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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 100,000
Max Cl/Cd: 40.45 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1046-il-100000-n5.txt
Download as CSV file: xf-s1046-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9380   0.09365   0.08714  -0.0177   1.0000   0.0644
 -16.000  -0.9444   0.08909   0.08256  -0.0197   1.0000   0.0676
 -15.750  -0.9519   0.08445   0.07788  -0.0218   1.0000   0.0708
 -15.500  -0.9602   0.07966   0.07298  -0.0239   1.0000   0.0749
 -15.250  -0.9679   0.07521   0.06849  -0.0257   1.0000   0.0787
 -15.000  -0.9768   0.07071   0.06395  -0.0276   1.0000   0.0826
 -14.750  -0.9836   0.06656   0.05967  -0.0291   1.0000   0.0871
 -14.500  -0.9913   0.06255   0.05564  -0.0305   1.0000   0.0912
 -14.250  -0.9988   0.05868   0.05171  -0.0318   1.0000   0.0958
 -14.000  -1.0043   0.05516   0.04806  -0.0328   1.0000   0.1013
 -13.750  -1.0115   0.05168   0.04458  -0.0337   1.0000   0.1060
 -13.500  -1.0160   0.04852   0.04129  -0.0343   1.0000   0.1123
 -13.250  -1.0212   0.04553   0.03830  -0.0347   1.0000   0.1179
 -13.000  -1.0243   0.04281   0.03549  -0.0348   1.0000   0.1248
 -12.750  -1.0272   0.04030   0.03296  -0.0347   1.0000   0.1314
 -12.500  -1.0285   0.03802   0.03059  -0.0344   1.0000   0.1396
 -12.250  -1.0300   0.03595   0.02853  -0.0338   1.0000   0.1469
 -12.000  -1.0288   0.03415   0.02663  -0.0329   1.0000   0.1556
 -11.750  -1.0283   0.03252   0.02501  -0.0317   1.0000   0.1632
 -11.500  -1.0250   0.03113   0.02355  -0.0303   1.0000   0.1715
 -11.250  -1.0217   0.02990   0.02229  -0.0286   1.0000   0.1797
 -11.000  -1.0168   0.02884   0.02118  -0.0267   1.0000   0.1877
 -10.750  -1.0115   0.02791   0.02018  -0.0244   1.0000   0.1963
 -10.500  -1.0056   0.02711   0.01938  -0.0219   1.0000   0.2041
 -10.250  -0.9977   0.02638   0.01853  -0.0196   1.0000   0.2133
 -10.000  -0.9876   0.02572   0.01791  -0.0175   1.0000   0.2216
  -9.750  -0.9756   0.02508   0.01721  -0.0155   1.0000   0.2310
  -9.500  -0.9628   0.02450   0.01658  -0.0136   1.0000   0.2404
  -9.250  -0.9489   0.02396   0.01603  -0.0118   1.0000   0.2494
  -9.000  -0.9346   0.02344   0.01540  -0.0100   1.0000   0.2593
  -8.750  -0.9197   0.02298   0.01498  -0.0082   1.0000   0.2678
  -8.500  -0.9049   0.02252   0.01447  -0.0063   1.0000   0.2769
  -8.250  -0.8905   0.02211   0.01404  -0.0044   1.0000   0.2858
  -8.000  -0.8765   0.02171   0.01364  -0.0023   1.0000   0.2940
  -7.750  -0.8641   0.02137   0.01326  -0.0001   1.0000   0.3028
  -7.500  -0.8475   0.02103   0.01295   0.0014   0.9971   0.3111
  -7.250  -0.8096   0.02063   0.01244  -0.0013   0.9828   0.3229
  -7.000  -0.7723   0.02026   0.01203  -0.0036   0.9690   0.3340
  -6.750  -0.7357   0.01991   0.01166  -0.0057   0.9550   0.3445
  -6.500  -0.6998   0.01957   0.01123  -0.0076   0.9408   0.3554
  -6.250  -0.6648   0.01926   0.01086  -0.0092   0.9266   0.3664
  -6.000  -0.6310   0.01897   0.01055  -0.0105   0.9123   0.3760
  -5.750  -0.5994   0.01870   0.01019  -0.0113   0.8977   0.3865
  -5.500  -0.5695   0.01847   0.00991  -0.0117   0.8832   0.3963
  -5.250  -0.5412   0.01826   0.00966  -0.0117   0.8691   0.4058
  -5.000  -0.5145   0.01807   0.00934  -0.0114   0.8552   0.4165
  -4.750  -0.4884   0.01790   0.00917  -0.0109   0.8415   0.4253
  -4.500  -0.4633   0.01774   0.00895  -0.0103   0.8278   0.4353
  -4.250  -0.4381   0.01760   0.00875  -0.0097   0.8147   0.4452
  -4.000  -0.4126   0.01746   0.00859  -0.0091   0.8025   0.4546
  -3.500  -0.3614   0.01722   0.00825  -0.0079   0.7784   0.4747
  -3.250  -0.3359   0.01711   0.00811  -0.0074   0.7666   0.4849
  -3.000  -0.3103   0.01701   0.00794  -0.0068   0.7556   0.4957
  -2.750  -0.2845   0.01692   0.00786  -0.0062   0.7441   0.5052
  -2.500  -0.2590   0.01684   0.00775  -0.0056   0.7324   0.5158
  -2.250  -0.2332   0.01677   0.00764  -0.0050   0.7217   0.5264
  -2.000  -0.2073   0.01671   0.00758  -0.0044   0.7107   0.5364
  -1.750  -0.1817   0.01666   0.00751  -0.0039   0.6992   0.5474
  -1.500  -0.1558   0.01661   0.00744  -0.0033   0.6886   0.5580
  -1.250  -0.1298   0.01658   0.00741  -0.0027   0.6777   0.5682
  -1.000  -0.1040   0.01655   0.00736  -0.0022   0.6662   0.5795
  -0.750  -0.0779   0.01653   0.00733  -0.0016   0.6558   0.5901
  -0.500  -0.0519   0.01652   0.00732  -0.0011   0.6447   0.6006
  -0.250  -0.0261   0.01651   0.00730  -0.0006   0.6333   0.6119
   0.000   0.0000   0.01651   0.00729   0.0000   0.6228   0.6229
   0.250   0.0261   0.01651   0.00730   0.0006   0.6120   0.6333
   0.500   0.0519   0.01652   0.00732   0.0011   0.6006   0.6447
   0.750   0.0779   0.01653   0.00733   0.0016   0.5902   0.6558
   1.000   0.1040   0.01655   0.00736   0.0022   0.5795   0.6662
   1.250   0.1298   0.01658   0.00740   0.0027   0.5683   0.6777
   1.500   0.1558   0.01661   0.00744   0.0033   0.5580   0.6886
   1.750   0.1817   0.01666   0.00751   0.0039   0.5474   0.6992
   2.000   0.2073   0.01671   0.00758   0.0044   0.5363   0.7107
   2.250   0.2332   0.01677   0.00764   0.0050   0.5264   0.7217
   2.500   0.2590   0.01684   0.00775   0.0056   0.5158   0.7324
   2.750   0.2845   0.01692   0.00786   0.0062   0.5052   0.7441
   3.000   0.3103   0.01701   0.00794   0.0068   0.4958   0.7556
   3.250   0.3359   0.01711   0.00811   0.0074   0.4849   0.7665
   3.500   0.3614   0.01722   0.00825   0.0079   0.4747   0.7784
   4.000   0.4126   0.01746   0.00859   0.0091   0.4546   0.8025
   4.250   0.4381   0.01760   0.00875   0.0097   0.4452   0.8147
   4.500   0.4633   0.01774   0.00895   0.0103   0.4353   0.8277
   4.750   0.4884   0.01790   0.00917   0.0109   0.4253   0.8415
   5.000   0.5145   0.01807   0.00934   0.0114   0.4165   0.8552
   5.250   0.5412   0.01826   0.00966   0.0117   0.4058   0.8691
   5.500   0.5695   0.01847   0.00991   0.0117   0.3964   0.8832
   5.750   0.5994   0.01870   0.01019   0.0113   0.3865   0.8978
   6.000   0.6311   0.01897   0.01055   0.0105   0.3760   0.9123
   6.250   0.6649   0.01926   0.01085   0.0092   0.3663   0.9266
   6.500   0.6998   0.01957   0.01123   0.0076   0.3554   0.9409
   6.750   0.7358   0.01991   0.01166   0.0057   0.3445   0.9550
   7.000   0.7724   0.02026   0.01203   0.0036   0.3339   0.9690
   7.250   0.8097   0.02063   0.01244   0.0012   0.3228   0.9829
   7.500   0.8476   0.02103   0.01295  -0.0014   0.3110   0.9973
   7.750   0.8641   0.02136   0.01326   0.0001   0.3028   1.0000
   8.000   0.8765   0.02171   0.01364   0.0023   0.2940   1.0000
   8.250   0.8905   0.02211   0.01404   0.0044   0.2858   1.0000
   8.500   0.9049   0.02251   0.01447   0.0063   0.2769   1.0000
   8.750   0.9198   0.02298   0.01498   0.0082   0.2678   1.0000
   9.000   0.9347   0.02343   0.01540   0.0100   0.2593   1.0000
   9.250   0.9490   0.02396   0.01603   0.0118   0.2493   1.0000
   9.500   0.9629   0.02450   0.01658   0.0136   0.2404   1.0000
   9.750   0.9758   0.02508   0.01721   0.0155   0.2310   1.0000
  10.000   0.9879   0.02571   0.01791   0.0174   0.2217   1.0000
  10.250   0.9980   0.02638   0.01853   0.0195   0.2133   1.0000
  10.500   1.0059   0.02711   0.01938   0.0219   0.2040   1.0000
  10.750   1.0119   0.02791   0.02018   0.0244   0.1962   1.0000
  11.000   1.0173   0.02883   0.02118   0.0266   0.1877   1.0000
  11.250   1.0224   0.02989   0.02228   0.0285   0.1797   1.0000
  11.500   1.0256   0.03112   0.02354   0.0302   0.1715   1.0000
  11.750   1.0289   0.03252   0.02501   0.0316   0.1631   1.0000
  12.000   1.0294   0.03414   0.02662   0.0328   0.1555   1.0000
  12.250   1.0308   0.03594   0.02852   0.0337   0.1467   1.0000
  12.500   1.0294   0.03801   0.03058   0.0343   0.1394   1.0000
  12.750   1.0284   0.04026   0.03293   0.0346   0.1314   1.0000
  13.000   1.0253   0.04279   0.03547   0.0347   0.1246   1.0000
  13.250   1.0221   0.04551   0.03828   0.0345   0.1177   1.0000
  13.500   1.0172   0.04849   0.04127   0.0341   0.1120   1.0000
  13.750   1.0129   0.05163   0.04453   0.0335   0.1059   1.0000
  14.000   1.0051   0.05517   0.04806   0.0326   0.1010   1.0000
  14.250   1.0003   0.05863   0.05166   0.0317   0.0956   1.0000
  14.500   0.9925   0.06253   0.05562   0.0304   0.0910   1.0000
  14.750   0.9851   0.06652   0.05962   0.0290   0.0869   1.0000
  15.000   0.9780   0.07072   0.06396   0.0274   0.0823   1.0000
  15.250   0.9695   0.07516   0.06843   0.0255   0.0785   1.0000
  15.500   0.9618   0.07962   0.07294   0.0237   0.0747   1.0000
  15.750   0.9538   0.08436   0.07779   0.0216   0.0707   1.0000
  16.000   0.9460   0.08906   0.08252   0.0195   0.0674   1.0000
  16.250   0.9397   0.09361   0.08711   0.0175   0.0643   1.0000
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