Recorded airfoil sections
Glasflugel 701
The UIUC airfoil-usage tables record the Glasflugel 701 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 |
|---|---|---|---|---|---|
| FX 67-K-170/17 | Other | 17.0% | 42% | 5.07% | 46% |
| FX 67-K-150/17 | Other | 15.0% | 42% | 4.84% | 46% |
FX 67-K-170/17
Other series · 17.0% thick at 42% chord · 5.07% camber at 46% chord
FX 67-K-150/17
Other series · 15.0% thick at 42% chord · 4.84% camber at 46% 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