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S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1046 17% (Danny Howell) (s1046-il)
Reynolds number: 200,000
Max Cl/Cd: 54.59 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1046-il-200000-n5.txt
Download as CSV file: xf-s1046-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9942   0.10207   0.09653  -0.0117   1.0000   0.0282
 -17.250  -1.0035   0.09678   0.09117  -0.0143   1.0000   0.0291
 -17.000  -1.0121   0.09171   0.08601  -0.0166   1.0000   0.0302
 -16.750  -1.0196   0.08693   0.08113  -0.0188   1.0000   0.0317
 -16.500  -1.0260   0.08240   0.07650  -0.0207   1.0000   0.0330
 -16.250  -1.0363   0.07739   0.07142  -0.0229   1.0000   0.0343
 -16.000  -1.0452   0.07272   0.06668  -0.0249   1.0000   0.0360
 -15.750  -1.0516   0.06851   0.06238  -0.0265   1.0000   0.0379
 -15.500  -1.0576   0.06447   0.05823  -0.0280   1.0000   0.0401
 -15.250  -1.0662   0.06023   0.05393  -0.0295   1.0000   0.0422
 -15.000  -1.0719   0.05647   0.05010  -0.0307   1.0000   0.0450
 -14.750  -1.0756   0.05311   0.04664  -0.0317   1.0000   0.0478
 -14.500  -1.0827   0.04949   0.04299  -0.0326   1.0000   0.0510
 -14.250  -1.0852   0.04652   0.03994  -0.0331   1.0000   0.0547
 -14.000  -1.0891   0.04349   0.03686  -0.0336   1.0000   0.0584
 -13.750  -1.0912   0.04075   0.03408  -0.0338   1.0000   0.0630
 -13.500  -1.0918   0.03826   0.03154  -0.0338   1.0000   0.0676
 -13.250  -1.0922   0.03588   0.02912  -0.0337   1.0000   0.0726
 -13.000  -1.0903   0.03381   0.02700  -0.0333   1.0000   0.0781
 -12.750  -1.0890   0.03178   0.02495  -0.0328   1.0000   0.0838
 -12.500  -1.0850   0.03006   0.02317  -0.0321   1.0000   0.0899
 -12.250  -1.0820   0.02837   0.02146  -0.0312   1.0000   0.0967
 -12.000  -1.0771   0.02691   0.01998  -0.0301   1.0000   0.1034
 -11.750  -1.0717   0.02559   0.01864  -0.0288   1.0000   0.1110
 -11.500  -1.0660   0.02439   0.01743  -0.0273   1.0000   0.1183
 -11.250  -1.0578   0.02341   0.01641  -0.0256   1.0000   0.1266
 -11.000  -1.0521   0.02241   0.01544  -0.0236   1.0000   0.1349
 -10.750  -1.0447   0.02159   0.01461  -0.0213   1.0000   0.1446
 -10.250  -1.0297   0.02023   0.01328  -0.0161   1.0000   0.1653
 -10.000  -1.0189   0.01963   0.01271  -0.0139   1.0000   0.1756
  -9.750  -1.0048   0.01912   0.01218  -0.0120   1.0000   0.1853
  -9.500  -0.9909   0.01862   0.01169  -0.0101   1.0000   0.1945
  -9.250  -0.9759   0.01816   0.01122  -0.0082   1.0000   0.2031
  -9.000  -0.9599   0.01777   0.01081  -0.0065   1.0000   0.2124
  -8.750  -0.9458   0.01736   0.01042  -0.0044   1.0000   0.2208
  -8.500  -0.9285   0.01701   0.01006  -0.0029   0.9986   0.2302
  -8.250  -0.8929   0.01657   0.00959  -0.0050   0.9828   0.2423
  -8.000  -0.8589   0.01615   0.00917  -0.0068   0.9638   0.2536
  -7.750  -0.8235   0.01578   0.00876  -0.0087   0.9451   0.2643
  -7.500  -0.7882   0.01546   0.00836  -0.0104   0.9264   0.2751
  -7.250  -0.7563   0.01513   0.00801  -0.0115   0.9070   0.2847
  -7.000  -0.7275   0.01487   0.00768  -0.0118   0.8875   0.2939
  -6.750  -0.7012   0.01465   0.00738  -0.0115   0.8689   0.3033
  -6.500  -0.6765   0.01443   0.00711  -0.0109   0.8518   0.3119
  -6.250  -0.6516   0.01427   0.00684  -0.0103   0.8362   0.3210
  -6.000  -0.6277   0.01407   0.00661  -0.0096   0.8216   0.3294
  -5.750  -0.6029   0.01392   0.00636  -0.0089   0.8080   0.3382
  -5.500  -0.5785   0.01374   0.00616  -0.0083   0.7949   0.3469
  -5.250  -0.5534   0.01360   0.00595  -0.0077   0.7826   0.3556
  -5.000  -0.5284   0.01345   0.00575  -0.0071   0.7712   0.3645
  -4.750  -0.5031   0.01332   0.00556  -0.0066   0.7598   0.3732
  -4.500  -0.4774   0.01319   0.00539  -0.0061   0.7486   0.3827
  -4.250  -0.4519   0.01306   0.00523  -0.0056   0.7381   0.3913
  -4.000  -0.4258   0.01296   0.00506  -0.0052   0.7275   0.4009
  -3.750  -0.4000   0.01283   0.00494  -0.0048   0.7169   0.4101
  -3.500  -0.3738   0.01274   0.00479  -0.0044   0.7072   0.4196
  -3.250  -0.3475   0.01264   0.00467  -0.0040   0.6965   0.4294
  -3.000  -0.3212   0.01254   0.00456  -0.0036   0.6866   0.4387
  -2.750  -0.2946   0.01248   0.00443  -0.0033   0.6766   0.4488
  -2.500  -0.2682   0.01238   0.00436  -0.0030   0.6660   0.4583
  -2.250  -0.2415   0.01231   0.00426  -0.0026   0.6562   0.4681
  -2.000  -0.2148   0.01225   0.00418  -0.0023   0.6456   0.4786
  -1.750  -0.1881   0.01218   0.00412  -0.0020   0.6352   0.4882
  -1.500  -0.1613   0.01214   0.00404  -0.0017   0.6250   0.4985
  -1.250  -0.1345   0.01208   0.00400  -0.0014   0.6141   0.5088
  -1.000  -0.1076   0.01204   0.00396  -0.0011   0.6035   0.5189
  -0.750  -0.0807   0.01203   0.00390  -0.0009   0.5933   0.5296
  -0.500  -0.0539   0.01199   0.00389  -0.0006   0.5822   0.5400
  -0.250  -0.0269   0.01197   0.00388  -0.0003   0.5717   0.5503
   0.250   0.0269   0.01197   0.00388   0.0003   0.5503   0.5717
   0.500   0.0539   0.01199   0.00389   0.0006   0.5400   0.5822
   0.750   0.0807   0.01203   0.00390   0.0009   0.5296   0.5933
   1.000   0.1076   0.01204   0.00396   0.0012   0.5188   0.6036
   1.250   0.1345   0.01208   0.00400   0.0014   0.5088   0.6142
   1.500   0.1613   0.01214   0.00404   0.0017   0.4985   0.6251
   1.750   0.1881   0.01218   0.00412   0.0020   0.4882   0.6352
   2.000   0.2148   0.01225   0.00418   0.0023   0.4785   0.6456
   2.250   0.2416   0.01231   0.00426   0.0026   0.4682   0.6562
   2.500   0.2682   0.01238   0.00436   0.0030   0.4583   0.6660
   2.750   0.2946   0.01248   0.00443   0.0033   0.4488   0.6766
   3.000   0.3212   0.01254   0.00456   0.0036   0.4387   0.6865
   3.250   0.3475   0.01264   0.00467   0.0040   0.4294   0.6965
   3.500   0.3738   0.01274   0.00479   0.0044   0.4196   0.7072
   3.750   0.4000   0.01283   0.00493   0.0048   0.4100   0.7170
   4.000   0.4258   0.01296   0.00506   0.0052   0.4010   0.7276
   4.250   0.4519   0.01306   0.00523   0.0056   0.3914   0.7380
   4.500   0.4774   0.01319   0.00539   0.0061   0.3826   0.7486
   4.750   0.5031   0.01332   0.00556   0.0066   0.3732   0.7598
   5.000   0.5284   0.01345   0.00575   0.0071   0.3645   0.7711
   5.250   0.5534   0.01360   0.00595   0.0077   0.3556   0.7826
   5.500   0.5785   0.01374   0.00616   0.0082   0.3469   0.7949
   5.750   0.6030   0.01392   0.00637   0.0089   0.3383   0.8080
   6.000   0.6277   0.01407   0.00661   0.0096   0.3295   0.8217
   6.250   0.6516   0.01427   0.00684   0.0103   0.3210   0.8362
   6.500   0.6765   0.01443   0.00711   0.0109   0.3118   0.8518
   6.750   0.7013   0.01465   0.00738   0.0115   0.3032   0.8689
   7.000   0.7276   0.01487   0.00768   0.0117   0.2940   0.8875
   7.250   0.7563   0.01513   0.00800   0.0115   0.2847   0.9070
   7.500   0.7883   0.01546   0.00836   0.0104   0.2750   0.9265
   7.750   0.8236   0.01578   0.00876   0.0087   0.2643   0.9450
   8.000   0.8590   0.01615   0.00917   0.0068   0.2536   0.9639
   8.250   0.8931   0.01657   0.00959   0.0050   0.2423   0.9829
   8.500   0.9286   0.01701   0.01006   0.0028   0.2302   0.9987
   8.750   0.9458   0.01736   0.01042   0.0044   0.2209   1.0000
   9.000   0.9600   0.01777   0.01080   0.0064   0.2124   1.0000
   9.250   0.9760   0.01816   0.01122   0.0082   0.2031   1.0000
   9.500   0.9910   0.01862   0.01169   0.0101   0.1945   1.0000
   9.750   1.0049   0.01912   0.01218   0.0120   0.1853   1.0000
  10.000   1.0192   0.01963   0.01271   0.0138   0.1756   1.0000
  10.250   1.0300   0.02023   0.01328   0.0161   0.1652   1.0000
  10.500   1.0363   0.02091   0.01392   0.0189   0.1549   1.0000
  10.750   1.0450   0.02159   0.01461   0.0213   0.1444   1.0000
  11.000   1.0525   0.02241   0.01544   0.0235   0.1348   1.0000
  11.250   1.0583   0.02340   0.01641   0.0256   0.1264   1.0000
  11.500   1.0664   0.02439   0.01742   0.0272   0.1180   1.0000
  11.750   1.0721   0.02559   0.01863   0.0287   0.1106   1.0000
  12.000   1.0774   0.02692   0.01998   0.0300   0.1031   1.0000
  12.250   1.0827   0.02835   0.02145   0.0311   0.0965   1.0000
  12.500   1.0859   0.03003   0.02315   0.0320   0.0900   1.0000
  12.750   1.0900   0.03175   0.02492   0.0327   0.0839   1.0000
  13.000   1.0910   0.03381   0.02700   0.0332   0.0779   1.0000
  13.250   1.0933   0.03585   0.02909   0.0335   0.0726   1.0000
  13.500   1.0927   0.03825   0.03152   0.0337   0.0675   1.0000
  13.750   1.0923   0.04072   0.03405   0.0337   0.0628   1.0000
  14.000   1.0902   0.04347   0.03684   0.0334   0.0583   1.0000
  14.250   1.0867   0.04646   0.03988   0.0330   0.0546   1.0000
  14.500   1.0840   0.04947   0.04296   0.0324   0.0508   1.0000
  14.750   1.0774   0.05302   0.04655   0.0315   0.0479   1.0000
  15.000   1.0733   0.05644   0.05006   0.0306   0.0447   1.0000
  15.250   1.0675   0.06020   0.05389   0.0294   0.0420   1.0000
  15.500   1.0591   0.06443   0.05818   0.0278   0.0400   1.0000
  15.750   1.0534   0.06843   0.06227   0.0263   0.0377   1.0000
  16.000   1.0468   0.07267   0.06663   0.0247   0.0358   1.0000
  16.250   1.0381   0.07732   0.07134   0.0227   0.0342   1.0000
  16.750   1.0216   0.08685   0.08105   0.0186   0.0315   1.0000
  17.000   1.0141   0.09164   0.08593   0.0164   0.0301   1.0000
  17.250   1.0052   0.09675   0.09112   0.0140   0.0289   1.0000
  17.500   0.9950   0.10221   0.09665   0.0114   0.0279   1.0000
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