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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 500,000
Max Cl/Cd: 70.38 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1046-il-500000-n5.txt
Download as CSV file: xf-s1046-il-500000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.0784   0.10224   0.09759  -0.0114   1.0000   0.0124
 -18.250  -1.0879   0.09702   0.09229  -0.0138   1.0000   0.0126
 -18.000  -1.0974   0.09191   0.08709  -0.0162   1.0000   0.0130
 -17.750  -1.1065   0.08697   0.08206  -0.0184   1.0000   0.0133
 -17.500  -1.1143   0.08228   0.07728  -0.0204   1.0000   0.0136
 -17.250  -1.1217   0.07777   0.07268  -0.0222   1.0000   0.0140
 -17.000  -1.1283   0.07346   0.06828  -0.0240   1.0000   0.0144
 -16.750  -1.1343   0.06929   0.06402  -0.0256   1.0000   0.0148
 -16.500  -1.1393   0.06536   0.05999  -0.0270   1.0000   0.0152
 -16.250  -1.1460   0.06131   0.05586  -0.0284   1.0000   0.0155
 -16.000  -1.1523   0.05741   0.05188  -0.0297   1.0000   0.0161
 -15.750  -1.1564   0.05389   0.04828  -0.0307   1.0000   0.0167
 -15.500  -1.1602   0.05051   0.04482  -0.0316   1.0000   0.0174
 -15.250  -1.1622   0.04743   0.04166  -0.0323   1.0000   0.0180
 -15.000  -1.1654   0.04436   0.03852  -0.0329   1.0000   0.0192
 -14.750  -1.1668   0.04156   0.03565  -0.0333   1.0000   0.0200
 -14.500  -1.1679   0.03889   0.03292  -0.0335   1.0000   0.0216
 -14.250  -1.1668   0.03651   0.03047  -0.0335   1.0000   0.0227
 -14.000  -1.1668   0.03411   0.02802  -0.0334   1.0000   0.0247
 -13.750  -1.1641   0.03204   0.02591  -0.0331   1.0000   0.0267
 -13.500  -1.1618   0.03001   0.02384  -0.0327   1.0000   0.0291
 -13.250  -1.1579   0.02821   0.02200  -0.0321   1.0000   0.0320
 -13.000  -1.1538   0.02651   0.02028  -0.0313   1.0000   0.0352
 -12.750  -1.1478   0.02504   0.01877  -0.0304   1.0000   0.0386
 -12.500  -1.1424   0.02362   0.01734  -0.0293   1.0000   0.0423
 -12.250  -1.1354   0.02240   0.01609  -0.0280   1.0000   0.0469
 -12.000  -1.1294   0.02122   0.01491  -0.0264   1.0000   0.0514
 -11.750  -1.1215   0.02025   0.01392  -0.0247   1.0000   0.0567
 -11.500  -1.1150   0.01929   0.01298  -0.0226   1.0000   0.0632
 -11.250  -1.1070   0.01849   0.01220  -0.0204   1.0000   0.0692
 -11.000  -1.0981   0.01782   0.01153  -0.0180   1.0000   0.0762
 -10.750  -1.0915   0.01714   0.01089  -0.0150   1.0000   0.0843
 -10.500  -1.0823   0.01659   0.01036  -0.0122   1.0000   0.0917
 -10.250  -1.0690   0.01607   0.00986  -0.0101   1.0000   0.1004
 -10.000  -1.0557   0.01553   0.00936  -0.0080   1.0000   0.1096
  -9.750  -1.0409   0.01506   0.00893  -0.0061   1.0000   0.1178
  -9.500  -1.0117   0.01454   0.00843  -0.0070   0.9855   0.1286
  -9.250  -0.9765   0.01394   0.00789  -0.0093   0.9571   0.1438
  -9.000  -0.9402   0.01336   0.00736  -0.0116   0.9271   0.1612
  -8.750  -0.9147   0.01299   0.00695  -0.0115   0.8946   0.1739
  -8.500  -0.8930   0.01275   0.00663  -0.0104   0.8678   0.1842
  -8.250  -0.8718   0.01248   0.00631  -0.0093   0.8457   0.1936
  -8.000  -0.8493   0.01227   0.00603  -0.0083   0.8270   0.2017
  -7.750  -0.8262   0.01205   0.00576  -0.0075   0.8108   0.2113
  -7.500  -0.8029   0.01181   0.00549  -0.0068   0.7959   0.2214
  -7.250  -0.7787   0.01161   0.00525  -0.0062   0.7825   0.2310
  -7.000  -0.7542   0.01142   0.00502  -0.0056   0.7701   0.2407
  -6.500  -0.7039   0.01108   0.00459  -0.0047   0.7470   0.2576
  -6.250  -0.6786   0.01089   0.00439  -0.0042   0.7367   0.2660
  -6.000  -0.6525   0.01077   0.00421  -0.0039   0.7262   0.2738
  -5.750  -0.6267   0.01059   0.00402  -0.0035   0.7164   0.2822
  -5.250  -0.5741   0.01032   0.00369  -0.0030   0.6972   0.2991
  -5.000  -0.5474   0.01021   0.00354  -0.0027   0.6879   0.3069
  -4.750  -0.5209   0.01007   0.00340  -0.0025   0.6787   0.3156
  -4.500  -0.4939   0.00996   0.00326  -0.0023   0.6695   0.3235
  -4.250  -0.4671   0.00986   0.00313  -0.0021   0.6604   0.3320
  -4.000  -0.4400   0.00975   0.00301  -0.0019   0.6509   0.3404
  -3.750  -0.4129   0.00966   0.00290  -0.0017   0.6417   0.3488
  -3.500  -0.3856   0.00956   0.00279  -0.0016   0.6317   0.3572
  -3.250  -0.3583   0.00949   0.00269  -0.0014   0.6221   0.3663
  -3.000  -0.3311   0.00940   0.00260  -0.0013   0.6117   0.3748
  -2.750  -0.3034   0.00934   0.00251  -0.0012   0.6015   0.3840
  -2.500  -0.2763   0.00926   0.00243  -0.0010   0.5913   0.3932
  -2.250  -0.2486   0.00921   0.00236  -0.0009   0.5804   0.4022
  -2.000  -0.2212   0.00915   0.00230  -0.0008   0.5699   0.4116
  -1.750  -0.1936   0.00912   0.00224  -0.0007   0.5594   0.4204
  -1.500  -0.1660   0.00908   0.00219  -0.0006   0.5487   0.4304
  -1.250  -0.1384   0.00904   0.00215  -0.0005   0.5385   0.4395
  -1.000  -0.1107   0.00903   0.00212  -0.0004   0.5281   0.4490
  -0.750  -0.0831   0.00900   0.00209  -0.0003   0.5179   0.4589
  -0.500  -0.0554   0.00899   0.00208  -0.0002   0.5077   0.4680
  -0.250  -0.0278   0.00899   0.00206  -0.0001   0.4976   0.4781
   0.000   0.0000   0.00897   0.00206   0.0000   0.4879   0.4878
   0.250   0.0278   0.00899   0.00206   0.0001   0.4781   0.4976
   0.500   0.0554   0.00899   0.00208   0.0002   0.4680   0.5077
   0.750   0.0831   0.00900   0.00209   0.0003   0.4589   0.5178
   1.250   0.1384   0.00904   0.00215   0.0005   0.4395   0.5384
   1.500   0.1660   0.00908   0.00219   0.0006   0.4305   0.5488
   1.750   0.1937   0.00912   0.00224   0.0007   0.4206   0.5595
   2.000   0.2212   0.00915   0.00230   0.0008   0.4117   0.5698
   2.250   0.2487   0.00921   0.00236   0.0009   0.4023   0.5803
   2.500   0.2763   0.00926   0.00243   0.0010   0.3931   0.5913
   2.750   0.3034   0.00934   0.00251   0.0012   0.3840   0.6014
   3.000   0.3311   0.00940   0.00260   0.0013   0.3748   0.6117
   3.250   0.3583   0.00949   0.00269   0.0014   0.3663   0.6220
   3.500   0.3856   0.00956   0.00279   0.0016   0.3573   0.6317
   3.750   0.4129   0.00966   0.00290   0.0017   0.3490   0.6417
   4.000   0.4400   0.00975   0.00301   0.0019   0.3404   0.6509
   4.250   0.4672   0.00986   0.00313   0.0021   0.3320   0.6603
   4.500   0.4939   0.00996   0.00326   0.0023   0.3235   0.6695
   4.750   0.5209   0.01007   0.00340   0.0025   0.3157   0.6787
   5.000   0.5474   0.01021   0.00354   0.0027   0.3069   0.6881
   5.250   0.5741   0.01032   0.00369   0.0030   0.2989   0.6971
   5.750   0.6267   0.01059   0.00402   0.0035   0.2820   0.7163
   6.000   0.6525   0.01077   0.00421   0.0039   0.2738   0.7263
   6.250   0.6786   0.01089   0.00439   0.0042   0.2659   0.7367
   6.500   0.7039   0.01108   0.00459   0.0047   0.2577   0.7470
   7.000   0.7543   0.01142   0.00502   0.0056   0.2408   0.7701
   7.250   0.7787   0.01161   0.00525   0.0062   0.2311   0.7826
   7.500   0.8030   0.01181   0.00549   0.0068   0.2213   0.7958
   7.750   0.8262   0.01205   0.00576   0.0075   0.2115   0.8107
   8.000   0.8494   0.01226   0.00603   0.0083   0.2019   0.8270
   8.250   0.8719   0.01248   0.00631   0.0093   0.1936   0.8457
   8.750   0.9145   0.01301   0.00696   0.0115   0.1730   0.8943
   9.000   0.9403   0.01336   0.00735   0.0116   0.1613   0.9270
   9.250   0.9766   0.01394   0.00789   0.0092   0.1437   0.9571
   9.500   1.0118   0.01454   0.00843   0.0070   0.1286   0.9856
   9.750   1.0410   0.01506   0.00892   0.0061   0.1180   1.0000
  10.000   1.0557   0.01553   0.00936   0.0080   0.1090   1.0000
  10.250   1.0691   0.01607   0.00986   0.0101   0.1002   1.0000
  10.500   1.0828   0.01658   0.01035   0.0122   0.0921   1.0000
  10.750   1.0919   0.01714   0.01089   0.0149   0.0844   1.0000
  11.000   1.0985   0.01781   0.01152   0.0179   0.0762   1.0000
  11.250   1.1076   0.01848   0.01219   0.0203   0.0693   1.0000
  11.500   1.1155   0.01928   0.01297   0.0225   0.0631   1.0000
  11.750   1.1221   0.02024   0.01391   0.0246   0.0567   1.0000
  12.000   1.1306   0.02118   0.01487   0.0263   0.0519   1.0000
  12.250   1.1362   0.02238   0.01607   0.0279   0.0470   1.0000
  12.500   1.1433   0.02359   0.01731   0.0292   0.0424   1.0000
  12.750   1.1487   0.02501   0.01875   0.0303   0.0388   1.0000
  13.000   1.1546   0.02649   0.02025   0.0312   0.0351   1.0000
  13.250   1.1588   0.02819   0.02198   0.0320   0.0319   1.0000
  13.500   1.1632   0.02995   0.02378   0.0326   0.0293   1.0000
  13.750   1.1653   0.03200   0.02586   0.0330   0.0267   1.0000
  14.000   1.1678   0.03409   0.02800   0.0333   0.0245   1.0000
  14.250   1.1685   0.03643   0.03039   0.0334   0.0229   1.0000
  14.500   1.1694   0.03883   0.03286   0.0333   0.0215   1.0000
  14.750   1.1696   0.04138   0.03548   0.0331   0.0204   1.0000
  15.000   1.1655   0.04446   0.03861   0.0327   0.0188   1.0000
  15.250   1.1640   0.04735   0.04158   0.0322   0.0182   1.0000
  15.500   1.1623   0.05039   0.04470   0.0315   0.0175   1.0000
  15.750   1.1585   0.05377   0.04816   0.0306   0.0167   1.0000
  16.000   1.1536   0.05740   0.05186   0.0295   0.0160   1.0000
  16.250   1.1479   0.06123   0.05577   0.0282   0.0155   1.0000
  16.500   1.1418   0.06522   0.05984   0.0268   0.0150   1.0000
  16.750   1.1365   0.06918   0.06390   0.0254   0.0147   1.0000
  17.000   1.1309   0.07329   0.06810   0.0238   0.0142   1.0000
  17.250   1.1237   0.07768   0.07259   0.0220   0.0139   1.0000
  17.500   1.1162   0.08222   0.07722   0.0201   0.0135   1.0000
  17.750   1.1081   0.08695   0.08204   0.0181   0.0132   1.0000
  18.000   1.0986   0.09197   0.08715   0.0159   0.0128   1.0000
  18.250   1.0896   0.09700   0.09226   0.0136   0.0126   1.0000
  18.500   1.0809   0.10210   0.09745   0.0112   0.0124   1.0000
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