Recorded airfoil sections
Slingsby T.42 Eagle 3
The UIUC airfoil-usage tables record the Slingsby T.42 Eagle 3 with 2 airfoil sections. Each is in the library with its geometry, a stored polar sweep, and DXF and .dat export. The source lists names only — it does not say which station carries which section — so they appear here thickest first.
Sections side by side
| Section | Series | Thickness | at x/c | Camber | at x/c |
|---|---|---|---|---|---|
| NACA 63(3)-618 | NACA | 18.0% | 33% | 3.31% | 50% |
| NACA 4412 | NACA | 12.0% | 29% | 4.01% | 42% |
NACA 63(3)-618
NACA series · 18.0% thick at 33% chord · 3.31% camber at 50% chord
Also recorded on 52 other aircraft
- Oldershaw O-2
- Polyt 5
- Schleicher Ka-6CR
- SIAI-Marchetti SF.210
- Slingsby T.37 Skylark
- Slingsby T.45 Swallow
- Szybowcowy Zaklad Doswiadczalny SZD-24 Foka
- Szybowcowy Zaklad Doswiadczalny SZD-24C Foka
- Szybowcowy Zaklad Doswiadczalny SZD-32 Foka 5
- FFA 2000
- FFA AS 202 Bravo
- FFA AS 32T Turbo Trainer
- all 52 on the section page
NACA 4412
NACA series · 12.0% thick at 29% chord · 4.01% camber at 42% chord
wing designs
The sections above are what the source records, not a wing anyone drew. Wings that were drawn — planform, sections and the analysis behind them, all readable — are published under Full-scale aircraft wing designs.
Aircraft-to-section mapping from the UIUC airfoil-usage tables. Section geometry is computed from the library's CST fit; nothing here is a performance claim about the aircraft. All recorded aircraft