Recorded airfoil sections

Schleicher Rhonadler

The UIUC airfoil-usage tables record the Schleicher Rhonadler 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 652Goettingen17.1%19%9.29%52%
CLARK YOther11.7%29%3.42%42%

GOE 652

Goettingen series · 17.1% thick at 19% chord · 9.29% camber at 52% chord

Also recorded on 2 other aircraft

CLARK Y

Other series · 11.7% thick at 29% chord · 3.42% camber at 42% chord

Also recorded on 295 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

Schleicher Rhonadler airfoil: GOE 652 and CLARK Y | Foil.tools