Recorded airfoil sections
Schempp-Hirth D 30 Cirrus
The UIUC airfoil-usage tables record the Schempp-Hirth D 30 Cirrus 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
NACA 2414
Other series · 14.0% thick at 29% chord · 2.01% camber at 42% chord
NACA 4412
NACA series · 12.0% thick at 29% chord · 4.01% camber at 42% chord
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