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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 100,000
Max Cl/Cd: 37.18 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1046-il-100000.txt
Download as CSV file: xf-s1046-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.5200   0.18632   0.18169   0.0217   1.0000   0.1271
 -17.750  -0.6758   0.19870   0.19327   0.0267   1.0000   0.1268
 -17.500  -0.9601   0.10939   0.10371  -0.0194   1.0000   0.0657
 -17.250  -0.8681   0.12390   0.11860  -0.0091   1.0000   0.0762
 -17.000  -0.9373   0.10620   0.10067  -0.0194   1.0000   0.0734
 -16.750  -0.9838   0.09436   0.08854  -0.0262   1.0000   0.0723
 -16.500  -1.0101   0.08666   0.08059  -0.0302   1.0000   0.0729
 -16.250  -1.0327   0.08004   0.07372  -0.0335   1.0000   0.0742
 -16.000  -1.0547   0.07398   0.06740  -0.0362   1.0000   0.0757
 -15.750  -1.0461   0.07187   0.06541  -0.0361   1.0000   0.0806
 -15.500  -1.0540   0.06795   0.06140  -0.0374   1.0000   0.0843
 -15.250  -0.7010   0.13214   0.12669  -0.0010   1.0000   0.1225
 -15.000  -1.0671   0.06074   0.05405  -0.0389   1.0000   0.0933
 -14.750  -1.0775   0.05704   0.05020  -0.0397   1.0000   0.0980
 -14.500  -1.0822   0.05394   0.04708  -0.0399   1.0000   0.1040
 -14.250  -1.0874   0.05114   0.04424  -0.0401   1.0000   0.1103
 -14.000  -1.0925   0.04829   0.04134  -0.0399   1.0000   0.1168
 -13.750  -1.0977   0.04584   0.03885  -0.0395   1.0000   0.1239
 -13.500  -1.1002   0.04356   0.03657  -0.0389   1.0000   0.1313
 -13.250  -1.1074   0.04129   0.03419  -0.0379   1.0000   0.1387
 -13.000  -1.1057   0.03963   0.03260  -0.0368   1.0000   0.1469
 -12.750  -1.1160   0.03758   0.03034  -0.0349   1.0000   0.1543
 -12.500  -1.1104   0.03646   0.02935  -0.0334   1.0000   0.1636
 -12.250  -1.1145   0.03500   0.02781  -0.0309   1.0000   0.1720
 -12.000  -1.1158   0.03403   0.02681  -0.0280   1.0000   0.1810
 -11.750  -1.1126   0.03324   0.02610  -0.0253   1.0000   0.1904
 -11.500  -1.1145   0.03225   0.02496  -0.0220   1.0000   0.2001
 -11.250  -1.1063   0.03166   0.02439  -0.0197   1.0000   0.2110
 -11.000  -1.0930   0.03110   0.02391  -0.0179   1.0000   0.2219
 -10.750  -1.0828   0.03038   0.02314  -0.0157   1.0000   0.2328
 -10.500  -1.0774   0.02957   0.02209  -0.0129   1.0000   0.2436
 -10.250  -1.0558   0.02918   0.02187  -0.0120   1.0000   0.2548
 -10.000  -1.0386   0.02865   0.02136  -0.0105   1.0000   0.2655
  -9.750  -1.0266   0.02795   0.02054  -0.0084   1.0000   0.2765
  -9.500  -1.0100   0.02751   0.02008  -0.0068   1.0000   0.2876
  -9.250  -0.9894   0.02714   0.01978  -0.0056   1.0000   0.2981
  -9.000  -0.9745   0.02657   0.01915  -0.0037   1.0000   0.3089
  -8.750  -0.9606   0.02609   0.01858  -0.0016   1.0000   0.3198
  -8.500  -0.9393   0.02580   0.01842  -0.0004   1.0000   0.3296
  -8.250  -0.9261   0.02525   0.01779   0.0018   1.0000   0.3397
  -8.000  -0.9116   0.02489   0.01743   0.0038   1.0000   0.3497
  -7.750  -0.8965   0.02455   0.01714   0.0059   1.0000   0.3586
  -7.500  -0.8926   0.02406   0.01648   0.0093   1.0000   0.3683
  -7.250  -0.8774   0.02390   0.01649   0.0113   1.0000   0.3761
  -7.000  -0.8730   0.02346   0.01590   0.0144   1.0000   0.3855
  -6.750  -0.8595   0.02335   0.01589   0.0165   1.0000   0.3936
  -6.500  -0.8504   0.02302   0.01548   0.0188   1.0000   0.4029
  -6.250  -0.8303   0.02287   0.01532   0.0194   0.9979   0.4130
  -6.000  -0.7832   0.02279   0.01525   0.0152   0.9878   0.4259
  -5.750  -0.7372   0.02263   0.01506   0.0112   0.9777   0.4388
  -5.500  -0.6900   0.02244   0.01482   0.0071   0.9681   0.4523
  -5.250  -0.6492   0.02220   0.01448   0.0042   0.9566   0.4656
  -5.000  -0.6051   0.02207   0.01438   0.0010   0.9464   0.4780
  -4.750  -0.5539   0.02192   0.01426  -0.0034   0.9386   0.4906
  -4.500  -0.5133   0.02172   0.01406  -0.0058   0.9274   0.5027
  -4.250  -0.4700   0.02148   0.01377  -0.0087   0.9180   0.5159
  -4.000  -0.4303   0.02124   0.01348  -0.0108   0.9074   0.5294
  -3.750  -0.3939   0.02121   0.01353  -0.0119   0.8952   0.5394
  -3.500  -0.3596   0.02107   0.01338  -0.0128   0.8836   0.5510
  -3.250  -0.3258   0.02087   0.01312  -0.0135   0.8731   0.5635
  -3.000  -0.2990   0.02084   0.01310  -0.0128   0.8592   0.5745
  -2.750  -0.2722   0.02083   0.01312  -0.0121   0.8459   0.5846
  -2.500  -0.2474   0.02074   0.01298  -0.0112   0.8329   0.5964
  -2.250  -0.2212   0.02069   0.01290  -0.0103   0.8211   0.6082
  -2.000  -0.1943   0.02070   0.01293  -0.0093   0.8089   0.6180
  -1.750  -0.1715   0.02066   0.01287  -0.0081   0.7953   0.6297
  -1.500  -0.1486   0.02062   0.01278  -0.0068   0.7824   0.6424
  -1.250  -0.1217   0.02067   0.01288  -0.0058   0.7708   0.6518
  -1.000  -0.0968   0.02060   0.01278  -0.0046   0.7593   0.6635
  -0.750  -0.0745   0.02058   0.01272  -0.0034   0.7460   0.6764
  -0.500  -0.0490   0.02065   0.01285  -0.0023   0.7336   0.6865
  -0.250  -0.0238   0.02062   0.01279  -0.0012   0.7226   0.6980
   0.000   0.0000   0.02056   0.01271   0.0000   0.7108   0.7108
   0.250   0.0238   0.02062   0.01279   0.0012   0.6981   0.7227
   0.500   0.0490   0.02065   0.01285   0.0023   0.6865   0.7336
   0.750   0.0745   0.02058   0.01273   0.0034   0.6764   0.7460
   1.000   0.0968   0.02060   0.01278   0.0046   0.6635   0.7593
   1.250   0.1217   0.02067   0.01288   0.0058   0.6518   0.7708
   1.500   0.1486   0.02062   0.01278   0.0068   0.6424   0.7824
   1.750   0.1715   0.02066   0.01287   0.0081   0.6297   0.7953
   2.000   0.1943   0.02069   0.01293   0.0093   0.6180   0.8088
   2.250   0.2212   0.02069   0.01290   0.0103   0.6082   0.8211
   2.500   0.2474   0.02074   0.01298   0.0112   0.5964   0.8329
   2.750   0.2721   0.02083   0.01312   0.0121   0.5846   0.8459
   3.000   0.2990   0.02084   0.01310   0.0128   0.5745   0.8592
   3.250   0.3258   0.02086   0.01312   0.0135   0.5635   0.8731
   3.500   0.3596   0.02107   0.01338   0.0128   0.5510   0.8837
   3.750   0.3939   0.02121   0.01353   0.0119   0.5395   0.8953
   4.000   0.4303   0.02124   0.01346   0.0108   0.5293   0.9074
   4.250   0.4700   0.02148   0.01377   0.0087   0.5159   0.9180
   4.500   0.5133   0.02172   0.01406   0.0058   0.5028   0.9274
   4.750   0.5539   0.02192   0.01426   0.0034   0.4906   0.9386
   5.000   0.6051   0.02207   0.01438  -0.0010   0.4780   0.9464
   5.250   0.6493   0.02219   0.01447  -0.0042   0.4656   0.9567
   5.500   0.6900   0.02245   0.01482  -0.0071   0.4524   0.9681
   5.750   0.7373   0.02263   0.01506  -0.0113   0.4389   0.9778
   6.000   0.7832   0.02279   0.01525  -0.0152   0.4260   0.9878
   6.250   0.8304   0.02287   0.01532  -0.0194   0.4129   0.9979
   6.500   0.8503   0.02301   0.01547  -0.0188   0.4029   1.0000
   6.750   0.8593   0.02335   0.01589  -0.0164   0.3936   1.0000
   7.000   0.8727   0.02347   0.01592  -0.0144   0.3855   1.0000
   7.250   0.8772   0.02390   0.01649  -0.0113   0.3762   1.0000
   7.500   0.8924   0.02405   0.01648  -0.0092   0.3683   1.0000
   7.750   0.8964   0.02455   0.01714  -0.0059   0.3586   1.0000
   8.000   0.9115   0.02489   0.01742  -0.0038   0.3498   1.0000
   8.250   0.9261   0.02524   0.01779  -0.0018   0.3397   1.0000
   8.500   0.9393   0.02580   0.01841   0.0004   0.3296   1.0000
   8.750   0.9606   0.02609   0.01858   0.0016   0.3198   1.0000
   9.000   0.9744   0.02657   0.01915   0.0037   0.3089   1.0000
   9.250   0.9894   0.02714   0.01978   0.0056   0.2981   1.0000
   9.500   1.0101   0.02751   0.02007   0.0067   0.2876   1.0000
   9.750   1.0267   0.02795   0.02053   0.0084   0.2765   1.0000
  10.000   1.0387   0.02865   0.02136   0.0105   0.2655   1.0000
  10.250   1.0558   0.02918   0.02187   0.0120   0.2548   1.0000
  10.500   1.0776   0.02958   0.02210   0.0129   0.2436   1.0000
  10.750   1.0830   0.03037   0.02313   0.0157   0.2327   1.0000
  11.000   1.0932   0.03110   0.02391   0.0178   0.2219   1.0000
  11.250   1.1064   0.03166   0.02439   0.0196   0.2109   1.0000
  11.500   1.1147   0.03224   0.02495   0.0219   0.2000   1.0000
  11.750   1.1130   0.03325   0.02610   0.0252   0.1903   1.0000
  12.000   1.1160   0.03404   0.02683   0.0280   0.1809   1.0000
  12.250   1.1152   0.03499   0.02779   0.0308   0.1719   1.0000
  12.500   1.1107   0.03646   0.02935   0.0333   0.1635   1.0000
  12.750   1.1163   0.03758   0.03034   0.0348   0.1542   1.0000
  13.000   1.1064   0.03962   0.03259   0.0367   0.1468   1.0000
  13.250   1.1078   0.04129   0.03420   0.0378   0.1386   1.0000
  13.500   1.1012   0.04353   0.03654   0.0388   0.1311   1.0000
  13.750   1.0986   0.04583   0.03884   0.0394   0.1238   1.0000
  14.000   1.0940   0.04824   0.04127   0.0398   0.1166   1.0000
  14.250   1.0878   0.05116   0.04426   0.0399   0.1101   1.0000
  14.500   1.0838   0.05387   0.04699   0.0398   0.1037   1.0000
  14.750   1.0787   0.05703   0.05020   0.0396   0.0980   1.0000
  15.000   1.0684   0.06070   0.05400   0.0388   0.0930   1.0000
  15.250   1.0727   0.06306   0.05623   0.0388   0.0871   1.0000
  15.500   1.0552   0.06795   0.06139   0.0372   0.0842   1.0000
  15.750   1.0482   0.07171   0.06523   0.0360   0.0803   1.0000
  16.000   1.0551   0.07408   0.06750   0.0360   0.0756   1.0000
  16.250   1.0337   0.08009   0.07378   0.0332   0.0741   1.0000
  16.500   1.0113   0.08670   0.08063   0.0300   0.0728   1.0000
  16.750   0.9846   0.09446   0.08863   0.0259   0.0720   1.0000
  17.000   0.9384   0.10625   0.10072   0.0191   0.0731   1.0000
  17.250   0.8508   0.12806   0.12282   0.0063   0.0771   1.0000
  17.500   0.9523   0.11109   0.10549   0.0178   0.0663   1.0000
  17.750   0.7000   0.18334   0.17791  -0.0211   0.0881   1.0000
  18.000   0.7045   0.18897   0.18356  -0.0231   0.0883   1.0000
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