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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 500,000
Max Cl/Cd: 66.11 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1048-il-500000-n5.txt
Download as CSV file: xf-s1048-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.0292   0.10081   0.09684  -0.0050   1.0000   0.0051
 -17.000  -1.0396   0.09500   0.09093  -0.0079   1.0000   0.0051
 -16.750  -1.0491   0.08949   0.08532  -0.0106   1.0000   0.0051
 -16.500  -1.0590   0.08401   0.07973  -0.0133   1.0000   0.0052
 -16.250  -1.0678   0.07885   0.07446  -0.0158   1.0000   0.0052
 -16.000  -1.0756   0.07399   0.06949  -0.0180   1.0000   0.0052
 -15.750  -1.0850   0.06902   0.06441  -0.0203   1.0000   0.0053
 -15.500  -1.0930   0.06441   0.05968  -0.0223   1.0000   0.0053
 -15.250  -1.1006   0.06000   0.05516  -0.0241   1.0000   0.0054
 -15.000  -1.1060   0.05605   0.05110  -0.0256   1.0000   0.0054
 -14.750  -1.1124   0.05209   0.04703  -0.0271   1.0000   0.0054
 -14.500  -1.1201   0.04808   0.04291  -0.0284   1.0000   0.0055
 -14.250  -1.1274   0.04426   0.03898  -0.0295   1.0000   0.0056
 -14.000  -1.1327   0.04081   0.03542  -0.0304   1.0000   0.0057
 -13.750  -1.1358   0.03776   0.03228  -0.0309   1.0000   0.0059
 -13.500  -1.1360   0.03515   0.02956  -0.0311   1.0000   0.0059
 -13.250  -1.1352   0.03277   0.02710  -0.0311   1.0000   0.0063
 -13.000  -1.1320   0.03076   0.02500  -0.0308   1.0000   0.0063
 -12.750  -1.1282   0.02892   0.02308  -0.0302   1.0000   0.0065
 -12.500  -1.1237   0.02729   0.02135  -0.0294   1.0000   0.0068
 -12.250  -1.1187   0.02583   0.01980  -0.0282   1.0000   0.0070
 -12.000  -1.1121   0.02459   0.01848  -0.0268   1.0000   0.0073
 -11.750  -1.1057   0.02346   0.01727  -0.0250   1.0000   0.0076
 -11.500  -1.0978   0.02252   0.01625  -0.0231   1.0000   0.0078
 -11.250  -1.0906   0.02162   0.01528  -0.0207   1.0000   0.0082
 -11.000  -1.0837   0.02079   0.01440  -0.0180   1.0000   0.0089
 -10.750  -1.0725   0.02011   0.01369  -0.0158   1.0000   0.0097
 -10.500  -1.0578   0.01946   0.01298  -0.0141   1.0000   0.0105
 -10.250  -1.0419   0.01884   0.01229  -0.0126   1.0000   0.0116
 -10.000  -1.0264   0.01816   0.01157  -0.0110   1.0000   0.0129
  -9.750  -1.0089   0.01758   0.01096  -0.0096   1.0000   0.0144
  -9.500  -0.9909   0.01703   0.01036  -0.0082   1.0000   0.0161
  -9.250  -0.9729   0.01646   0.00978  -0.0068   1.0000   0.0184
  -9.000  -0.9538   0.01596   0.00925  -0.0055   1.0000   0.0209
  -8.750  -0.9354   0.01542   0.00872  -0.0041   1.0000   0.0254
  -8.500  -0.9173   0.01487   0.00819  -0.0027   1.0000   0.0322
  -8.250  -0.8991   0.01433   0.00770  -0.0012   1.0000   0.0414
  -8.000  -0.8808   0.01382   0.00724   0.0003   1.0000   0.0522
  -7.750  -0.8558   0.01325   0.00674   0.0003   0.9964   0.0678
  -7.500  -0.8242   0.01261   0.00622  -0.0011   0.9865   0.0899
  -7.250  -0.7929   0.01199   0.00573  -0.0024   0.9722   0.1157
  -7.000  -0.7580   0.01147   0.00530  -0.0043   0.9551   0.1391
  -6.750  -0.7223   0.01106   0.00492  -0.0062   0.9341   0.1593
  -6.500  -0.6923   0.01063   0.00456  -0.0069   0.9081   0.1856
  -6.250  -0.6678   0.01029   0.00425  -0.0064   0.8813   0.2115
  -6.000  -0.6437   0.01003   0.00399  -0.0057   0.8575   0.2326
  -5.750  -0.6190   0.00986   0.00377  -0.0050   0.8362   0.2470
  -5.500  -0.5940   0.00968   0.00356  -0.0045   0.8168   0.2631
  -5.250  -0.5689   0.00950   0.00336  -0.0040   0.7988   0.2812
  -5.000  -0.5432   0.00936   0.00317  -0.0035   0.7822   0.2963
  -4.750  -0.5171   0.00923   0.00301  -0.0032   0.7664   0.3096
  -4.500  -0.4908   0.00911   0.00286  -0.0028   0.7516   0.3225
  -4.250  -0.4642   0.00901   0.00272  -0.0026   0.7374   0.3348
  -4.000  -0.4376   0.00891   0.00258  -0.0023   0.7238   0.3476
  -3.750  -0.4107   0.00883   0.00246  -0.0021   0.7107   0.3600
  -3.500  -0.3839   0.00874   0.00234  -0.0019   0.6979   0.3718
  -3.250  -0.3569   0.00866   0.00223  -0.0016   0.6854   0.3831
  -3.000  -0.3297   0.00859   0.00214  -0.0015   0.6730   0.3942
  -2.750  -0.3023   0.00853   0.00205  -0.0013   0.6608   0.4053
  -2.500  -0.2750   0.00847   0.00197  -0.0012   0.6487   0.4164
  -2.250  -0.2477   0.00841   0.00189  -0.0010   0.6367   0.4276
  -2.000  -0.2203   0.00837   0.00183  -0.0009   0.6247   0.4385
  -1.750  -0.1928   0.00833   0.00177  -0.0008   0.6123   0.4498
  -1.500  -0.1653   0.00829   0.00172  -0.0007   0.6001   0.4610
  -1.250  -0.1378   0.00825   0.00168  -0.0005   0.5880   0.4719
  -1.000  -0.1102   0.00823   0.00164  -0.0004   0.5762   0.4830
  -0.750  -0.0827   0.00822   0.00161  -0.0003   0.5640   0.4941
  -0.250  -0.0276   0.00819   0.00158  -0.0001   0.5401   0.5170
   0.000   0.0000   0.00819   0.00158   0.0000   0.5286   0.5285
   0.250   0.0276   0.00819   0.00158   0.0001   0.5170   0.5401
   0.750   0.0827   0.00822   0.00161   0.0003   0.4942   0.5641
   1.000   0.1102   0.00823   0.00164   0.0004   0.4831   0.5761
   1.250   0.1378   0.00825   0.00168   0.0005   0.4719   0.5880
   1.500   0.1653   0.00829   0.00172   0.0007   0.4611   0.6002
   1.750   0.1927   0.00833   0.00177   0.0008   0.4496   0.6123
   2.000   0.2203   0.00837   0.00183   0.0009   0.4385   0.6246
   2.250   0.2477   0.00841   0.00189   0.0010   0.4275   0.6365
   2.500   0.2750   0.00847   0.00197   0.0012   0.4163   0.6487
   2.750   0.3022   0.00853   0.00205   0.0013   0.4051   0.6606
   3.000   0.3296   0.00859   0.00214   0.0015   0.3940   0.6730
   3.250   0.3569   0.00866   0.00223   0.0016   0.3831   0.6854
   3.500   0.3838   0.00874   0.00234   0.0019   0.3716   0.6979
   3.750   0.4107   0.00883   0.00246   0.0021   0.3600   0.7108
   4.000   0.4375   0.00891   0.00258   0.0023   0.3476   0.7239
   4.250   0.4642   0.00901   0.00272   0.0026   0.3349   0.7374
   4.500   0.4908   0.00912   0.00286   0.0028   0.3224   0.7516
   4.750   0.5171   0.00923   0.00301   0.0032   0.3099   0.7665
   5.000   0.5432   0.00936   0.00317   0.0035   0.2962   0.7821
   5.250   0.5689   0.00950   0.00336   0.0040   0.2810   0.7988
   5.500   0.5940   0.00968   0.00356   0.0045   0.2632   0.8169
   6.000   0.6437   0.01004   0.00399   0.0057   0.2323   0.8573
   6.250   0.6677   0.01028   0.00424   0.0064   0.2117   0.8813
   6.500   0.6923   0.01063   0.00456   0.0069   0.1857   0.9081
   6.750   0.7223   0.01106   0.00492   0.0062   0.1590   0.9342
   7.000   0.7580   0.01147   0.00530   0.0043   0.1389   0.9551
   7.250   0.7927   0.01199   0.00573   0.0024   0.1156   0.9721
   7.500   0.8242   0.01260   0.00622   0.0011   0.0908   0.9864
   7.750   0.8557   0.01324   0.00674  -0.0003   0.0682   0.9962
   8.000   0.8808   0.01382   0.00724  -0.0003   0.0520   1.0000
   8.250   0.8991   0.01433   0.00770   0.0012   0.0413   1.0000
   8.500   0.9173   0.01487   0.00819   0.0027   0.0323   1.0000
   8.750   0.9354   0.01542   0.00872   0.0042   0.0253   1.0000
   9.000   0.9539   0.01595   0.00924   0.0055   0.0211   1.0000
   9.250   0.9728   0.01646   0.00977   0.0068   0.0184   1.0000
   9.500   0.9909   0.01702   0.01035   0.0082   0.0162   1.0000
   9.750   1.0089   0.01758   0.01096   0.0096   0.0145   1.0000
  10.000   1.0264   0.01816   0.01157   0.0110   0.0129   1.0000
  10.250   1.0421   0.01883   0.01227   0.0125   0.0117   1.0000
  10.500   1.0578   0.01946   0.01297   0.0141   0.0105   1.0000
  10.750   1.0726   0.02010   0.01367   0.0158   0.0096   1.0000
  11.000   1.0836   0.02079   0.01441   0.0180   0.0090   1.0000
  11.250   1.0908   0.02161   0.01527   0.0207   0.0082   1.0000
  11.500   1.0979   0.02252   0.01624   0.0231   0.0079   1.0000
  11.750   1.1057   0.02346   0.01727   0.0250   0.0075   1.0000
  12.000   1.1126   0.02456   0.01845   0.0267   0.0074   1.0000
  12.250   1.1186   0.02583   0.01980   0.0282   0.0070   1.0000
  12.500   1.1246   0.02723   0.02128   0.0293   0.0067   1.0000
  12.750   1.1288   0.02889   0.02305   0.0302   0.0066   1.0000
  13.000   1.1325   0.03073   0.02497   0.0308   0.0062   1.0000
  13.250   1.1352   0.03280   0.02713   0.0310   0.0062   1.0000
  13.500   1.1364   0.03514   0.02955   0.0311   0.0060   1.0000
  13.750   1.1353   0.03784   0.03236   0.0308   0.0059   1.0000
  14.000   1.1336   0.04075   0.03537   0.0303   0.0058   1.0000
  14.250   1.1267   0.04439   0.03911   0.0294   0.0056   1.0000
  14.500   1.1215   0.04796   0.04280   0.0284   0.0055   1.0000
  14.750   1.1122   0.05219   0.04713   0.0269   0.0054   1.0000
  15.000   1.1093   0.05570   0.05075   0.0256   0.0054   1.0000
  15.250   1.1027   0.05979   0.05494   0.0241   0.0053   1.0000
  15.500   1.0949   0.06424   0.05951   0.0222   0.0053   1.0000
  15.750   1.0855   0.06906   0.06444   0.0201   0.0053   1.0000
  16.000   1.0781   0.07375   0.06925   0.0180   0.0052   1.0000
  16.250   1.0705   0.07858   0.07419   0.0157   0.0051   1.0000
  16.500   1.0599   0.08403   0.07975   0.0131   0.0051   1.0000
  16.750   1.0506   0.08941   0.08523   0.0105   0.0051   1.0000
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