Recorded airfoil sections
Stelux Trenzo
The UIUC airfoil-usage tables record the Stelux Trenzo 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 64(2)-415 | NACA | 15.0% | 35% | 2.21% | 50% |
| NACA 23012 12% | NACA | 12.0% | 29% | 1.86% | 15% |
NACA 64(2)-415
NACA series · 15.0% thick at 35% chord · 2.21% camber at 50% chord
Also recorded on 24 other aircraft
- Fairchild F-27
- Fairchild FH-227
- Fokker 50
- Fokker 60
- Fokker F27 Friendship (C-31)
- Kendall K.1
- Grumman American AA-1B Tr-2
- Grumman American AA-1B Trainer
- Grumman American AA-1C Lynx
- Grumman American AA-1C T-Cat
- Grumman American AA-5 Traveler
- Grumman American AA-5A Cheetah
- all 24 on the section page
NACA 23012 12%
NACA series · 12.0% thick at 29% chord · 1.86% camber at 15% 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