Gossamer Condor — 96 ft of wing at 11 mphvs140cm2 surf foil stabilizer
root section l7769 → naca0008 · dihedral 3.00° → 0.00° · area 66293551 mm² → 15140 mm² · span 29260 mm → 334 mm · root chord 2862 mm → 47 mm · mac 2358 mm → 45 mm
units
- Gossamer Condor — 96 ft of wing at 11 mph
- 140cm2 surf foil stabilizer
What changed
| Property | Gossamer Condor | 140cm2 surf foil stab… | Change | % |
|---|---|---|---|---|
| Geometry | ||||
| Span | 29260 mm | 334 mm | -28926 mm | -98.9% |
| Root chord | 2862 mm | 47 mm | -2815 mm | -98.4% |
| Tip chord | 1431 mm | 37 mm | -1394 mm | -97.4% |
| Sweep parameter | 11.711 | 5.703 | -6.008 | -51.3% |
| Dihedral | 3.00° | 0.00° | -3.00° | -100.0% |
| TE thickness | 2 mm | 1 mm | -1 mm | -46.7% |
| Sections | 40 | 30 | -10 | -25.0% |
| Tip cap reach | 0.200 | 0.350 | +0.150 | +75.0% |
| Derived | ||||
| Aspect ratio | 12.914 | 7.368 | -5.546 | -42.9% |
| Area | 66293551 mm² | 15140 mm² | -66278411 mm² | -100.0% |
| Taper | 0.500 | 0.787 | +0.287 | +57.4% |
| MAC | 2358 mm | 45 mm | -2313 mm | -98.1% |
| Sections | ||||
| Root section | l7769 | naca0008 | changed | — |
| Shapedeviation at matched span fractions, 64 samples | ||||
| Chord deviation (max) | 2815 mm | |||
| Chord deviation (RMS) | 2266 mm | |||
| Twist deviation (max) | 0.00° | |||
| Dihedral deviation (max) | 767 mm | |||
| Tip cap deviation (max) | 15067 mm | |||