Recorded airfoil sections

Fokker F.VII-3M

The UIUC airfoil-usage tables record the Fokker F.VII-3M 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 386	Goettingen	20.4%	27%	5.43%	37%
GOE 388	Goettingen	10.4%	26%	5.48%	42%

GOE 386

Goettingen series · 20.4% thick at 27% chord · 5.43% camber at 37% chord

Coordinates, polars & DXF

Also recorded on 7 other aircraft

GOE 388

Goettingen series · 10.4% thick at 26% chord · 5.48% camber at 42% chord

Coordinates, polars & DXF

Also recorded on 1 other aircraft

Klemm Kl 35

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