140cm2 surf foil stabilizervsMIT Daedalus 88 — the 34 m human-powered wing
root section naca0008 → dae11 · tip section — → dae31 · area 15140 mm² → 31712462 mm² · span 334 mm → 34100 mm · root chord 47 mm → 1050 mm · mac 45 mm → 939 mm
units
- 140cm2 surf foil stabilizer
- MIT Daedalus 88 — the 34 m human-powered wing
What changed
| Property | 140cm2 surf foil stab… | MIT Daedalus 88 | Change | % |
|---|---|---|---|---|
| Geometry | ||||
| Span | 334 mm | 34100 mm | +33766 mm | +10109.6% |
| Root chord | 47 mm | 1050 mm | +1003 mm | +2134.0% |
| Tip chord | 37 mm | 762 mm | +725 mm | +1959.5% |
| Sweep parameter | 5.703 | 0.484 | -5.219 | -91.5% |
| Dihedral | 0.00° | 1.00° | +1.00° | — |
| Tip twist | 0.00° | -1.50° | -1.50° | — |
| TE thickness | 1 mm | 2 mm | +1 mm | +87.5% |
| Sections | 30 | 40 | +10 | +33.3% |
| Tip cap reach | 0.350 | 0.250 | -0.100 | -28.6% |
| Derived | ||||
| Aspect ratio | 7.368 | 36.667 | +29.299 | +397.6% |
| Area | 15140 mm² | 31712462 mm² | +31697322 mm² | +209363.2% |
| Taper | 0.787 | 0.726 | -0.062 | -7.8% |
| MAC | 45 mm | 939 mm | +894 mm | +1964.4% |
| Sections | ||||
| Root section | naca0008 | dae11 | 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 | |||