5210
  -6.750  -0.6368   0.02766   0.02135  -0.0196   0.9354   0.5365
  -6.500  -0.5912   0.02921   0.02285  -0.0206   0.9273   0.5497
  -6.250  -0.5659   0.02949   0.02300  -0.0203   0.9173   0.5629
  -6.000  -0.4985   0.03187   0.02536  -0.0226   0.9122   0.5664
  -5.750  -0.4616   0.03277   0.02617  -0.0227   0.9039   0.5749
  -5.500  -0.4282   0.03345   0.02677  -0.0223   0.8949   0.5822
  -5.250  -0.4171   0.03315   0.02639  -0.0204   0.8841   0.5934
  -5.000  -0.3765   0.03406   0.02722  -0.0203   0.8771   0.5981
  -4.750  -0.3810   0.03297   0.02604  -0.0175   0.8654   0.6110
  -4.500  -0.3378   0.03388   0.02689  -0.0176   0.8598   0.6139
  -4.250  -0.2999   0.03467   0.02764  -0.0177   0.8512   0.6176
  -4.000  -0.3054   0.03330   0.02616  -0.0147   0.8427   0.6296
  -3.750  -0.2693   0.03394   0.02679  -0.0149   0.8343   0.6330
  -3.500  -0.2745   0.03256   0.02529  -0.0120   0.8270   0.6452
  -3.250  -0.2398   0.03316   0.02589  -0.0122   0.8185   0.6482
  -3.000  -0.2121   0.03324   0.02591  -0.0115   0.8123   0.6534
  -2.750  -0.2106   0.03236   0.02499  -0.0096   0.8034   0.6632
  -2.500  -0.1792   0.03261   0.02520  -0.0093   0.7975   0.6672
  -2.250  -0.1809   0.03159   0.02411  -0.0072   0.7895   0.6782
  -2.000  -0.1499   0.03189   0.02441  -0.0069   0.7827   0.6814
  -1.750  -0.1239   0.03180   0.02426  -0.0061   0.7781   0.6867
  -1.500  -0.1203   0.03129   0.02373  -0.0048   0.7689   0.6958
  -1.250  -0.0908   0.03139   0.02382  -0.0043   0.7637   0.6997
  -1.000  -0.0779   0.03113   0.02352  -0.0032   0.7568   0.7077
  -0.750  -0.0602   0.03103   0.02341  -0.0024   0.7497   0.7135
  -0.500  -0.0318   0.03099   0.02336  -0.0018   0.7456   0.7181
  -0.250  -0.0279   0.03077   0.02312  -0.0005   0.7368   0.7279
   0.000   0.0000   0.03092   0.02329   0.0000   0.7314   0.7314
   0.250   0.0279   0.03077   0.02312   0.0005   0.7279   0.7368
   0.500   0.0317   0.03099   0.02336   0.0018   0.7181   0.7456
   0.750   0.0602   0.03103   0.02341   0.0024   0.7135   0.7497
   1.000   0.0779   0.03113   0.02352   0.0032   0.7077   0.7568
   1.250   0.0907   0.03139   0.02382   0.0043   0.6997   0.7637
   1.500   0.1203   0.03129   0.02373   0.0048   0.6958   0.7689
   1.750   0.1240   0.03179   0.02425   0.0061   0.6867   0.7781
   2.000   0.1498   0.03191   0.02442   0.0069   0.6814   0.7827
   2.250   0.1810   0.03159   0.02410   0.0072   0.6782   0.7895
   2.500   0.1792   0.03261   0.02520   0.0093   0.6672   0.7975
   2.750   0.2106   0.03236   0.02498   0.0096   0.6632   0.8034
   3.000   0.2121   0.03324   0.02591   0.0115   0.6534   0.8123
   3.250   0.2399   0.03316   0.02588   0.0122   0.6482   0.8185
   3.500   0.2743   0.03258   0.02530   0.0120   0.6452   0.8270
   3.750   0.2692   0.03395   0.02679   0.0149   0.6330   0.8343
   4.000   0.3054   0.03330   0.02617   0.0147   0.6296   0.8426
   4.250   0.2999   0.03466   0.02764   0.0177   0.6176   0.8512
   4.500   0.3376   0.03389   0.02690   0.0176   0.6139   0.8598
   4.750   0.3812   0.03295   0.02602   0.0175   0.6110   0.8654
   5.000   0.3764   0.03407   0.02723   0.0203   0.5981   0.8771
   5.250   0.4173   0.03314   0.02637   0.0203   0.5934   0.8840
   5.500   0.4282   0.03345   0.02677   0.0222   0.5822   0.8949
   5.750   0.4905   0.03132   0.02469   0.0207   0.5796   0.9005
   6.000   0.4982   0.03189   0.02538   0.0226   0.5664   0.9123
   6.250   0.5657   0.02949   0.02301   0.0203   0.5629   0.9173
   6.500   0.5911   0.02922   0.02287   0.0206   0.5498   0.9274
   6.750   0.6367   0.02766   0.02135   0.0196   0.5365   0.9355
   7.000   0.6895   0.02583   0.01955   0.0177   0.5211   0.9416
   7.250   0.7376   0.02458   0.01834   0.0155   0.5043   0.9487
   7.500   0.7834   0.02357   0.01738   0.0132   0.4855   0.9560
   7.750   0.8292   0.02285   0.01673   0.0102   0.4615   0.9634
   8.000   0.8706   0.02235   0.01631   0.0076   0.4300   0.9718
   8.250   0.9052   0.02223   0.01619   0.0054   0.3818   0.9824
   8.500   0.9301   0.02314   0.01665   0.0036   0.2999   0.9956
   8.750   0.9131   0.02405   0.01725   0.0085   0.2647   1.0000
   9.000   0.8774   0.02410   0.01723   0.0173   0.2607   1.0000
   9.250   0.8537   0.02491   0.01781   0.0231   0.2409   1.0000
   9.500   0.8457   0.02662   0.01914   0.0257   0.2124   1.0000
   9.750   0.8470   0.02831   0.02058   0.0273   0.1882   1.0000
  10.000   0.8556   0.02981   0.02182   0.0285   0.1707   1.0000
  10.250   0.8699   0.03111   0.02296   0.0293   0.1571   1.0000
  10.500   0.8893   0.03231   0.02405   0.0299   0.1466   1.0000
  10.750   0.9205   0.03340   0.02487   0.0298   0.1377   1.0000
  11.000   0.9387   0.03465   0.02627   0.0304   0.1316   1.0000
  11.250   0.9682   0.03582   0.02729   0.0301   0.1254   1.0000
  11.500   0.9949   0.03734   0.02890   0.0300   0.1205   1.0000
  11.750   1.0156   0.03885   0.03055   0.0303   0.1167   1.0000
  12.000   1.0417   0.04037   0.03209   0.0301   0.1129   1.0000
  12.250   1.0791   0.04262   0.03428   0.0288   0.1088   1.0000
  12.500   1.0833   0.04440   0.03635   0.0303   0.1069   1.0000
  12.750   1.0894   0.04646   0.03865   0.0314   0.1048   1.0000
  13.000   1.0960   0.04862   0.04101   0.0324   0.1029   1.0000
  13.250   1.1041   0.05075   0.04328   0.0331   0.1007   1.0000
  13.500   1.1155   0.05287   0.04546   0.0335   0.0983   1.0000
  13.750   1.1338   0.05638   0.04902   0.0331   0.0959   1.0000
  14.000   1.1170   0.05924   0.05217   0.0347   0.0953   1.0000
  14.250   1.0969   0.06261   0.05583   0.0356   0.0948   1.0000
  14.500   1.0745   0.06659   0.06008   0.0359   0.0945   1.0000
  14.750   1.0482   0.07128   0.06504   0.0355   0.0942   1.0000
  15.000   1.0183   0.07685   0.07086   0.0342   0.0943   1.0000
  15.250   0.9833   0.08356   0.07780   0.0319   0.0945   1.0000
  15.500   0.9448   0.09160   0.08605   0.0284   0.0951   1.0000
  15.750   0.9055   0.10103   0.09565   0.0238   0.0958   1.0000
  16.000   0.6649   0.17621   0.17100  -0.0164   0.1677   1.0000
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