Recorded airfoil sections
Aceair Aeris 200
The UIUC airfoil-usage tables record the Aceair Aeris 200 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 |
|---|---|---|---|---|---|
| NASA NLF(1)-0215F | Other | 15.0% | 39% | 3.97% | 39% |
| FX 75-141 | Other | 14.1% | 35% | 3.40% | 56% |
NASA NLF(1)-0215F
Other series · 15.0% thick at 39% chord · 3.97% camber at 39% chord
Also recorded on 10 other aircraft
- Freedom Master Air Shark
- LoPresti Sharkfire
- Neico Lancair 200
- Neico Lancair 320
- Neico Lancair 360
- Prescott Pusher
- Seawind International Seawing 2500
- Seawind International Seawing 3000
- Wheeler Express
- Whigham GW-7
FX 75-141
Other series · 14.1% thick at 35% chord · 3.40% camber at 56% 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