Recorded airfoil sections

Supermarine 545

The UIUC airfoil-usage tables record the Supermarine 545 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
RAE 103	RAE	10.0%	39%	symmetric	—
RAE 100	RAE	10.0%	27%	symmetric	—

RAE 103

RAE series · 10.0% thick at 39% chord · symmetric

Coordinates, polars & DXF

Also recorded on 1 other aircraft

Short SA.4 Sperrin

RAE 100

RAE series · 10.0% thick at 27% chord · symmetric

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