Recorded airfoil sections
Schleicher ASW 21
The UIUC airfoil-usage tables record the Schleicher ASW 21 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 S 02-196 | Other | 19.6% | 35% | 3.74% | 46% |
| WORTMANN FX 60-126 | Other | 12.6% | 27% | 3.56% | 56% |
FX S 02-196
Other series · 19.6% thick at 35% chord · 3.74% camber at 46% chord
Also recorded on 3 other aircraft
- Schleicher ASK 21 TG-9 Vanguard
- Schempp-Hirth Standard Cirrus
- Szybowcowy Zaklad Doswiadczalny SZD-51-1 Junior
WORTMANN FX 60-126
Other series · 12.6% thick at 27% chord · 3.56% camber at 56% chord
Also recorded on 59 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