Surf / pump foil — 900 mm reference front wingvsDownwind glide foil — high aspect reference front wing

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

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

What changed

PropertySurf / pump foilDownwind glide foilChange%
Geometry
Span900 mm1240 mm+340 mm+37.8%
Root chord150 mm130 mm-20 mm-13.3%
Tip chord76 mm48 mm-28 mm-36.8%
Sweep parameter8.5539.717+1.164+13.6%
Dihedral-1.50°-2.50°-1.00°+66.7%
Tip twist-2.00°-2.50°-0.50°+25.0%
TE thickness0 mm0 mm-0 mm-20.0%
Tip cap peak (chord fraction)0.4500.500+0.050+11.1%
Tip cap reach0.3500.400+0.050+14.3%
Derived
Aspect ratio7.24112.696+5.455+75.3%
Area111865 mm²121109 mm²+9245 mm²+8.3%
Taper0.5070.369-0.137-27.1%
MAC128 mm104 mm-24 mm-18.9%
Sections
Root sectiona18e818changed—
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 — “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×); “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×). 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/DSurf / pump foilDownwind glide foil

water (sea), ρ = 1025 kg/m³

data
V (kt)Surf / pump foilDownwind glide foil
8.5518.3222.02
8.7519.1823.32
9.6022.0329.03
9.9122.8331.15
10.4524.1732.16
11.2725.3133.73
11.3025.3533.73
12.1525.8133.52
12.6425.8433.40
13.0025.8732.99
13.8525.5732.03
14.0025.4631.87
14.7024.9630.72
15.3624.3329.65
15.5524.1529.28