Downwind glide foil — high aspect reference front wingvsSurf / pump foil — 900 mm reference front wing

root section e818 → a18 · tip chord 48 mm → 76 mm · aspect ratio 12.696 → 7.241 · dihedral -2.50° → -1.50° · taper 0.369 → 0.507 · span 1240 mm → 900 mm

units
  • Downwind glide foil — high aspect reference front wing
  • Surf / pump foil — 900 mm reference front wing

What changed

PropertyDownwind glide foilSurf / pump foilChange%
Geometry
Span1240 mm900 mm-340 mm-27.4%
Root chord130 mm150 mm+20 mm+15.4%
Tip chord48 mm76 mm+28 mm+58.3%
Sweep parameter9.7178.553-1.164-12.0%
Dihedral-2.50°-1.50°+1.00°-40.0%
Tip twist-2.50°-2.00°+0.50°-20.0%
TE thickness0 mm0 mm+0 mm+25.0%
Tip cap peak (chord fraction)0.5000.450-0.050-10.0%
Tip cap reach0.4000.350-0.050-12.5%
Derived
Aspect ratio12.6967.241-5.455-43.0%
Area121109 mm²111865 mm²-9245 mm²-7.6%
Taper0.3690.507+0.137+37.2%
MAC104 mm128 mm+24 mm+23.2%
Sections
Root sectione818a18changed—
Shapedeviation at matched span fractions, 64 samples
Chord deviation (max)30 mm
Chord deviation (RMS)27 mm
Twist deviation (max)0.50°
Dihedral deviation (max)15 mm
Tip cap deviation (max)174 mm

Performance

CoefficientsDimensionless — how good the shape is, independent of size and speed.
ForcesNewtons and watts — what each wing actually carries and costs at this condition.
Spanwise

withheld — “Downwind glide foil” integrates to CL 0.061 against the polar’s CL at the same α (this analysis predates the loading reporting its own) 0.446 (0.14×); “Surf / pump foil” integrates to CL 0.022 against the polar’s CL at the same α (this analysis predates the loading reporting its own) 0.363 (0.06×). A loading that does not integrate back to its own wing’s CL is not a coarse curve, it is a wrong one.

Efficiency
20.0025.0030.0010.0012.0014.00V (kt)L/DDownwind glide foilSurf / pump foil

water (sea), ρ = 1025 kg/m³

data
V (kt)Downwind glide foilSurf / pump foil
8.5522.0218.32
8.7523.3219.18
9.6029.0322.03
9.9131.1522.83
10.4532.1624.17
11.2733.7325.31
11.3033.7325.35
12.1533.5225.81
12.6433.4025.84
13.0032.9925.87
13.8532.0325.57
14.0031.8725.46
14.7030.7224.96
15.3629.6524.33
15.5529.2824.15