S1048 14% (Danny Howell) (s1048-il)
S1048 14% (Danny Howell) - Selig S1048 airfoil
| Details | Dat file | Parser | |
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(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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Polars for S1048 14% (Danny Howell) (s1048-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s1048-il | 50,000 | 9 | 24.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1048-il | 50,000 | 5 | 28.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1048-il | 100,000 | 9 | 40.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1048-il | 100,000 | 5 | 41.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1048-il | 200,000 | 9 | 56 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1048-il | 200,000 | 5 | 54.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1048-il | 500,000 | 9 | 75.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1048-il | 500,000 | 5 | 66.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s1048-il | 1,000,000 | 9 | 83.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s1048-il | 1,000,000 | 5 | 72.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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