Recorded airfoil sections

QAC Q2

The UIUC airfoil-usage tables record the QAC Q2 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
UNIVERSITY OF GLASGOW GU25-5(11)8Other20.0%42%7.13%46%
EPPLER E1212Eppler17.7%22%3.21%35%

UNIVERSITY OF GLASGOW GU25-5(11)8

Other series · 20.0% thick at 42% chord · 7.13% camber at 46% chord

Also recorded on 5 other aircraft

EPPLER E1212

Eppler series · 17.7% thick at 22% chord · 3.21% camber at 35% chord

Also recorded on 3 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

QAC Q2 airfoil: UNIVERSITY OF GLASGOW GU25-5(11)8 and EPPLER E1212 | Foil.tools