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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.87 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1046-il-1000000.txt
Download as CSV file: xf-s1046-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.1274   0.10837   0.10454  -0.0092   1.0000   0.0101
 -19.250  -1.1390   0.10283   0.09891  -0.0119   1.0000   0.0103
 -19.000  -1.1516   0.09725   0.09325  -0.0145   1.0000   0.0105
 -18.750  -1.1636   0.09187   0.08779  -0.0169   1.0000   0.0107
 -18.500  -1.1747   0.08673   0.08256  -0.0191   1.0000   0.0109
 -18.250  -1.1850   0.08179   0.07753  -0.0212   1.0000   0.0111
 -18.000  -1.1924   0.07738   0.07304  -0.0230   1.0000   0.0115
 -17.750  -1.2018   0.07277   0.06833  -0.0248   1.0000   0.0117
 -17.500  -1.2091   0.06852   0.06399  -0.0263   1.0000   0.0119
 -17.250  -1.2143   0.06464   0.06003  -0.0277   1.0000   0.0122
 -17.000  -1.2270   0.05987   0.05517  -0.0293   1.0000   0.0126
 -16.750  -1.2383   0.05541   0.05063  -0.0308   1.0000   0.0131
 -16.500  -1.2432   0.05186   0.04700  -0.0318   1.0000   0.0134
 -16.250  -1.2478   0.04844   0.04351  -0.0326   1.0000   0.0138
 -16.000  -1.2506   0.04532   0.04031  -0.0333   1.0000   0.0144
 -15.750  -1.2498   0.04271   0.03762  -0.0337   1.0000   0.0149
 -15.500  -1.2537   0.03968   0.03451  -0.0341   1.0000   0.0155
 -15.250  -1.2573   0.03679   0.03156  -0.0343   1.0000   0.0163
 -15.000  -1.2574   0.03433   0.02905  -0.0343   1.0000   0.0171
 -14.750  -1.2549   0.03219   0.02684  -0.0341   1.0000   0.0179
 -14.500  -1.2524   0.03012   0.02472  -0.0338   1.0000   0.0191
 -14.250  -1.2506   0.02808   0.02264  -0.0333   1.0000   0.0204
 -14.000  -1.2461   0.02635   0.02087  -0.0326   1.0000   0.0218
 -13.750  -1.2420   0.02468   0.01916  -0.0318   1.0000   0.0238
 -13.500  -1.2376   0.02313   0.01759  -0.0307   1.0000   0.0262
 -13.250  -1.2332   0.02170   0.01614  -0.0294   1.0000   0.0294
 -12.750  -1.2221   0.01930   0.01374  -0.0261   1.0000   0.0377
 -12.500  -1.2154   0.01833   0.01277  -0.0241   1.0000   0.0423
 -12.250  -1.2075   0.01751   0.01194  -0.0220   1.0000   0.0471
 -12.000  -1.2011   0.01670   0.01116  -0.0194   1.0000   0.0527
 -11.750  -1.1923   0.01608   0.01054  -0.0169   1.0000   0.0581
 -11.500  -1.1846   0.01549   0.00998  -0.0139   1.0000   0.0638
 -11.250  -1.1765   0.01494   0.00946  -0.0109   1.0000   0.0710
 -11.000  -1.1624   0.01445   0.00899  -0.0088   1.0000   0.0782
 -10.750  -1.1483   0.01394   0.00852  -0.0067   1.0000   0.0863
 -10.500  -1.1335   0.01346   0.00809  -0.0047   1.0000   0.0949
 -10.250  -1.1174   0.01305   0.00771  -0.0029   1.0000   0.1031
 -10.000  -1.1018   0.01263   0.00733  -0.0009   1.0000   0.1126
  -9.750  -1.0864   0.01221   0.00697   0.0012   1.0000   0.1226
  -9.250  -1.0169   0.01122   0.00614  -0.0027   0.9837   0.1519
  -9.000  -0.9794   0.01078   0.00576  -0.0052   0.9670   0.1662
  -8.750  -0.9426   0.01040   0.00540  -0.0073   0.9408   0.1791
  -8.500  -0.9181   0.01015   0.00511  -0.0067   0.9061   0.1910
  -8.250  -0.8958   0.00996   0.00486  -0.0057   0.8782   0.2023
  -8.000  -0.8726   0.00980   0.00464  -0.0048   0.8558   0.2126
  -7.750  -0.8489   0.00959   0.00441  -0.0040   0.8367   0.2235
  -7.500  -0.8240   0.00943   0.00421  -0.0035   0.8197   0.2328
  -7.250  -0.7987   0.00929   0.00403  -0.0030   0.8047   0.2413
  -7.000  -0.7733   0.00913   0.00384  -0.0026   0.7907   0.2500
  -6.750  -0.7468   0.00902   0.00369  -0.0023   0.7778   0.2587
  -6.500  -0.7211   0.00884   0.00351  -0.0019   0.7661   0.2688
  -6.250  -0.6944   0.00873   0.00336  -0.0017   0.7551   0.2768
  -6.000  -0.6679   0.00859   0.00321  -0.0014   0.7444   0.2857
  -5.750  -0.6408   0.00848   0.00308  -0.0013   0.7345   0.2933
  -5.500  -0.6140   0.00837   0.00294  -0.0010   0.7248   0.3021
  -5.250  -0.5867   0.00825   0.00282  -0.0009   0.7151   0.3099
  -5.000  -0.5594   0.00815   0.00270  -0.0008   0.7063   0.3186
  -4.750  -0.5321   0.00804   0.00258  -0.0006   0.6967   0.3272
  -4.500  -0.5043   0.00796   0.00248  -0.0006   0.6880   0.3360
  -4.250  -0.4770   0.00785   0.00238  -0.0004   0.6787   0.3450
  -3.750  -0.4216   0.00769   0.00219  -0.0003   0.6606   0.3629
  -3.500  -0.3935   0.00761   0.00211  -0.0003   0.6515   0.3714
  -3.250  -0.3658   0.00755   0.00203  -0.0002   0.6422   0.3811
  -3.000  -0.3377   0.00746   0.00196  -0.0002   0.6325   0.3899
  -2.750  -0.3096   0.00742   0.00189  -0.0001   0.6230   0.3992
  -2.500  -0.2818   0.00734   0.00183  -0.0001   0.6128   0.4090
  -2.250  -0.2534   0.00730   0.00178  -0.0001   0.6027   0.4181
  -2.000  -0.2256   0.00725   0.00172   0.0000   0.5924   0.4283
  -1.750  -0.1974   0.00721   0.00168   0.0000   0.5818   0.4379
  -1.500  -0.1690   0.00718   0.00164  -0.0001   0.5713   0.4479
  -1.250  -0.1412   0.00715   0.00161   0.0000   0.5605   0.4579
  -1.000  -0.1128   0.00713   0.00158   0.0000   0.5498   0.4675
  -0.750  -0.0846   0.00711   0.00156   0.0000   0.5395   0.4780
  -0.500  -0.0566   0.00710   0.00154   0.0000   0.5286   0.4878
   0.000   0.0000   0.00708   0.00153   0.0000   0.5085   0.5084
   0.500   0.0566   0.00710   0.00154   0.0000   0.4878   0.5286
   0.750   0.0846   0.00711   0.00156   0.0000   0.4779   0.5395
   1.000   0.1128   0.00713   0.00158   0.0000   0.4674   0.5499
   1.250   0.1412   0.00715   0.00161   0.0000   0.4579   0.5606
   1.500   0.1690   0.00718   0.00164   0.0001   0.4478   0.5714
   1.750   0.1974   0.00721   0.00168   0.0000   0.4379   0.5818
   2.000   0.2256   0.00725   0.00172   0.0000   0.4283   0.5924
   2.250   0.2534   0.00730   0.00178   0.0001   0.4181   0.6028
   2.500   0.2818   0.00734   0.00183   0.0001   0.4090   0.6129
   2.750   0.3096   0.00742   0.00189   0.0001   0.3993   0.6230
   3.000   0.3377   0.00746   0.00196   0.0002   0.3899   0.6325
   3.250   0.3658   0.00755   0.00203   0.0002   0.3811   0.6422
   3.500   0.3935   0.00761   0.00211   0.0003   0.3713   0.6515
   3.750   0.4216   0.00769   0.00219   0.0003   0.3629   0.6606
   4.250   0.4770   0.00785   0.00238   0.0004   0.3449   0.6787
   4.500   0.5043   0.00796   0.00248   0.0006   0.3360   0.6881
   4.750   0.5321   0.00804   0.00258   0.0006   0.3272   0.6967
   5.000   0.5594   0.00815   0.00270   0.0008   0.3186   0.7061
   5.250   0.5867   0.00825   0.00282   0.0009   0.3099   0.7152
   5.500   0.6140   0.00837   0.00294   0.0010   0.3021   0.7248
   5.750   0.6408   0.00848   0.00308   0.0013   0.2934   0.7344
   6.000   0.6679   0.00859   0.00321   0.0014   0.2857   0.7443
   6.250   0.6944   0.00873   0.00336   0.0017   0.2768   0.7551
   6.500   0.7211   0.00884   0.00351   0.0019   0.2689   0.7660
   6.750   0.7468   0.00902   0.00369   0.0023   0.2588   0.7777
   7.000   0.7733   0.00913   0.00384   0.0026   0.2499   0.7907
   7.250   0.7987   0.00929   0.00403   0.0030   0.2411   0.8047
   7.500   0.8241   0.00943   0.00421   0.0035   0.2327   0.8196
   7.750   0.8489   0.00959   0.00441   0.0040   0.2236   0.8365
   8.000   0.8726   0.00980   0.00464   0.0048   0.2125   0.8557
   8.250   0.8959   0.00996   0.00486   0.0056   0.2024   0.8781
   8.500   0.9182   0.01015   0.00510   0.0067   0.1911   0.9061
   8.750   0.9427   0.01040   0.00540   0.0073   0.1790   0.9411
   9.000   0.9796   0.01078   0.00576   0.0051   0.1660   0.9672
   9.250   1.0171   0.01121   0.00614   0.0027   0.1527   0.9837
   9.750   1.0866   0.01220   0.00697  -0.0012   0.1233   1.0000
  10.000   1.1018   0.01263   0.00733   0.0009   0.1124   1.0000
  10.250   1.1172   0.01306   0.00771   0.0029   0.1027   1.0000
  10.500   1.1335   0.01346   0.00809   0.0047   0.0947   1.0000
  10.750   1.1485   0.01394   0.00852   0.0067   0.0864   1.0000
  11.000   1.1624   0.01446   0.00899   0.0088   0.0780   1.0000
  11.250   1.1762   0.01496   0.00947   0.0109   0.0704   1.0000
  11.500   1.1852   0.01549   0.00997   0.0138   0.0640   1.0000
  11.750   1.1925   0.01608   0.01055   0.0168   0.0580   1.0000
  12.000   1.2013   0.01671   0.01117   0.0194   0.0524   1.0000
  12.250   1.2079   0.01750   0.01194   0.0219   0.0470   1.0000
  12.500   1.2158   0.01833   0.01277   0.0241   0.0421   1.0000
  12.750   1.2228   0.01929   0.01372   0.0260   0.0378   1.0000
  13.000   1.2272   0.02050   0.01492   0.0279   0.0329   1.0000
  13.250   1.2333   0.02172   0.01615   0.0294   0.0292   1.0000
  13.500   1.2386   0.02310   0.01756   0.0306   0.0263   1.0000
  13.750   1.2427   0.02467   0.01915   0.0317   0.0237   1.0000
  14.000   1.2472   0.02632   0.02084   0.0325   0.0218   1.0000
  14.250   1.2516   0.02806   0.02262   0.0331   0.0203   1.0000
  14.500   1.2528   0.03016   0.02476   0.0336   0.0189   1.0000
  14.750   1.2565   0.03212   0.02678   0.0339   0.0180   1.0000
  15.000   1.2588   0.03429   0.02901   0.0341   0.0170   1.0000
  15.250   1.2582   0.03680   0.03157   0.0341   0.0162   1.0000
  15.500   1.2541   0.03975   0.03457   0.0339   0.0153   1.0000
  15.750   1.2531   0.04248   0.03739   0.0335   0.0147   1.0000
  16.000   1.2523   0.04528   0.04026   0.0331   0.0143   1.0000
  16.250   1.2501   0.04833   0.04339   0.0324   0.0137   1.0000
  16.500   1.2453   0.05180   0.04694   0.0315   0.0134   1.0000
  16.750   1.2390   0.05553   0.05073   0.0304   0.0129   1.0000
  17.000   1.2281   0.05996   0.05525   0.0290   0.0125   1.0000
  17.250   1.2150   0.06478   0.06017   0.0273   0.0121   1.0000
  17.500   1.2120   0.06836   0.06383   0.0261   0.0118   1.0000
  17.750   1.2028   0.07289   0.06845   0.0244   0.0116   1.0000
  18.000   1.1950   0.07727   0.07292   0.0227   0.0112   1.0000
  18.250   1.1863   0.08188   0.07761   0.0208   0.0111   1.0000
  18.500   1.1777   0.08656   0.08238   0.0189   0.0110   1.0000
  18.750   1.1672   0.09161   0.08752   0.0167   0.0108   1.0000
  19.000   1.1537   0.09720   0.09321   0.0142   0.0106   1.0000
  19.250   1.1438   0.10236   0.09844   0.0118   0.0104   1.0000
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