Recorded airfoil sections
Schempp-Hirth Minimoa
The UIUC airfoil-usage tables record the Schempp-Hirth Minimoa 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
GOE 681
Goettingen series · 17.0% thick at 26% chord · 4.36% camber at 39% chord
Also recorded on 7 other aircraft
- Gonzalez Gil-Pazo GP-1
- Gonzalez Gil-Pazo GP-2
- Movero Vandor
- Schempp-Hirth Goppingen Go 3 Minimoa
- Tachikawa Ki-25
- Walraven 2
- Walraven 3
GOE 693
Goettingen series · 12.0% thick at 33% chord · 3.62% camber at 44% chord
Also recorded on 7 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