Recorded airfoil sections
OMAC 1
The UIUC airfoil-usage tables record the OMAC 1 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)-215 | NACA | 15.0% | 35% | 1.10% | 50% |
| NACA 64(1)-212 MOD B | Other | 12.1% | 33% | 1.51% | 12% |
NACA 64(2)-215
NACA series · 15.0% thick at 35% chord · 1.10% camber at 50% chord
Also recorded on 9 other aircraft
- General Avia F15F Delfino
- Griffon Aerospace Lionheart
- MBB Bo 209 Monsun
- Procaer F.15 Ficchio
- UTVA Lasta
- Monnett Monex
- Panstwowe Zaklady Lotnicze PZL 130 Orlik
- Panstwowe Zaklady Lotnicze PZL 140 Orlik 2000
- Siegrist RS1 ILSE
NACA 64(1)-212 MOD B
Other series · 12.1% thick at 33% chord · 1.51% camber at 12% chord
Also recorded on 1 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