Recorded airfoil sections

Great Lakes 2T-1A Sport Trainer

The UIUC airfoil-usage tables record the Great Lakes 2T-1A Sport Trainer 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

SectionSeriesThicknessat x/cCamberat x/c
NACA M6NACA12.1%33%2.14%29%
NACA M12NACA12.0%35%1.98%31%

NACA M6

NACA series · 12.1% thick at 33% chord · 2.14% camber at 29% chord

Also recorded on 62 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

Great Lakes 2T-1A Sport Trainer airfoil: NACA M6 and NACA M12 | Foil.tools