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NACA 16-012 (naca16012-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 16-012 (naca16012-il)
Reynolds number: 500,000
Max Cl/Cd: 44.51 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca16012-il-500000-n5.txt
Download as CSV file: xf-naca16012-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 16-012                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9003   0.06613   0.06331  -0.0621   1.0000   0.0047
 -14.500  -0.9255   0.05930   0.05630  -0.0649   1.0000   0.0047
 -14.250  -0.9497   0.05397   0.05079  -0.0652   1.0000   0.0047
 -14.000  -0.9711   0.04980   0.04643  -0.0639   1.0000   0.0047
 -13.750  -0.9924   0.04621   0.04265  -0.0613   1.0000   0.0047
 -13.500  -1.0114   0.04324   0.03949  -0.0578   1.0000   0.0048
 -13.250  -1.0281   0.04075   0.03683  -0.0536   1.0000   0.0048
 -13.000  -1.0423   0.03868   0.03459  -0.0490   1.0000   0.0049
 -12.750  -1.0542   0.03694   0.03270  -0.0441   1.0000   0.0049
 -12.500  -1.0644   0.03543   0.03102  -0.0391   1.0000   0.0050
 -12.250  -1.0660   0.03393   0.02937  -0.0356   0.9994   0.0051
 -12.000  -1.0568   0.03231   0.02757  -0.0341   0.9980   0.0052
 -11.750  -1.0459   0.03085   0.02594  -0.0326   0.9965   0.0053
 -11.500  -1.0328   0.02947   0.02437  -0.0314   0.9952   0.0055
 -11.250  -1.0190   0.02814   0.02287  -0.0300   0.9937   0.0057
 -11.000  -1.0047   0.02688   0.02142  -0.0286   0.9916   0.0059
 -10.750  -0.9882   0.02571   0.02008  -0.0275   0.9899   0.0061
 -10.500  -0.9693   0.02465   0.01885  -0.0267   0.9884   0.0064
 -10.250  -0.9479   0.02369   0.01772  -0.0263   0.9872   0.0067
 -10.000  -0.9265   0.02253   0.01637  -0.0260   0.9862   0.0070
  -9.750  -0.9091   0.02153   0.01526  -0.0247   0.9840   0.0075
  -9.500  -0.8900   0.02081   0.01445  -0.0237   0.9817   0.0079
  -9.250  -0.8680   0.02010   0.01365  -0.0232   0.9800   0.0083
  -9.000  -0.8440   0.01939   0.01284  -0.0231   0.9787   0.0088
  -8.750  -0.8188   0.01868   0.01203  -0.0232   0.9776   0.0094
  -8.500  -0.7926   0.01804   0.01127  -0.0235   0.9767   0.0099
  -8.250  -0.7672   0.01726   0.01044  -0.0237   0.9759   0.0112
  -8.000  -0.7513   0.01689   0.01002  -0.0216   0.9720   0.0123
  -7.750  -0.7274   0.01645   0.00954  -0.0212   0.9699   0.0135
  -7.500  -0.7015   0.01598   0.00900  -0.0213   0.9684   0.0148
  -7.250  -0.6755   0.01545   0.00846  -0.0215   0.9672   0.0173
  -7.000  -0.6470   0.01512   0.00812  -0.0222   0.9663   0.0203
  -6.750  -0.6176   0.01484   0.00778  -0.0230   0.9655   0.0225
  -6.500  -0.5899   0.01436   0.00725  -0.0235   0.9646   0.0253
  -6.250  -0.5740   0.01414   0.00702  -0.0212   0.9603   0.0277
  -6.000  -0.5502   0.01388   0.00673  -0.0207   0.9579   0.0301
  -5.750  -0.5237   0.01361   0.00641  -0.0208   0.9561   0.0318
  -5.500  -0.4970   0.01327   0.00602  -0.0209   0.9546   0.0340
  -5.250  -0.4702   0.01290   0.00564  -0.0211   0.9534   0.0375
  -5.000  -0.4423   0.01260   0.00532  -0.0215   0.9523   0.0410
  -4.750  -0.4155   0.01233   0.00503  -0.0216   0.9508   0.0447
  -4.500  -0.4008   0.01215   0.00486  -0.0189   0.9458   0.0504
  -4.250  -0.3769   0.01187   0.00462  -0.0184   0.9433   0.0622
  -4.000  -0.3519   0.01153   0.00437  -0.0182   0.9414   0.0865
  -3.750  -0.3267   0.01114   0.00411  -0.0180   0.9397   0.1232
  -3.500  -0.3016   0.01069   0.00386  -0.0178   0.9383   0.1738
  -3.250  -0.2848   0.01028   0.00368  -0.0158   0.9347   0.2367
  -3.000  -0.2706   0.00981   0.00350  -0.0132   0.9302   0.3134
  -2.750  -0.2560   0.00911   0.00324  -0.0108   0.9270   0.4246
  -2.500  -0.2474   0.00817   0.00289  -0.0070   0.9241   0.5730
  -2.250  -0.2466   0.00757   0.00279  -0.0010   0.9184   0.6908
  -2.000  -0.2296   0.00729   0.00281   0.0015   0.9148   0.7635
  -1.750  -0.2026   0.00719   0.00286   0.0018   0.9129   0.8100
  -1.500  -0.1721   0.00730   0.00311   0.0015   0.9115   0.8558
  -1.250  -0.1412   0.00746   0.00331   0.0011   0.9101   0.8765
  -1.000  -0.1102   0.00748   0.00330   0.0003   0.9087   0.8826
  -0.750  -0.0843   0.00757   0.00340   0.0006   0.9051   0.8869
  -0.500  -0.0609   0.00758   0.00339   0.0015   0.9014   0.8917
  -0.250  -0.0334   0.00754   0.00334   0.0014   0.8987   0.8952
   0.000   0.0000   0.00755   0.00334   0.0000   0.8969   0.8969
   0.250   0.0334   0.00754   0.00334  -0.0014   0.8952   0.8987
   0.500   0.0609   0.00758   0.00339  -0.0015   0.8918   0.9014
   0.750   0.0843   0.00757   0.00340  -0.0006   0.8869   0.9051
   1.000   0.1102   0.00748   0.00330  -0.0003   0.8826   0.9087
   1.250   0.1412   0.00746   0.00331  -0.0011   0.8765   0.9101
   1.500   0.1720   0.00730   0.00311  -0.0015   0.8560   0.9115
   1.750   0.2026   0.00719   0.00286  -0.0017   0.8098   0.9129
   2.000   0.2296   0.00728   0.00281  -0.0015   0.7640   0.9148
   2.250   0.2463   0.00757   0.00279   0.0011   0.6892   0.9185
   2.500   0.2472   0.00818   0.00289   0.0071   0.5713   0.9241
   2.750   0.2560   0.00911   0.00324   0.0108   0.4246   0.9270
   3.000   0.2707   0.00981   0.00350   0.0132   0.3136   0.9302
   3.250   0.2848   0.01028   0.00368   0.0158   0.2363   0.9347
   3.500   0.3017   0.01069   0.00385   0.0178   0.1742   0.9383
   3.750   0.3267   0.01114   0.00411   0.0180   0.1229   0.9397
   4.000   0.3519   0.01153   0.00436   0.0182   0.0866   0.9414
   4.250   0.3769   0.01187   0.00461   0.0184   0.0620   0.9433
   4.500   0.4009   0.01215   0.00486   0.0189   0.0504   0.9458
   4.750   0.4159   0.01233   0.00503   0.0215   0.0447   0.9508
   5.000   0.4423   0.01259   0.00532   0.0215   0.0410   0.9523
   5.250   0.4702   0.01290   0.00564   0.0211   0.0376   0.9534
   5.500   0.4971   0.01327   0.00602   0.0209   0.0340   0.9546
   5.750   0.5238   0.01361   0.00641   0.0208   0.0318   0.9561
   6.000   0.5503   0.01388   0.00672   0.0207   0.0301   0.9579
   6.250   0.5740   0.01414   0.00702   0.0212   0.0277   0.9604
   6.500   0.5900   0.01436   0.00725   0.0234   0.0252   0.9646
   6.750   0.6177   0.01484   0.00778   0.0230   0.0226   0.9655
   7.000   0.6470   0.01512   0.00812   0.0222   0.0203   0.9663
   7.250   0.6756   0.01545   0.00845   0.0215   0.0172   0.9673
   7.500   0.7016   0.01598   0.00900   0.0213   0.0148   0.9685
   7.750   0.7275   0.01644   0.00953   0.0212   0.0136   0.9700
   8.000   0.7514   0.01688   0.01002   0.0215   0.0123   0.9721
   8.250   0.7675   0.01726   0.01044   0.0236   0.0112   0.9759
   8.500   0.7929   0.01804   0.01128   0.0234   0.0099   0.9767
   8.750   0.8191   0.01868   0.01203   0.0231   0.0094   0.9776
   9.000   0.8443   0.01938   0.01283   0.0230   0.0088   0.9787
   9.250   0.8683   0.02010   0.01365   0.0231   0.0083   0.9801
   9.500   0.8904   0.02081   0.01445   0.0236   0.0079   0.9818
   9.750   0.9095   0.02154   0.01526   0.0246   0.0075   0.9841
  10.000   0.9270   0.02252   0.01636   0.0259   0.0071   0.9862
  10.250   0.9484   0.02369   0.01772   0.0262   0.0067   0.9872
  10.500   0.9699   0.02465   0.01885   0.0266   0.0064   0.9884
  10.750   0.9890   0.02568   0.02005   0.0273   0.0061   0.9899
  11.000   1.0054   0.02690   0.02144   0.0284   0.0059   0.9917
  11.250   1.0199   0.02814   0.02287   0.0299   0.0056   0.9938
  11.500   1.0338   0.02946   0.02437   0.0312   0.0055   0.9953
  11.750   1.0468   0.03085   0.02594   0.0324   0.0053   0.9966
  12.000   1.0576   0.03232   0.02759   0.0339   0.0052   0.9980
  12.250   1.0666   0.03396   0.02940   0.0354   0.0051   0.9995
  12.500   1.0641   0.03546   0.03106   0.0392   0.0050   1.0000
  12.750   1.0544   0.03693   0.03269   0.0441   0.0049   1.0000
  13.000   1.0424   0.03868   0.03459   0.0490   0.0049   1.0000
  13.250   1.0284   0.04073   0.03681   0.0536   0.0048   1.0000
  13.500   1.0116   0.04323   0.03949   0.0578   0.0048   1.0000
  13.750   0.9928   0.04620   0.04264   0.0613   0.0047   1.0000
  14.000   0.9720   0.04976   0.04639   0.0639   0.0047   1.0000
  14.250   0.9500   0.05401   0.05083   0.0651   0.0047   1.0000
  14.500   0.9263   0.05930   0.05630   0.0647   0.0047   1.0000
  14.750   0.9010   0.06619   0.06338   0.0619   0.0047   1.0000
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