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S1048 14% (Danny Howell) (s1048-il)

S1048 14% (Danny Howell) - Selig S1048 airfoil


Airfoil s1048-il
Details Dat file Parser  
(s1048-il) S1048 14% (Danny Howell)
Selig S1048 airfoil
Max thickness 14% at 27% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
       S1048 14% (Danny Howell)
       1.00000     0.00000
       0.99634     0.00019
       0.98582     0.00118
       0.96921     0.00300
       0.94687     0.00538
       0.91899     0.00836
       0.88602     0.01204
       0.84851     0.01641
       0.80705     0.02143
       0.76226     0.02701
       0.71480     0.03302
       0.66537     0.03929
       0.61466     0.04560
       0.56329     0.05161
       0.51178     0.05709
       0.46066     0.06183
       0.41045     0.06565
       0.36165     0.06836
       0.31466     0.06980
       0.26988     0.06985
       0.22762     0.06844
       0.18817     0.06559
       0.15181     0.06136
       0.11879     0.05587
       0.08936     0.04925
       0.06374     0.04170
       0.04212     0.03343
       0.02468     0.02472
       0.01160     0.01588
       0.00308     0.00733
       0.00000     0.00000
       0.00308    -0.00733
       0.01160    -0.01588
       0.02468    -0.02472
       0.04212    -0.03343
       0.06374    -0.04170
       0.08936    -0.04925
       0.11879    -0.05587
       0.15181    -0.06136
       0.18817    -0.06559
       0.22762    -0.06844
       0.26988    -0.06985
       0.31466    -0.06980
       0.36165    -0.06836
       0.41045    -0.06565
       0.46066    -0.06183
       0.51178    -0.05709
       0.56329    -0.05161
       0.61466    -0.04560
       0.66537    -0.03929
       0.71480    -0.03302
       0.76226    -0.02701
       0.80705    -0.02143
       0.84851    -0.01641
       0.88602    -0.01204
       0.91899    -0.00836
       0.94687    -0.00538
       0.96921    -0.00300
       0.98582    -0.00118
       0.99634    -0.00019
       1.00000     0.00000
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Selig format dat file

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Polars for S1048 14% (Danny Howell) (s1048-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1048-il50,000924.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   s1048-il50,000528.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   s1048-il100,000940.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   s1048-il100,000541.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s1048-il200,000956 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1048-il200,000554.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1048-il500,000975.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s1048-il500,000566.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s1048-il1,000,000983.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1048-il1,000,000572.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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