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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 500,000
Max Cl/Cd: 76.98 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1046-il-500000.txt
Download as CSV file: xf-s1046-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.0741   0.09553   0.09092  -0.0148   1.0000   0.0190
 -17.750  -1.0859   0.09014   0.08547  -0.0172   1.0000   0.0195
 -17.500  -1.0958   0.08511   0.08037  -0.0194   1.0000   0.0200
 -17.250  -1.1045   0.08035   0.07553  -0.0214   1.0000   0.0206
 -17.000  -1.1124   0.07582   0.07090  -0.0232   1.0000   0.0212
 -16.750  -1.1192   0.07150   0.06649  -0.0249   1.0000   0.0220
 -16.500  -1.1240   0.06755   0.06244  -0.0263   1.0000   0.0224
 -16.250  -1.1378   0.06254   0.05735  -0.0282   1.0000   0.0231
 -16.000  -1.1487   0.05801   0.05275  -0.0297   1.0000   0.0241
 -15.750  -1.1557   0.05413   0.04879  -0.0309   1.0000   0.0250
 -15.500  -1.1612   0.05054   0.04512  -0.0318   1.0000   0.0262
 -15.250  -1.1655   0.04720   0.04169  -0.0326   1.0000   0.0275
 -15.000  -1.1742   0.04356   0.03801  -0.0332   1.0000   0.0293
 -14.750  -1.1785   0.04049   0.03487  -0.0336   1.0000   0.0310
 -14.500  -1.1807   0.03775   0.03206  -0.0337   1.0000   0.0336
 -14.250  -1.1852   0.03487   0.02916  -0.0337   1.0000   0.0364
 -14.000  -1.1846   0.03259   0.02682  -0.0335   1.0000   0.0400
 -13.750  -1.1874   0.03011   0.02433  -0.0330   1.0000   0.0442
 -13.500  -1.1862   0.02809   0.02228  -0.0324   1.0000   0.0491
 -13.250  -1.1845   0.02621   0.02039  -0.0315   1.0000   0.0545
 -13.000  -1.1818   0.02451   0.01869  -0.0304   1.0000   0.0599
 -12.750  -1.1757   0.02317   0.01731  -0.0292   1.0000   0.0657
 -12.500  -1.1725   0.02174   0.01590  -0.0277   1.0000   0.0723
 -12.250  -1.1655   0.02064   0.01480  -0.0261   1.0000   0.0789
 -12.000  -1.1592   0.01961   0.01378  -0.0241   1.0000   0.0861
 -11.750  -1.1523   0.01871   0.01288  -0.0220   1.0000   0.0935
 -11.500  -1.1434   0.01797   0.01215  -0.0198   1.0000   0.1017
 -11.250  -1.1362   0.01725   0.01146  -0.0171   1.0000   0.1102
 -11.000  -1.1283   0.01663   0.01087  -0.0142   1.0000   0.1190
 -10.750  -1.1174   0.01611   0.01037  -0.0117   1.0000   0.1286
 -10.500  -1.1042   0.01557   0.00987  -0.0096   1.0000   0.1390
 -10.250  -1.0903   0.01505   0.00938  -0.0076   1.0000   0.1495
 -10.000  -1.0748   0.01460   0.00896  -0.0057   1.0000   0.1595
  -9.500  -1.0430   0.01380   0.00822  -0.0020   1.0000   0.1794
  -9.250  -1.0271   0.01344   0.00789   0.0000   1.0000   0.1891
  -9.000  -1.0114   0.01315   0.00761   0.0020   1.0000   0.1997
  -8.500  -0.9434   0.01239   0.00694  -0.0015   0.9868   0.2274
  -8.250  -0.9054   0.01201   0.00660  -0.0039   0.9754   0.2396
  -8.000  -0.8669   0.01167   0.00626  -0.0064   0.9608   0.2502
  -7.750  -0.8285   0.01140   0.00596  -0.0087   0.9431   0.2609
  -7.500  -0.7967   0.01115   0.00568  -0.0096   0.9202   0.2716
  -7.250  -0.7722   0.01097   0.00544  -0.0089   0.8952   0.2808
  -7.000  -0.7478   0.01088   0.00524  -0.0081   0.8743   0.2897
  -6.750  -0.7247   0.01069   0.00502  -0.0071   0.8560   0.2984
  -6.500  -0.6997   0.01059   0.00483  -0.0065   0.8398   0.3068
  -6.250  -0.6752   0.01043   0.00464  -0.0058   0.8250   0.3157
  -6.000  -0.6496   0.01031   0.00446  -0.0054   0.8112   0.3239
  -5.750  -0.6241   0.01018   0.00430  -0.0049   0.7986   0.3329
  -5.500  -0.5983   0.01006   0.00413  -0.0045   0.7869   0.3414
  -5.250  -0.5721   0.00996   0.00398  -0.0041   0.7757   0.3508
  -5.000  -0.5460   0.00982   0.00383  -0.0037   0.7644   0.3595
  -4.500  -0.4930   0.00962   0.00357  -0.0031   0.7440   0.3779
  -4.250  -0.4659   0.00952   0.00344  -0.0029   0.7338   0.3870
  -4.000  -0.4393   0.00944   0.00333  -0.0026   0.7242   0.3967
  -3.750  -0.4122   0.00933   0.00322  -0.0024   0.7140   0.4058
  -3.500  -0.3849   0.00927   0.00312  -0.0022   0.7044   0.4157
  -3.250  -0.3581   0.00917   0.00302  -0.0019   0.6945   0.4253
  -3.000  -0.3306   0.00910   0.00294  -0.0018   0.6845   0.4351
  -2.750  -0.3034   0.00904   0.00285  -0.0016   0.6752   0.4453
  -2.500  -0.2760   0.00895   0.00278  -0.0014   0.6648   0.4553
  -2.250  -0.2484   0.00891   0.00271  -0.0013   0.6551   0.4656
  -2.000  -0.2211   0.00884   0.00264  -0.0011   0.6449   0.4759
  -1.750  -0.1934   0.00878   0.00259  -0.0010   0.6345   0.4859
  -1.500  -0.1657   0.00877   0.00254  -0.0008   0.6246   0.4967
  -1.250  -0.1383   0.00870   0.00250  -0.0007   0.6138   0.5070
  -1.000  -0.1106   0.00866   0.00246  -0.0005   0.6033   0.5174
  -0.750  -0.0829   0.00866   0.00242  -0.0004   0.5930   0.5284
  -0.500  -0.0554   0.00861   0.00241  -0.0003   0.5818   0.5388
  -0.250  -0.0276   0.00860   0.00240  -0.0001   0.5711   0.5494
   0.000   0.0000   0.00862   0.00238   0.0000   0.5607   0.5606
   0.250   0.0276   0.00860   0.00240   0.0001   0.5494   0.5712
   0.500   0.0554   0.00861   0.00241   0.0003   0.5388   0.5818
   0.750   0.0829   0.00866   0.00242   0.0004   0.5284   0.5930
   1.000   0.1106   0.00866   0.00246   0.0005   0.5174   0.6033
   1.250   0.1383   0.00870   0.00250   0.0007   0.5070   0.6138
   1.750   0.1935   0.00878   0.00259   0.0010   0.4859   0.6345
   2.000   0.2211   0.00884   0.00265   0.0011   0.4759   0.6448
   2.250   0.2484   0.00891   0.00271   0.0013   0.4656   0.6550
   2.500   0.2760   0.00895   0.00278   0.0014   0.4552   0.6648
   2.750   0.3034   0.00904   0.00285   0.0016   0.4453   0.6751
   3.000   0.3306   0.00910   0.00294   0.0018   0.4351   0.6846
   3.250   0.3581   0.00917   0.00302   0.0019   0.4254   0.6945
   3.500   0.3849   0.00927   0.00312   0.0022   0.4157   0.7044
   3.750   0.4122   0.00933   0.00322   0.0024   0.4058   0.7140
   4.000   0.4393   0.00944   0.00333   0.0026   0.3967   0.7242
   4.250   0.4659   0.00952   0.00344   0.0029   0.3869   0.7338
   4.500   0.4930   0.00962   0.00357   0.0031   0.3778   0.7439
   5.000   0.5460   0.00982   0.00383   0.0037   0.3595   0.7645
   5.250   0.5721   0.00996   0.00398   0.0041   0.3507   0.7757
   5.500   0.5983   0.01006   0.00413   0.0044   0.3415   0.7869
   5.750   0.6241   0.01018   0.00429   0.0049   0.3328   0.7986
   6.000   0.6496   0.01031   0.00446   0.0054   0.3239   0.8112
   6.250   0.6752   0.01043   0.00464   0.0058   0.3155   0.8250
   6.500   0.6997   0.01059   0.00483   0.0065   0.3068   0.8398
   6.750   0.7247   0.01069   0.00502   0.0071   0.2983   0.8561
   7.000   0.7478   0.01087   0.00524   0.0081   0.2897   0.8743
   7.250   0.7723   0.01097   0.00544   0.0088   0.2808   0.8952
   7.500   0.7967   0.01115   0.00568   0.0096   0.2716   0.9201
   7.750   0.8286   0.01140   0.00596   0.0087   0.2610   0.9431
   8.000   0.8670   0.01167   0.00626   0.0064   0.2503   0.9609
   8.250   0.9055   0.01201   0.00660   0.0039   0.2397   0.9755
   8.500   0.9435   0.01239   0.00694   0.0015   0.2273   0.9869
   9.000   1.0115   0.01314   0.00761  -0.0020   0.2000   1.0000
   9.250   1.0271   0.01344   0.00789   0.0000   0.1893   1.0000
   9.500   1.0430   0.01380   0.00822   0.0020   0.1794   1.0000
  10.000   1.0747   0.01460   0.00896   0.0057   0.1592   1.0000
  10.250   1.0904   0.01505   0.00938   0.0076   0.1494   1.0000
  10.500   1.1044   0.01557   0.00987   0.0096   0.1392   1.0000
  10.750   1.1177   0.01611   0.01037   0.0117   0.1287   1.0000
  11.000   1.1285   0.01664   0.01087   0.0142   0.1187   1.0000
  11.250   1.1366   0.01724   0.01145   0.0170   0.1103   1.0000
  11.500   1.1437   0.01797   0.01214   0.0197   0.1016   1.0000
  11.750   1.1528   0.01870   0.01287   0.0219   0.0936   1.0000
  12.000   1.1598   0.01961   0.01377   0.0241   0.0863   1.0000
  12.250   1.1662   0.02063   0.01478   0.0260   0.0789   1.0000
  12.500   1.1731   0.02173   0.01590   0.0276   0.0722   1.0000
  12.750   1.1765   0.02315   0.01729   0.0292   0.0657   1.0000
  13.000   1.1825   0.02451   0.01868   0.0303   0.0597   1.0000
  13.250   1.1854   0.02619   0.02037   0.0314   0.0542   1.0000
  13.500   1.1872   0.02806   0.02225   0.0322   0.0491   1.0000
  13.750   1.1886   0.03007   0.02429   0.0329   0.0442   1.0000
  14.000   1.1855   0.03258   0.02680   0.0333   0.0398   1.0000
  14.250   1.1865   0.03484   0.02913   0.0336   0.0364   1.0000
  14.500   1.1817   0.03773   0.03205   0.0336   0.0335   1.0000
  14.750   1.1796   0.04048   0.03487   0.0334   0.0314   1.0000
  15.000   1.1756   0.04352   0.03795   0.0331   0.0289   1.0000
  15.250   1.1662   0.04724   0.04173   0.0324   0.0275   1.0000
  15.500   1.1622   0.05055   0.04513   0.0316   0.0263   1.0000
  15.750   1.1574   0.05406   0.04873   0.0307   0.0249   1.0000
  16.000   1.1503   0.05798   0.05271   0.0295   0.0240   1.0000
  16.250   1.1394   0.06250   0.05730   0.0279   0.0231   1.0000
  16.500   1.1278   0.06724   0.06213   0.0262   0.0223   1.0000
  16.750   1.1214   0.07140   0.06639   0.0247   0.0218   1.0000
  17.000   1.1147   0.07570   0.07078   0.0230   0.0210   1.0000
  17.250   1.1063   0.08030   0.07547   0.0211   0.0204   1.0000
  17.500   1.0971   0.08516   0.08040   0.0191   0.0198   1.0000
  17.750   1.0868   0.09024   0.08556   0.0169   0.0193   1.0000
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