Recorded airfoil sections

Latecoere 14

The UIUC airfoil-usage tables record the Latecoere 14 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
GOE 435	Goettingen	26.2%	26%	4.72%	52%
GOE 430	Goettingen	13.3%	27%	4.82%	54%

GOE 435

Goettingen series · 26.2% thick at 26% chord · 4.72% camber at 52% chord

Coordinates, polars & DXF

GOE 430

Goettingen series · 13.3% thick at 27% chord · 4.82% camber at 54% chord

Coordinates, polars & DXF

Also recorded on 1 other aircraft

Liore et Olivier LeO 8

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