Recorded airfoil sections

Satoh-Maeda SM-OX

The UIUC airfoil-usage tables record the Satoh-Maeda SM-OX 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
NACA 4418NACA18.0%29%4.01%42%
NACA 4415NACA15.0%29%3.97%42%

NACA 4418

NACA series · 18.0% thick at 29% chord · 4.01% camber at 42% chord

Also recorded on 17 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

Satoh-Maeda SM-OX airfoil: NACA 4418 and NACA 4415 | Foil.tools