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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 500,000
Max Cl/Cd: 75.15 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1048-il-500000.txt
Download as CSV file: xf-s1048-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1048 14% (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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.8629   0.16676   0.16421   0.0289   1.0000   0.0099
 -18.750  -0.8841   0.15582   0.15313   0.0225   1.0000   0.0098
 -18.500  -0.9057   0.14557   0.14275   0.0165   1.0000   0.0097
 -18.250  -0.9280   0.13551   0.13253   0.0104   1.0000   0.0096
 -18.000  -0.9433   0.12757   0.12446   0.0057   1.0000   0.0095
 -17.750  -0.9607   0.11939   0.11613   0.0010   1.0000   0.0095
 -17.500  -0.9737   0.11231   0.10891  -0.0032   1.0000   0.0095
 -17.250  -0.9865   0.10562   0.10208  -0.0069   1.0000   0.0095
 -17.000  -0.9991   0.09905   0.09536  -0.0106   1.0000   0.0095
 -16.750  -1.0092   0.09318   0.08935  -0.0138   1.0000   0.0096
 -16.500  -1.0189   0.08753   0.08355  -0.0168   1.0000   0.0096
 -16.250  -1.0260   0.08263   0.07852  -0.0191   1.0000   0.0096
 -16.000  -1.0330   0.07784   0.07360  -0.0213   1.0000   0.0096
 -15.750  -1.0382   0.07345   0.06909  -0.0233   1.0000   0.0096
 -15.500  -1.0432   0.06912   0.06462  -0.0254   1.0000   0.0098
 -15.250  -1.0466   0.06525   0.06063  -0.0269   1.0000   0.0098
 -15.000  -1.0505   0.06147   0.05673  -0.0282   1.0000   0.0099
 -14.750  -1.0519   0.05821   0.05336  -0.0291   1.0000   0.0099
 -14.500  -1.0633   0.05407   0.04913  -0.0293   1.0000   0.0103
 -14.250  -1.0649   0.05096   0.04593  -0.0300   1.0000   0.0103
 -14.000  -1.0671   0.04783   0.04273  -0.0307   1.0000   0.0105
 -13.750  -1.0684   0.04485   0.03967  -0.0313   1.0000   0.0107
 -13.500  -1.0685   0.04208   0.03683  -0.0317   1.0000   0.0109
 -13.250  -1.0686   0.03941   0.03406  -0.0319   1.0000   0.0109
 -13.000  -1.0667   0.03699   0.03157  -0.0321   1.0000   0.0114
 -12.750  -1.0643   0.03473   0.02922  -0.0320   1.0000   0.0117
 -12.500  -1.0624   0.03251   0.02691  -0.0317   1.0000   0.0119
 -12.250  -1.0608   0.03039   0.02470  -0.0312   1.0000   0.0122
 -12.000  -1.0562   0.02865   0.02287  -0.0304   1.0000   0.0125
 -11.750  -1.0502   0.02716   0.02128  -0.0294   1.0000   0.0129
 -11.500  -1.0503   0.02538   0.01941  -0.0278   1.0000   0.0132
 -11.250  -1.0564   0.02348   0.01743  -0.0250   1.0000   0.0139
 -11.000  -1.0529   0.02233   0.01623  -0.0225   1.0000   0.0145
 -10.750  -1.0461   0.02146   0.01530  -0.0199   1.0000   0.0152
 -10.500  -1.0378   0.02071   0.01449  -0.0173   1.0000   0.0160
 -10.250  -1.0244   0.02003   0.01373  -0.0154   1.0000   0.0170
 -10.000  -1.0185   0.01879   0.01244  -0.0125   1.0000   0.0186
  -9.750  -1.0040   0.01803   0.01163  -0.0107   1.0000   0.0204
  -9.500  -0.9885   0.01729   0.01082  -0.0090   1.0000   0.0227
  -9.250  -0.9737   0.01647   0.01000  -0.0071   1.0000   0.0264
  -9.000  -0.9579   0.01570   0.00923  -0.0054   1.0000   0.0326
  -8.750  -0.9422   0.01494   0.00853  -0.0036   1.0000   0.0444
  -8.500  -0.9271   0.01413   0.00786  -0.0017   1.0000   0.0633
  -8.250  -0.9107   0.01344   0.00729   0.0000   1.0000   0.0844
  -8.000  -0.8932   0.01285   0.00681   0.0016   1.0000   0.1061
  -7.750  -0.8755   0.01229   0.00637   0.0032   1.0000   0.1289
  -7.500  -0.8576   0.01178   0.00597   0.0048   1.0000   0.1519
  -7.250  -0.8393   0.01136   0.00564   0.0063   1.0000   0.1742
  -7.000  -0.8221   0.01094   0.00533   0.0081   1.0000   0.1968
  -6.750  -0.7910   0.01055   0.00503   0.0070   0.9970   0.2216
  -6.500  -0.7523   0.01019   0.00474   0.0043   0.9914   0.2469
  -6.250  -0.7141   0.00984   0.00448   0.0019   0.9845   0.2744
  -6.000  -0.6777   0.00951   0.00424  -0.0001   0.9754   0.2978
  -5.750  -0.6405   0.00927   0.00402  -0.0022   0.9652   0.3167
  -5.500  -0.6029   0.00905   0.00380  -0.0042   0.9530   0.3335
  -5.250  -0.5679   0.00883   0.00360  -0.0057   0.9363   0.3504
  -5.000  -0.5371   0.00868   0.00342  -0.0062   0.9150   0.3653
  -4.750  -0.5099   0.00858   0.00326  -0.0059   0.8929   0.3784
  -4.500  -0.4844   0.00848   0.00311  -0.0053   0.8707   0.3910
  -4.250  -0.4588   0.00840   0.00298  -0.0047   0.8509   0.4031
  -4.000  -0.4329   0.00833   0.00285  -0.0041   0.8325   0.4154
  -3.750  -0.4066   0.00827   0.00274  -0.0037   0.8151   0.4274
  -3.500  -0.3801   0.00822   0.00263  -0.0033   0.7986   0.4396
  -3.250  -0.3535   0.00816   0.00253  -0.0030   0.7832   0.4515
  -3.000  -0.3269   0.00810   0.00244  -0.0026   0.7684   0.4631
  -2.750  -0.3000   0.00805   0.00235  -0.0023   0.7542   0.4747
  -2.500  -0.2730   0.00801   0.00227  -0.0021   0.7403   0.4866
  -2.000  -0.2188   0.00793   0.00215  -0.0016   0.7132   0.5110
  -1.750  -0.1916   0.00788   0.00209  -0.0014   0.7000   0.5230
  -1.500  -0.1643   0.00785   0.00205  -0.0012   0.6870   0.5352
  -1.250  -0.1369   0.00783   0.00201  -0.0010   0.6742   0.5475
  -1.000  -0.1095   0.00782   0.00197  -0.0008   0.6616   0.5601
  -0.750  -0.0822   0.00780   0.00194  -0.0006   0.6489   0.5727
  -0.500  -0.0549   0.00778   0.00193  -0.0004   0.6361   0.5851
  -0.250  -0.0275   0.00776   0.00192  -0.0002   0.6230   0.5975
   0.000   0.0000   0.00776   0.00192   0.0000   0.6102   0.6102
   0.250   0.0275   0.00776   0.00192   0.0002   0.5976   0.6230
   0.500   0.0549   0.00778   0.00193   0.0004   0.5851   0.6361
   0.750   0.0822   0.00780   0.00194   0.0006   0.5726   0.6489
   1.000   0.1095   0.00782   0.00197   0.0008   0.5601   0.6616
   1.250   0.1369   0.00783   0.00201   0.0010   0.5474   0.6742
   1.500   0.1643   0.00785   0.00205   0.0012   0.5352   0.6870
   1.750   0.1915   0.00788   0.00209   0.0014   0.5230   0.7000
   2.000   0.2187   0.00793   0.00215   0.0016   0.5110   0.7133
   2.500   0.2730   0.00801   0.00227   0.0021   0.4866   0.7402
   2.750   0.3000   0.00805   0.00235   0.0023   0.4748   0.7541
   3.000   0.3269   0.00810   0.00244   0.0026   0.4631   0.7683
   3.250   0.3535   0.00816   0.00253   0.0030   0.4515   0.7833
   3.500   0.3800   0.00822   0.00263   0.0033   0.4396   0.7987
   3.750   0.4066   0.00827   0.00274   0.0037   0.4274   0.8152
   4.000   0.4329   0.00833   0.00285   0.0041   0.4154   0.8325
   4.250   0.4588   0.00840   0.00298   0.0047   0.4032   0.8509
   4.500   0.4844   0.00848   0.00311   0.0053   0.3910   0.8708
   4.750   0.5099   0.00858   0.00326   0.0059   0.3785   0.8928
   5.000   0.5370   0.00868   0.00342   0.0063   0.3652   0.9151
   5.250   0.5679   0.00883   0.00360   0.0057   0.3505   0.9363
   5.500   0.6029   0.00905   0.00380   0.0042   0.3336   0.9530
   5.750   0.6404   0.00927   0.00402   0.0022   0.3169   0.9652
   6.000   0.6777   0.00951   0.00424   0.0001   0.2980   0.9754
   6.250   0.7141   0.00983   0.00448  -0.0019   0.2743   0.9845
   6.500   0.7522   0.01019   0.00474  -0.0043   0.2469   0.9914
   6.750   0.7910   0.01054   0.00503  -0.0070   0.2219   0.9970
   7.000   0.8221   0.01094   0.00533  -0.0081   0.1970   1.0000
   7.250   0.8394   0.01135   0.00563  -0.0063   0.1746   1.0000
   7.500   0.8576   0.01178   0.00597  -0.0048   0.1518   1.0000
   7.750   0.8755   0.01229   0.00637  -0.0032   0.1287   1.0000
   8.000   0.8931   0.01286   0.00681  -0.0016   0.1058   1.0000
   8.250   0.9107   0.01344   0.00729   0.0000   0.0846   1.0000
   8.500   0.9271   0.01413   0.00785   0.0017   0.0634   1.0000
   8.750   0.9421   0.01494   0.00853   0.0036   0.0443   1.0000
   9.000   0.9579   0.01570   0.00923   0.0054   0.0326   1.0000
   9.250   0.9737   0.01646   0.01000   0.0071   0.0265   1.0000
   9.500   0.9883   0.01730   0.01083   0.0090   0.0226   1.0000
   9.750   1.0041   0.01802   0.01163   0.0107   0.0205   1.0000
  10.000   1.0189   0.01877   0.01242   0.0125   0.0187   1.0000
  10.250   1.0249   0.02001   0.01371   0.0153   0.0169   1.0000
  10.500   1.0378   0.02072   0.01450   0.0173   0.0160   1.0000
  10.750   1.0462   0.02148   0.01531   0.0199   0.0150   1.0000
  11.000   1.0535   0.02232   0.01621   0.0224   0.0142   1.0000
  11.250   1.0555   0.02355   0.01750   0.0251   0.0137   1.0000
  11.500   1.0498   0.02544   0.01947   0.0277   0.0131   1.0000
  11.750   1.0512   0.02712   0.02125   0.0293   0.0129   1.0000
  12.000   1.0570   0.02864   0.02286   0.0303   0.0125   1.0000
  12.250   1.0600   0.03051   0.02482   0.0311   0.0123   1.0000
  12.500   1.0643   0.03239   0.02679   0.0316   0.0119   1.0000
  12.750   1.0654   0.03467   0.02917   0.0319   0.0117   1.0000
  13.000   1.0679   0.03695   0.03153   0.0320   0.0113   1.0000
  13.250   1.0690   0.03943   0.03410   0.0319   0.0112   1.0000
  13.500   1.0712   0.04191   0.03663   0.0315   0.0107   1.0000
  13.750   1.0698   0.04480   0.03962   0.0312   0.0107   1.0000
  14.000   1.0695   0.04766   0.04256   0.0306   0.0106   1.0000
  14.250   1.0670   0.05082   0.04580   0.0299   0.0104   1.0000
  14.500   1.0633   0.05415   0.04921   0.0293   0.0102   1.0000
  14.750   1.0611   0.05739   0.05254   0.0285   0.0101   1.0000
  15.000   1.0521   0.06139   0.05665   0.0280   0.0099   1.0000
  15.250   1.0483   0.06518   0.06056   0.0267   0.0098   1.0000
  15.500   1.0445   0.06912   0.06463   0.0251   0.0097   1.0000
  15.750   1.0398   0.07330   0.06893   0.0233   0.0097   1.0000
  16.000   1.0346   0.07774   0.07350   0.0212   0.0096   1.0000
  16.250   1.0273   0.08269   0.07859   0.0188   0.0095   1.0000
  16.500   1.0203   0.08767   0.08370   0.0162   0.0095   1.0000
  16.750   1.0105   0.09321   0.08939   0.0135   0.0095   1.0000
  17.000   0.9995   0.09932   0.09564   0.0101   0.0094   1.0000
  17.250   0.9882   0.10564   0.10210   0.0066   0.0094   1.0000
  17.500   0.9728   0.11297   0.10960   0.0024   0.0093   1.0000
  17.750   0.9606   0.11978   0.11653  -0.0014   0.0094   1.0000
  18.000   0.9459   0.12719   0.12407  -0.0056   0.0096   1.0000
  18.250   0.9281   0.13581   0.13283  -0.0108   0.0096   1.0000
  18.500   0.9096   0.14511   0.14228  -0.0164   0.0096   1.0000
  18.750   0.8814   0.15695   0.15428  -0.0233   0.0098   1.0000
  19.000   0.8652   0.16663   0.16407  -0.0290   0.0099   1.0000
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