Recorded airfoil sections

Solaris 230

The UIUC airfoil-usage tables record the Solaris 230 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
FX 61-184	Other	18.4%	37%	3.06%	63%
FX 61-163	Other	16.4%	35%	2.58%	33%

FX 61-184

Other series · 18.4% thick at 37% chord · 3.06% camber at 63% chord

Coordinates, polars & DXF

Also recorded on 45 other aircraft

FX 61-163

Other series · 16.4% thick at 35% chord · 2.58% camber at 33% chord

Coordinates, polars & DXF

Also recorded on 44 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