Recorded airfoil sections
Szybowcowy Zaklad Doswiadczalny SZD-24C Foka
The UIUC airfoil-usage tables record the Szybowcowy Zaklad Doswiadczalny SZD-24C Foka 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 4415 | NACA | 15.0% | 29% | 3.97% | 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
NACA 4415
NACA series · 15.0% thick at 29% chord · 3.97% camber at 42% chord
Also recorded on 73 other aircraft
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