Recorded airfoil sections
Reims F177
The UIUC airfoil-usage tables record the Reims F177 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
NACA 2415
Other series · 15.0% thick at 29% chord · 2.01% camber at 42% chord
Also recorded on 41 other aircraft
- Libis 160
- Libis KB-6T Matajur
- Martin 313 P7M Submaster
- McKinnie 165
- Slingsby T.18 Hengist
- Fiat G.55 Centauro
- Fiat G.59
- FMA IA 55
- FMA IA 62
- Focke Wulf FW 44 Stieglitz
- Granville Brothers Gee Bee C-8 Eightster
- Groppo Trail
- all 41 on the section page
NACA 2412
NACA series · 12.0% thick at 29% chord · 2.00% 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