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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.94 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1046-il-1000000-n5.txt
Download as CSV file: xf-s1046-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1046 17% (Danny Howell)                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.1560   0.10361   0.09956  -0.0115   1.0000   0.0070
 -19.250  -1.1650   0.09858   0.09445  -0.0138   1.0000   0.0071
 -19.000  -1.1744   0.09360   0.08938  -0.0161   1.0000   0.0072
 -18.500  -1.1937   0.08381   0.07941  -0.0203   1.0000   0.0075
 -18.250  -1.2028   0.07912   0.07464  -0.0222   1.0000   0.0076
 -18.000  -1.2123   0.07449   0.06993  -0.0241   1.0000   0.0080
 -17.750  -1.2200   0.07016   0.06553  -0.0257   1.0000   0.0081
 -17.500  -1.2269   0.06604   0.06132  -0.0272   1.0000   0.0083
 -17.250  -1.2333   0.06209   0.05729  -0.0286   1.0000   0.0086
 -17.000  -1.2383   0.05836   0.05348  -0.0298   1.0000   0.0089
 -16.750  -1.2421   0.05485   0.04990  -0.0308   1.0000   0.0092
 -16.500  -1.2444   0.05163   0.04660  -0.0317   1.0000   0.0094
 -16.250  -1.2460   0.04855   0.04345  -0.0325   1.0000   0.0096
 -16.000  -1.2497   0.04534   0.04017  -0.0332   1.0000   0.0101
 -15.750  -1.2513   0.04248   0.03724  -0.0336   1.0000   0.0105
 -15.500  -1.2514   0.03985   0.03455  -0.0339   1.0000   0.0110
 -15.250  -1.2501   0.03744   0.03207  -0.0341   1.0000   0.0113
 -15.000  -1.2473   0.03522   0.02979  -0.0341   1.0000   0.0118
 -14.750  -1.2429   0.03323   0.02774  -0.0341   1.0000   0.0121
 -14.500  -1.2404   0.03113   0.02559  -0.0338   1.0000   0.0129
 -14.250  -1.2359   0.02927   0.02368  -0.0335   1.0000   0.0135
 -14.000  -1.2301   0.02759   0.02196  -0.0330   1.0000   0.0142
 -13.750  -1.2229   0.02609   0.02041  -0.0324   1.0000   0.0149
 -13.500  -1.2159   0.02464   0.01891  -0.0316   1.0000   0.0157
 -13.250  -1.2090   0.02327   0.01751  -0.0307   1.0000   0.0168
 -13.000  -1.2006   0.02209   0.01629  -0.0296   1.0000   0.0179
 -12.750  -1.1924   0.02097   0.01515  -0.0283   1.0000   0.0193
 -12.500  -1.1843   0.01994   0.01409  -0.0268   1.0000   0.0212
 -12.250  -1.1768   0.01897   0.01311  -0.0250   1.0000   0.0239
 -12.000  -1.1682   0.01814   0.01227  -0.0231   1.0000   0.0270
 -11.750  -1.1608   0.01734   0.01148  -0.0207   1.0000   0.0310
 -11.500  -1.1511   0.01672   0.01085  -0.0184   1.0000   0.0342
 -11.250  -1.1430   0.01611   0.01026  -0.0156   1.0000   0.0392
 -11.000  -1.1353   0.01558   0.00974  -0.0125   1.0000   0.0437
 -10.750  -1.1223   0.01513   0.00930  -0.0102   1.0000   0.0478
 -10.500  -1.1030   0.01458   0.00878  -0.0093   0.9920   0.0539
 -10.250  -1.0617   0.01389   0.00812  -0.0130   0.9521   0.0639
 -10.000  -1.0360   0.01339   0.00757  -0.0131   0.9001   0.0744
  -9.750  -1.0198   0.01304   0.00715  -0.0112   0.8643   0.0832
  -9.500  -1.0022   0.01266   0.00674  -0.0096   0.8387   0.0942
  -9.250  -0.9819   0.01234   0.00638  -0.0084   0.8186   0.1032
  -9.000  -0.9609   0.01202   0.00604  -0.0074   0.8005   0.1131
  -8.750  -0.9394   0.01168   0.00570  -0.0064   0.7854   0.1238
  -8.500  -0.9175   0.01134   0.00538  -0.0055   0.7716   0.1363
  -8.000  -0.8710   0.01075   0.00480  -0.0041   0.7470   0.1597
  -7.750  -0.8467   0.01051   0.00456  -0.0036   0.7364   0.1708
  -7.250  -0.7967   0.01006   0.00410  -0.0027   0.7160   0.1895
  -7.000  -0.7709   0.00989   0.00391  -0.0024   0.7065   0.1985
  -6.750  -0.7454   0.00967   0.00371  -0.0020   0.6969   0.2096
  -6.500  -0.7195   0.00948   0.00353  -0.0017   0.6884   0.2198
  -6.250  -0.6929   0.00934   0.00337  -0.0015   0.6790   0.2283
  -6.000  -0.6665   0.00917   0.00320  -0.0012   0.6709   0.2375
  -5.750  -0.6394   0.00906   0.00307  -0.0011   0.6618   0.2444
  -5.500  -0.6126   0.00891   0.00292  -0.0009   0.6534   0.2533
  -5.250  -0.5853   0.00881   0.00279  -0.0008   0.6442   0.2600
  -5.000  -0.5582   0.00867   0.00266  -0.0006   0.6359   0.2685
  -4.750  -0.5307   0.00859   0.00255  -0.0005   0.6261   0.2760
  -4.500  -0.5034   0.00847   0.00243  -0.0004   0.6166   0.2848
  -4.250  -0.4757   0.00839   0.00233  -0.0004   0.6071   0.2920
  -4.000  -0.4482   0.00829   0.00223  -0.0003   0.5968   0.3006
  -3.750  -0.4204   0.00822   0.00214  -0.0002   0.5863   0.3078
  -3.500  -0.3928   0.00814   0.00205  -0.0001   0.5759   0.3160
  -3.250  -0.3649   0.00808   0.00197  -0.0001   0.5649   0.3239
  -3.000  -0.3371   0.00802   0.00190  -0.0001   0.5546   0.3320
  -2.750  -0.3092   0.00797   0.00183   0.0000   0.5439   0.3398
  -2.500  -0.2812   0.00792   0.00177   0.0000   0.5335   0.3487
  -2.250  -0.2532   0.00787   0.00172   0.0000   0.5234   0.3565
  -1.750  -0.1971   0.00779   0.00162   0.0000   0.5037   0.3744
  -1.500  -0.1690   0.00777   0.00159   0.0000   0.4938   0.3834
  -1.250  -0.1410   0.00774   0.00156   0.0001   0.4836   0.3923
  -0.500  -0.0564   0.00769   0.00150   0.0000   0.4554   0.4188
  -0.250  -0.0282   0.00769   0.00149   0.0000   0.4466   0.4280
   0.000   0.0000   0.00768   0.00149   0.0000   0.4374   0.4374
   0.250   0.0282   0.00769   0.00149   0.0000   0.4282   0.4466
   0.500   0.0564   0.00769   0.00150   0.0000   0.4188   0.4554
   1.250   0.1410   0.00774   0.00156  -0.0001   0.3923   0.4837
   1.500   0.1690   0.00777   0.00159   0.0000   0.3834   0.4939
   1.750   0.1971   0.00779   0.00162   0.0000   0.3742   0.5036
   2.250   0.2532   0.00787   0.00172   0.0000   0.3565   0.5237
   2.500   0.2812   0.00791   0.00177   0.0000   0.3489   0.5336
   2.750   0.3092   0.00797   0.00183   0.0000   0.3400   0.5439
   3.000   0.3371   0.00802   0.00190   0.0001   0.3320   0.5545
   3.250   0.3649   0.00808   0.00197   0.0001   0.3239   0.5650
   3.500   0.3928   0.00815   0.00205   0.0001   0.3159   0.5758
   3.750   0.4204   0.00822   0.00214   0.0002   0.3078   0.5864
   4.000   0.4483   0.00829   0.00223   0.0003   0.3006   0.5966
   4.250   0.4757   0.00839   0.00233   0.0004   0.2918   0.6071
   4.500   0.5034   0.00846   0.00243   0.0004   0.2848   0.6168
   4.750   0.5307   0.00859   0.00255   0.0005   0.2759   0.6261
   5.000   0.5582   0.00868   0.00266   0.0006   0.2684   0.6356
   5.250   0.5852   0.00881   0.00279   0.0008   0.2599   0.6444
   5.500   0.6126   0.00891   0.00292   0.0009   0.2533   0.6535
   5.750   0.6394   0.00906   0.00307   0.0011   0.2445   0.6617
   6.000   0.6665   0.00917   0.00320   0.0012   0.2375   0.6706
   6.250   0.6929   0.00934   0.00337   0.0015   0.2284   0.6790
   6.500   0.7196   0.00948   0.00352   0.0017   0.2201   0.6882
   6.750   0.7455   0.00967   0.00371   0.0020   0.2098   0.6967
   7.000   0.7709   0.00989   0.00391   0.0024   0.1982   0.7064
   7.250   0.7966   0.01007   0.00411   0.0027   0.1892   0.7160
   7.750   0.8467   0.01051   0.00456   0.0036   0.1707   0.7363
   8.000   0.8709   0.01076   0.00481   0.0041   0.1592   0.7470
   8.500   0.9175   0.01134   0.00538   0.0055   0.1363   0.7715
   8.750   0.9394   0.01168   0.00570   0.0064   0.1238   0.7858
   9.000   0.9609   0.01202   0.00604   0.0074   0.1129   0.8008
   9.250   0.9822   0.01232   0.00637   0.0084   0.1039   0.8186
   9.500   1.0019   0.01268   0.00675   0.0096   0.0933   0.8390
   9.750   1.0203   0.01302   0.00714   0.0111   0.0843   0.8645
  10.000   1.0358   0.01340   0.00758   0.0131   0.0737   0.9002
  10.250   1.0618   0.01391   0.00814   0.0129   0.0629   0.9527
  10.500   1.1032   0.01458   0.00878   0.0093   0.0537   0.9922
  10.750   1.1225   0.01513   0.00930   0.0102   0.0477   1.0000
  11.000   1.1353   0.01559   0.00974   0.0125   0.0434   1.0000
  11.250   1.1430   0.01613   0.01027   0.0156   0.0388   1.0000
  11.500   1.1523   0.01668   0.01082   0.0182   0.0348   1.0000
  11.750   1.1612   0.01734   0.01147   0.0207   0.0310   1.0000
  12.000   1.1684   0.01815   0.01228   0.0230   0.0267   1.0000
  12.250   1.1773   0.01896   0.01310   0.0249   0.0239   1.0000
  12.500   1.1848   0.01994   0.01409   0.0267   0.0211   1.0000
  12.750   1.1936   0.02093   0.01511   0.0282   0.0195   1.0000
  13.000   1.2012   0.02208   0.01628   0.0295   0.0178   1.0000
  13.250   1.2097   0.02326   0.01750   0.0306   0.0167   1.0000
  13.500   1.2172   0.02459   0.01886   0.0315   0.0158   1.0000
  13.750   1.2239   0.02606   0.02038   0.0322   0.0148   1.0000
  14.000   1.2311   0.02756   0.02193   0.0328   0.0141   1.0000
  14.250   1.2368   0.02925   0.02366   0.0333   0.0133   1.0000
  14.500   1.2414   0.03112   0.02558   0.0337   0.0127   1.0000
  14.750   1.2447   0.03315   0.02766   0.0339   0.0122   1.0000
  15.000   1.2489   0.03517   0.02974   0.0340   0.0117   1.0000
  15.250   1.2520   0.03736   0.03199   0.0339   0.0113   1.0000
  15.500   1.2523   0.03987   0.03456   0.0337   0.0106   1.0000
  15.750   1.2526   0.04247   0.03722   0.0334   0.0103   1.0000
  16.000   1.2514   0.04530   0.04012   0.0329   0.0100   1.0000
  16.250   1.2484   0.04844   0.04333   0.0323   0.0095   1.0000
  16.500   1.2469   0.05152   0.04649   0.0315   0.0094   1.0000
  16.750   1.2445   0.05475   0.04979   0.0306   0.0090   1.0000
  17.000   1.2407   0.05826   0.05338   0.0295   0.0090   1.0000
  17.250   1.2358   0.06197   0.05717   0.0283   0.0086   1.0000
  17.500   1.2292   0.06596   0.06124   0.0270   0.0082   1.0000
  17.750   1.2226   0.07005   0.06541   0.0255   0.0082   1.0000
  18.000   1.2136   0.07455   0.06998   0.0238   0.0078   1.0000
  18.250   1.2051   0.07904   0.07455   0.0220   0.0076   1.0000
  18.500   1.1970   0.08357   0.07917   0.0201   0.0076   1.0000
  18.750   1.1872   0.08846   0.08414   0.0181   0.0074   1.0000
  19.000   1.1765   0.09354   0.08931   0.0158   0.0073   1.0000
  19.250   1.1681   0.09837   0.09423   0.0136   0.0072   1.0000
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