Piper J-3 Cub — a rectangular wing that worksvsGossamer Albatross II — same span, two-thirds the area

root section usa35b → l7769 · dihedral 1.00° → 3.60° · area 16577850 mm² → 45296522 mm² · span 10730 mm → 29260 mm · aspect ratio 6.945 → 18.901 · te thickness 3 mm → 2 mm

units

These analyses are not directly comparable

The geometry comparison below is unaffected — it is a comparison of shapes, not of runs.

  • Piper J-3 Cub — a rectangular wing that works
  • Gossamer Albatross II — same span, two-thirds the area

What changed

PropertyPiper J-3 CubGossamer Albatross IIChange%
Geometry
Span10730 mm29260 mm+18530 mm+172.7%
Root chord1545 mm1651 mm+106 mm+6.9%
Tip chord1545 mm1404 mm-141 mm-9.1%
Sweep parameter0.0007.476+7.476—
Dihedral1.00°3.60°+2.60°+260.0%
TE thickness3 mm2 mm-2 mm-50.0%
Tip cap reach0.3000.200-0.100-33.3%
Derived
Aspect ratio6.94518.901+11.956+172.2%
Area16577850 mm²45296522 mm²+28718672 mm²+173.2%
Taper1.0000.850-0.150-15.0%
MAC1545 mm1552 mm+7 mm+0.5%
Sections
Root sectionusa35bl7769changed—
Shapedeviation at matched span fractions, 64 samples
Chord deviation (max)141 mm
Chord deviation (RMS)80 mm
Twist deviation (max)0.00°
Dihedral deviation (max)827 mm
Tip cap deviation (max)9449 mm

Performance

CoefficientsDimensionless — how good the shape is, independent of size and speed.
Spanwise

withheld — “Piper J-3 Cub” integrates to CL 0.002 against the polar’s CL at the same α (this analysis predates the loading reporting its own) 0.330 (0.01×); “Gossamer Albatross II” integrates to CL 0.118 against the polar’s CL at the same α (this analysis predates the loading reporting its own) 0.613 (0.19×). A loading that does not integrate back to its own wing’s CL is not a coarse curve, it is a wrong one.

Drag polar
0.4000.6000.8001.001.201.400.0100.0200.0300.0400.0500.060CDCLPiper J-3 CubGossamer Albatross II

air, ρ = 1.225 kg/m³

data
CDPiper J-3 CubGossamer Albatross II
0.0120.3130.374
0.0130.3280.419
0.0130.3300.423
0.0130.3470.472
0.0150.3760.535
0.0150.3780.539
0.0170.4190.613
0.0170.4370.637
0.0200.4830.709
0.0210.5110.746
0.0250.5680.829
0.0270.6050.876
0.0320.6730.982
0.0360.7291.06
0.0430.7961.18
0.0530.8941.30
0.0650.9921.45