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NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-415 AIRFOIL (n63415-il)
Reynolds number: 100,000
Max Cl/Cd: 52.33 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63415-il-100000-n5.txt
Download as CSV file: xf-n63415-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-415 AIRFOIL                             
  
 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  -0.5886   0.08097   0.07539  -0.0602   1.0000   0.0375
 -12.500  -0.6408   0.06938   0.06356  -0.0684   1.0000   0.0367
 -12.250  -0.6757   0.06224   0.05619  -0.0725   1.0000   0.0362
 -12.000  -0.6959   0.05773   0.05149  -0.0743   1.0000   0.0364
 -11.750  -0.7103   0.05431   0.04792  -0.0749   1.0000   0.0368
 -11.500  -0.7250   0.05121   0.04464  -0.0746   1.0000   0.0372
 -11.250  -0.7391   0.04862   0.04189  -0.0731   1.0000   0.0375
 -11.000  -0.7535   0.04652   0.03964  -0.0704   1.0000   0.0379
 -10.750  -0.7635   0.04445   0.03737  -0.0676   1.0000   0.0384
 -10.500  -0.7711   0.04255   0.03528  -0.0645   1.0000   0.0388
 -10.250  -0.7788   0.04094   0.03347  -0.0609   1.0000   0.0393
 -10.000  -0.7773   0.03901   0.03123  -0.0588   0.9972   0.0400
  -9.750  -0.7503   0.03684   0.02887  -0.0610   0.9886   0.0415
  -9.500  -0.7211   0.03527   0.02720  -0.0632   0.9809   0.0434
  -9.250  -0.6912   0.03348   0.02518  -0.0651   0.9736   0.0454
  -9.000  -0.6615   0.03172   0.02311  -0.0666   0.9660   0.0474
  -8.750  -0.6290   0.03018   0.02152  -0.0685   0.9602   0.0496
  -8.500  -0.5993   0.02902   0.02031  -0.0700   0.9524   0.0523
  -8.250  -0.5670   0.02778   0.01891  -0.0715   0.9458   0.0552
  -8.000  -0.5384   0.02664   0.01772  -0.0724   0.9379   0.0580
  -7.750  -0.5088   0.02565   0.01672  -0.0736   0.9303   0.0618
  -7.500  -0.4809   0.02476   0.01572  -0.0742   0.9221   0.0655
  -7.250  -0.4545   0.02381   0.01478  -0.0748   0.9139   0.0697
  -7.000  -0.4294   0.02305   0.01397  -0.0749   0.9052   0.0748
  -6.750  -0.4046   0.02222   0.01310  -0.0751   0.8968   0.0804
  -6.500  -0.3815   0.02155   0.01237  -0.0749   0.8879   0.0886
  -6.250  -0.3572   0.02075   0.01160  -0.0750   0.8799   0.0998
  -6.000  -0.3349   0.02003   0.01091  -0.0746   0.8710   0.1176
  -5.750  -0.3116   0.01914   0.01020  -0.0747   0.8633   0.1519
  -5.500  -0.2906   0.01820   0.00955  -0.0745   0.8549   0.2125
  -5.250  -0.2688   0.01722   0.00904  -0.0744   0.8471   0.3084
  -5.000  -0.2453   0.01675   0.00894  -0.0740   0.8397   0.3970
  -4.750  -0.2199   0.01663   0.00890  -0.0735   0.8320   0.4532
  -4.500  -0.1921   0.01662   0.00890  -0.0732   0.8262   0.4940
  -4.250  -0.1673   0.01673   0.00900  -0.0725   0.8177   0.5248
  -4.000  -0.1399   0.01684   0.00904  -0.0720   0.8115   0.5501
  -3.750  -0.1137   0.01695   0.00907  -0.0714   0.8042   0.5695
  -3.500  -0.0873   0.01705   0.00910  -0.0708   0.7972   0.5854
  -3.250  -0.0596   0.01714   0.00911  -0.0703   0.7918   0.5998
  -3.000  -0.0344   0.01723   0.00916  -0.0697   0.7837   0.6116
  -2.750  -0.0060   0.01717   0.00895  -0.0698   0.7777   0.6225
  -2.500   0.0202   0.01721   0.00897  -0.0692   0.7711   0.6295
  -2.250   0.0477   0.01717   0.00883  -0.0692   0.7641   0.6390
  -2.000   0.0755   0.01715   0.00874  -0.0688   0.7590   0.6456
  -1.750   0.1017   0.01718   0.00872  -0.0687   0.7514   0.6539
  -1.500   0.1291   0.01716   0.00864  -0.0685   0.7453   0.6608
  -1.250   0.1568   0.01715   0.00857  -0.0683   0.7398   0.6679
  -1.000   0.1836   0.01716   0.00854  -0.0684   0.7324   0.6757
  -0.750   0.2109   0.01716   0.00851  -0.0680   0.7270   0.6817
  -0.500   0.2384   0.01717   0.00848  -0.0681   0.7207   0.6895
  -0.250   0.2647   0.01721   0.00852  -0.0678   0.7141   0.6958
   0.000   0.2929   0.01720   0.00846  -0.0677   0.7091   0.7027
   0.250   0.3196   0.01727   0.00853  -0.0677   0.7024   0.7104
   0.500   0.3457   0.01731   0.00859  -0.0672   0.6962   0.7166
   0.750   0.3752   0.01730   0.00852  -0.0675   0.6916   0.7248
   1.000   0.3995   0.01743   0.00873  -0.0669   0.6844   0.7311
   1.250   0.4267   0.01748   0.00877  -0.0668   0.6786   0.7388
   1.500   0.4545   0.01750   0.00879  -0.0667   0.6738   0.7460
   1.750   0.4787   0.01766   0.00902  -0.0661   0.6666   0.7534
   2.000   0.5063   0.01771   0.00908  -0.0661   0.6612   0.7615
   2.250   0.5322   0.01779   0.00921  -0.0656   0.6557   0.7686
   2.500   0.5579   0.01794   0.00943  -0.0654   0.6487   0.7774
   2.750   0.5841   0.01798   0.00950  -0.0649   0.6435   0.7845
   3.000   0.6101   0.01814   0.00973  -0.0647   0.6369   0.7938
   3.250   0.6340   0.01825   0.00993  -0.0639   0.6303   0.8014
   3.500   0.6630   0.01827   0.00995  -0.0639   0.6253   0.8108
   3.750   0.6843   0.01849   0.01032  -0.0628   0.6173   0.8193
   4.000   0.7110   0.01855   0.01043  -0.0625   0.6112   0.8289
   4.250   0.7347   0.01869   0.01066  -0.0617   0.6043   0.8385
   4.500   0.7583   0.01880   0.01089  -0.0609   0.5969   0.8483
   4.750   0.7845   0.01884   0.01099  -0.0604   0.5903   0.8594
   5.000   0.8051   0.01896   0.01124  -0.0591   0.5812   0.8703
   5.250   0.8285   0.01894   0.01131  -0.0580   0.5724   0.8820
   5.500   0.8509   0.01891   0.01136  -0.0567   0.5618   0.8953
   5.750   0.8712   0.01894   0.01152  -0.0553   0.5502   0.9106
   6.000   0.8944   0.01889   0.01157  -0.0542   0.5388   0.9280
   6.250   0.9208   0.01882   0.01157  -0.0539   0.5255   0.9496
   6.500   0.9516   0.01882   0.01168  -0.0547   0.5083   1.0000
   6.750   0.9757   0.01900   0.01193  -0.0545   0.4887   1.0000
   7.000   0.9987   0.01915   0.01206  -0.0540   0.4635   1.0000
   7.250   1.0184   0.01946   0.01232  -0.0530   0.4325   1.0000
   7.500   1.0360   0.01991   0.01267  -0.0518   0.3956   1.0000
   7.750   1.0507   0.02055   0.01314  -0.0502   0.3525   1.0000
   8.000   1.0605   0.02147   0.01380  -0.0481   0.3060   1.0000
   8.250   1.0648   0.02263   0.01469  -0.0453   0.2614   1.0000
   8.500   1.0664   0.02402   0.01583  -0.0425   0.2214   1.0000
   8.750   1.0680   0.02558   0.01718  -0.0401   0.1867   1.0000
   9.000   1.0701   0.02724   0.01868  -0.0381   0.1574   1.0000
   9.250   1.0726   0.02898   0.02029  -0.0363   0.1332   1.0000
   9.500   1.0759   0.03078   0.02198  -0.0347   0.1134   1.0000
   9.750   1.0795   0.03264   0.02377  -0.0334   0.0990   1.0000
  10.000   1.0839   0.03452   0.02563  -0.0322   0.0882   1.0000
  10.250   1.0880   0.03649   0.02758  -0.0311   0.0802   1.0000
  10.500   1.0928   0.03846   0.02957  -0.0302   0.0738   1.0000
  10.750   1.0977   0.04048   0.03162  -0.0293   0.0689   1.0000
  11.000   1.1038   0.04245   0.03365  -0.0286   0.0646   1.0000
  11.250   1.1074   0.04468   0.03585  -0.0280   0.0612   1.0000
  11.500   1.1155   0.04657   0.03785  -0.0274   0.0576   1.0000
  11.750   1.1220   0.04863   0.03996  -0.0269   0.0547   1.0000
  12.000   1.1269   0.05088   0.04220  -0.0265   0.0523   1.0000
  12.250   1.1360   0.05280   0.04428  -0.0261   0.0495   1.0000
  12.500   1.1435   0.05489   0.04644  -0.0258   0.0472   1.0000
  12.750   1.1501   0.05710   0.04866  -0.0256   0.0453   1.0000
  13.000   1.1583   0.05923   0.05087  -0.0253   0.0435   1.0000
  13.250   1.1672   0.06138   0.05319  -0.0250   0.0416   1.0000
  13.500   1.1752   0.06363   0.05554  -0.0249   0.0400   1.0000
  13.750   1.1826   0.06595   0.05791  -0.0249   0.0387   1.0000
  14.000   1.1913   0.06817   0.06010  -0.0248   0.0374   1.0000
  14.250   1.1969   0.07095   0.06312  -0.0249   0.0362   1.0000
  14.500   1.2015   0.07388   0.06626  -0.0251   0.0350   1.0000
  14.750   1.2051   0.07694   0.06949  -0.0255   0.0340   1.0000
  15.000   1.2082   0.08009   0.07281  -0.0261   0.0332   1.0000
  15.250   1.2111   0.08331   0.07616  -0.0267   0.0325   1.0000
  15.500   1.2141   0.08656   0.07950  -0.0274   0.0320   1.0000
  15.750   1.2182   0.08974   0.08275  -0.0280   0.0314   1.0000
  16.000   1.2133   0.09432   0.08756  -0.0295   0.0311   1.0000
  16.250   1.2031   0.09982   0.09336  -0.0316   0.0308   1.0000
  16.500   1.1905   0.10592   0.09974  -0.0344   0.0305   1.0000
  16.750   1.1746   0.11279   0.10690  -0.0380   0.0303   1.0000
  17.000   1.1566   0.12040   0.11478  -0.0423   0.0302   1.0000
  17.250   1.1347   0.12924   0.12388  -0.0477   0.0302   1.0000
  17.500   1.1084   0.13971   0.13461  -0.0546   0.0303   1.0000
  17.750   1.0727   0.15358   0.14873  -0.0640   0.0306   1.0000
  18.000   1.0157   0.17632   0.17164  -0.0788   0.0311   1.0000
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