Recorded airfoil sections
PLAVIA Gurripato II
The UIUC airfoil-usage tables record the PLAVIA Gurripato II 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
| Section | Series | Thickness | at x/c | Camber | at x/c |
|---|---|---|---|---|---|
| GOE 535 | Goettingen | 16.3% | 26% | 5.77% | 50% |
| NACA 23012 12% | NACA | 12.0% | 29% | 1.86% | 15% |
GOE 535
Goettingen series · 16.3% thick at 26% chord · 5.77% camber at 50% chord
Also recorded on 58 other aircraft
NACA 23012 12%
NACA series · 12.0% thick at 29% chord · 1.86% camber at 15% chord
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