Recorded airfoil sections

Jacobs Schweyer Weihe (TG-19)

The UIUC airfoil-usage tables record the Jacobs Schweyer Weihe (TG-19) 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 549	Goettingen	13.9%	29%	4.68%	37%
NACA M12	Other	12.0%	33%	2.00%	33%

GOE 549

Goettingen series · 13.9% thick at 29% chord · 4.68% camber at 37% chord

Coordinates, polars & DXF

Also recorded on 59 other aircraft

NACA M12

Other series · 12.0% thick at 33% chord · 2.00% camber at 33% chord

Coordinates, polars & DXF

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