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NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-215 MOD B (n63215b-il)
Reynolds number: 100,000
Max Cl/Cd: 35.32 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63215b-il-100000-n5.txt
Download as CSV file: xf-n63215b-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-215 MOD B                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6191   0.11806   0.11231  -0.0174   1.0000   0.0355
 -14.250  -0.6960   0.09493   0.08896  -0.0321   1.0000   0.0347
 -14.000  -0.7402   0.08320   0.07698  -0.0401   1.0000   0.0343
 -13.750  -0.7730   0.07494   0.06847  -0.0454   1.0000   0.0341
 -13.500  -0.7984   0.06851   0.06180  -0.0488   1.0000   0.0341
 -13.250  -0.8180   0.06332   0.05637  -0.0511   1.0000   0.0342
 -13.000  -0.8337   0.05889   0.05169  -0.0524   1.0000   0.0345
 -12.750  -0.8457   0.05507   0.04763  -0.0531   1.0000   0.0348
 -12.500  -0.8558   0.05161   0.04387  -0.0532   1.0000   0.0353
 -12.250  -0.8621   0.04861   0.04059  -0.0528   1.0000   0.0357
 -12.000  -0.8621   0.04608   0.03785  -0.0521   1.0000   0.0363
 -11.750  -0.8529   0.04428   0.03605  -0.0515   1.0000   0.0370
 -11.500  -0.8450   0.04264   0.03435  -0.0507   1.0000   0.0378
 -11.250  -0.8380   0.04110   0.03275  -0.0497   1.0000   0.0389
 -11.000  -0.8308   0.03952   0.03103  -0.0485   1.0000   0.0402
 -10.750  -0.8222   0.03794   0.02926  -0.0471   1.0000   0.0415
 -10.500  -0.8128   0.03647   0.02760  -0.0456   1.0000   0.0429
 -10.250  -0.7988   0.03525   0.02647  -0.0445   1.0000   0.0444
 -10.000  -0.7862   0.03417   0.02538  -0.0431   1.0000   0.0459
  -9.750  -0.7718   0.03304   0.02418  -0.0418   1.0000   0.0476
  -9.500  -0.7564   0.03192   0.02296  -0.0405   1.0000   0.0492
  -9.250  -0.7420   0.03086   0.02184  -0.0389   1.0000   0.0510
  -9.000  -0.7308   0.02994   0.02102  -0.0370   1.0000   0.0526
  -8.750  -0.7235   0.02920   0.02031  -0.0344   1.0000   0.0543
  -8.500  -0.7206   0.02857   0.01968  -0.0310   1.0000   0.0556
  -8.250  -0.6925   0.02754   0.01858  -0.0320   0.9895   0.0582
  -8.000  -0.6604   0.02639   0.01743  -0.0339   0.9802   0.0615
  -7.750  -0.6295   0.02539   0.01645  -0.0356   0.9699   0.0655
  -7.500  -0.5988   0.02449   0.01546  -0.0370   0.9603   0.0698
  -7.250  -0.5688   0.02344   0.01448  -0.0385   0.9519   0.0752
  -7.000  -0.5424   0.02263   0.01364  -0.0391   0.9411   0.0829
  -6.750  -0.5163   0.02180   0.01283  -0.0397   0.9316   0.0944
  -6.500  -0.4907   0.02089   0.01203  -0.0401   0.9228   0.1118
  -6.250  -0.4695   0.02006   0.01134  -0.0398   0.9123   0.1395
  -6.000  -0.4481   0.01910   0.01063  -0.0395   0.9037   0.1863
  -5.750  -0.4308   0.01810   0.01004  -0.0387   0.8939   0.2569
  -5.500  -0.4121   0.01731   0.00973  -0.0377   0.8855   0.3449
  -5.250  -0.3891   0.01700   0.00966  -0.0369   0.8775   0.4119
  -5.000  -0.3640   0.01691   0.00966  -0.0362   0.8704   0.4604
  -4.750  -0.3392   0.01694   0.00973  -0.0353   0.8626   0.4962
  -4.500  -0.3120   0.01701   0.00976  -0.0348   0.8572   0.5254
  -4.250  -0.2871   0.01715   0.00990  -0.0339   0.8496   0.5456
  -4.000  -0.2601   0.01723   0.00994  -0.0333   0.8436   0.5626
  -3.750  -0.2336   0.01735   0.01002  -0.0326   0.8375   0.5790
  -3.500  -0.2079   0.01752   0.01017  -0.0317   0.8307   0.5950
  -3.250  -0.1806   0.01758   0.01015  -0.0312   0.8257   0.6085
  -3.000  -0.1541   0.01766   0.01023  -0.0306   0.8194   0.6159
  -2.750  -0.1276   0.01760   0.01007  -0.0301   0.8115   0.6256
  -2.500  -0.1015   0.01759   0.01003  -0.0291   0.8022   0.6328
  -2.250  -0.0747   0.01742   0.00974  -0.0285   0.7925   0.6415
  -2.000  -0.0493   0.01737   0.00967  -0.0275   0.7811   0.6471
  -1.750  -0.0226   0.01723   0.00945  -0.0269   0.7713   0.6548
  -1.500   0.0038   0.01713   0.00931  -0.0261   0.7612   0.6612
  -1.250   0.0301   0.01708   0.00924  -0.0254   0.7517   0.6680
  -1.000   0.0575   0.01697   0.00905  -0.0250   0.7435   0.6754
  -0.750   0.0834   0.01694   0.00903  -0.0243   0.7332   0.6810
  -0.500   0.1109   0.01681   0.00884  -0.0239   0.7239   0.6884
  -0.250   0.1369   0.01674   0.00877  -0.0231   0.7122   0.6944
   0.000   0.1630   0.01666   0.00868  -0.0224   0.6994   0.7011
   0.250   0.1897   0.01654   0.00852  -0.0218   0.6854   0.7084
   0.500   0.2151   0.01645   0.00843  -0.0208   0.6685   0.7144
   0.750   0.2414   0.01634   0.00827  -0.0202   0.6497   0.7229
   1.000   0.2666   0.01627   0.00819  -0.0191   0.6303   0.7290
   1.250   0.2922   0.01621   0.00809  -0.0183   0.6070   0.7366
   1.500   0.3172   0.01617   0.00798  -0.0174   0.5768   0.7434
   1.750   0.3413   0.01618   0.00789  -0.0162   0.5348   0.7504
   2.000   0.3641   0.01633   0.00771  -0.0150   0.4615   0.7582
   2.250   0.3822   0.01683   0.00772  -0.0131   0.3828   0.7648
   2.500   0.4030   0.01737   0.00791  -0.0121   0.3497   0.7733
   2.750   0.4241   0.01776   0.00821  -0.0108   0.3285   0.7799
   3.000   0.4475   0.01812   0.00847  -0.0101   0.3110   0.7889
   3.250   0.4694   0.01845   0.00875  -0.0090   0.2962   0.7963
   3.500   0.4928   0.01878   0.00900  -0.0083   0.2830   0.8059
   3.750   0.5145   0.01909   0.00927  -0.0071   0.2714   0.8135
   4.000   0.5385   0.01939   0.00954  -0.0065   0.2609   0.8231
   4.250   0.5599   0.01972   0.00981  -0.0053   0.2522   0.8315
   4.500   0.5831   0.02000   0.01010  -0.0045   0.2424   0.8412
   4.750   0.6047   0.02032   0.01038  -0.0034   0.2339   0.8508
   5.000   0.6266   0.02061   0.01068  -0.0024   0.2252   0.8608
   5.250   0.6484   0.02096   0.01098  -0.0014   0.2181   0.8722
   5.500   0.6696   0.02124   0.01131  -0.0002   0.2110   0.8838
   5.750   0.6905   0.02161   0.01162   0.0009   0.2055   0.8964
   6.000   0.7131   0.02194   0.01202   0.0018   0.1998   0.9103
   6.250   0.7369   0.02230   0.01242   0.0024   0.1941   0.9259
   6.500   0.7639   0.02277   0.01284   0.0022   0.1892   0.9438
   7.000   0.8278   0.02374   0.01392  -0.0006   0.1771   1.0000
   7.250   0.8517   0.02434   0.01440  -0.0007   0.1728   1.0000
   7.500   0.8765   0.02492   0.01508  -0.0008   0.1677   1.0000
   7.750   0.9008   0.02554   0.01571  -0.0009   0.1634   1.0000
   8.000   0.9243   0.02617   0.01631  -0.0008   0.1597   1.0000
   8.250   0.9477   0.02690   0.01702  -0.0007   0.1560   1.0000
   8.500   0.9702   0.02762   0.01785  -0.0005   0.1517   1.0000
   8.750   0.9918   0.02831   0.01857  -0.0001   0.1477   1.0000
   9.000   1.0128   0.02900   0.01923   0.0003   0.1443   1.0000
   9.250   1.0341   0.02984   0.02005   0.0006   0.1413   1.0000
   9.500   1.0535   0.03071   0.02110   0.0012   0.1377   1.0000
   9.750   1.0722   0.03156   0.02204   0.0019   0.1343   1.0000
  10.000   1.0901   0.03235   0.02285   0.0026   0.1314   1.0000
  10.250   1.1077   0.03316   0.02363   0.0033   0.1289   1.0000
  10.500   1.1250   0.03420   0.02470   0.0041   0.1267   1.0000
  10.750   1.1381   0.03538   0.02611   0.0053   0.1243   1.0000
  11.000   1.1506   0.03660   0.02748   0.0064   0.1219   1.0000
  11.250   1.1625   0.03780   0.02879   0.0075   0.1197   1.0000
  11.500   1.1743   0.03898   0.03005   0.0085   0.1177   1.0000
  11.750   1.1864   0.04010   0.03120   0.0094   0.1159   1.0000
  12.000   1.1999   0.04122   0.03232   0.0101   0.1142   1.0000
  12.250   1.2078   0.04283   0.03404   0.0110   0.1125   1.0000
  12.500   1.2067   0.04493   0.03641   0.0122   0.1107   1.0000
  12.750   1.2051   0.04718   0.03890   0.0131   0.1089   1.0000
  13.000   1.2031   0.04956   0.04147   0.0138   0.1072   1.0000
  13.250   1.2008   0.05209   0.04416   0.0141   0.1057   1.0000
  13.500   1.1979   0.05479   0.04701   0.0143   0.1045   1.0000
  13.750   1.1950   0.05758   0.04993   0.0141   0.1033   1.0000
  14.000   1.1935   0.06036   0.05282   0.0138   0.1022   1.0000
  14.250   1.1941   0.06305   0.05559   0.0133   0.1012   1.0000
  14.500   1.1979   0.06559   0.05816   0.0129   0.1002   1.0000
  14.750   1.1756   0.07121   0.06399   0.0109   0.0994   1.0000
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