Recorded airfoil sections

Vliegtuigbouw V-20

The UIUC airfoil-usage tables record the Vliegtuigbouw V-20 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 535Goettingen16.3%26%5.77%50%
NACA M6NACA12.1%33%2.14%29%

NACA M6

NACA series · 12.1% thick at 33% chord · 2.14% camber at 29% chord

Coordinates, polars & DXF

Also recorded on 62 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

Vliegtuigbouw V-20 airfoil: GOE 535 and NACA M6 | Foil.tools