Recorded airfoil sections

Westland Lynx (early blades)

The UIUC airfoil-usage tables record the Westland Lynx (early blades) 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
NPL 9615	Other	11.3%	33%	1.02%	19%
NPL 9660	Other	11.3%	33%	1.01%	19%

NPL 9615

Other series · 11.3% thick at 33% chord · 1.02% camber at 19% chord

Coordinates, polars & DXF

Also recorded on 2 other aircraft

Westland 30
Westland Lynx

NPL 9660

Other series · 11.3% thick at 33% chord · 1.01% camber at 19% chord

Coordinates, polars & DXF

Also recorded on 1 other aircraft

Westland 30

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