Recorded airfoil sections

Gonzalez Gil-Pazo GP-2

The UIUC airfoil-usage tables record the Gonzalez Gil-Pazo GP-2 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
GOE 681Goettingen17.0%26%4.36%39%
CLARK YHOther11.9%29%2.50%35%

GOE 681

Goettingen series · 17.0% thick at 26% chord · 4.36% camber at 39% chord

Also recorded on 7 other aircraft

CLARK YH

Other series · 11.9% thick at 29% chord · 2.50% camber at 35% chord

Also recorded on 89 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

Gonzalez Gil-Pazo GP-2 airfoil: GOE 681 and CLARK YH | Foil.tools