Recorded airfoil sections

Lockheed-Vega 134 B-38 Flying Fortress

The UIUC airfoil-usage tables record the Lockheed-Vega 134 B-38 Flying Fortress 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 0018NACA18.0%29%symmetric—
NACA 0010NACA10.0%29%symmetric—

NACA 0018

NACA series · 18.0% thick at 29% chord · symmetric

Also recorded on 14 other aircraft

NACA 0010

NACA series · 10.0% thick at 29% chord · symmetric

Also recorded on 9 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

Lockheed-Vega 134 B-38 Flying Fortress airfoil: NACA 0018 and NACA 0010 | Foil.tools