Recorded airfoil sections
Partenair S45 Mystere
The UIUC airfoil-usage tables record the Partenair S45 Mystere 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 65(3)-218 | NACA | 18.0% | 39% | 1.10% | 50% |
| NACA 65(2)-215 | NACA | 15.0% | 39% | 1.10% | 50% |
NACA 65(3)-218
NACA series · 18.0% thick at 39% chord · 1.10% camber at 50% chord
Also recorded on 1 other aircraft
NACA 65(2)-215
NACA series · 15.0% thick at 39% chord · 1.10% camber at 50% chord
Also recorded on 4 other aircraft
- Maverick Aircraft Twinjet
- On Mark Marksman
- Partenair S44 Mystere
- Turner T-40A
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