MIT Daedalus 88 — the 34 m human-powered wingvs140cm2 surf foil stabilizer
root section dae11 → naca0008 · tip section dae31 → — · sweep parameter 0.484 → 5.703 · dihedral 1.00° → 0.00° · tip twist -1.50° → 0.00° · area 31712462 mm² → 15140 mm²
units
- MIT Daedalus 88 — the 34 m human-powered wing
- 140cm2 surf foil stabilizer
What changed
| Property | MIT Daedalus 88 | 140cm2 surf foil stab… | Change | % |
|---|---|---|---|---|
| Geometry | ||||
| Span | 34100 mm | 334 mm | -33766 mm | -99.0% |
| Root chord | 1050 mm | 47 mm | -1003 mm | -95.5% |
| Tip chord | 762 mm | 37 mm | -725 mm | -95.1% |
| Sweep parameter | 0.484 | 5.703 | +5.219 | +1078.3% |
| Dihedral | 1.00° | 0.00° | -1.00° | -100.0% |
| Tip twist | -1.50° | 0.00° | +1.50° | -100.0% |
| TE thickness | 2 mm | 1 mm | -1 mm | -46.7% |
| Sections | 40 | 30 | -10 | -25.0% |
| Tip cap reach | 0.250 | 0.350 | +0.100 | +40.0% |
| Derived | ||||
| Aspect ratio | 36.667 | 7.368 | -29.299 | -79.9% |
| Area | 31712462 mm² | 15140 mm² | -31697322 mm² | -100.0% |
| Taper | 0.726 | 0.787 | +0.062 | +8.5% |
| MAC | 939 mm | 45 mm | -894 mm | -95.2% |
| Sections | ||||
| Root section | dae11 | naca0008 | changed | — |
| Tip section | dae31 | — | changed | — |
| Shapedeviation at matched span fractions, 64 samples | ||||
| Chord deviation (max) | 1003 mm | |||
| Chord deviation (RMS) | 889 mm | |||
| Twist deviation (max) | 1.50° | |||
| Dihedral deviation (max) | 298 mm | |||
| Tip cap deviation (max) | 16978 mm | |||