Recorded airfoil sections
McDonnell F2H Banshee
The UIUC airfoil-usage tables record the McDonnell F2H Banshee 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 |
|---|---|---|---|---|---|
| NACA 65(1)-212 | NACA | 12.0% | 39% | 1.10% | 50% |
| NACA 65-209 | NACA | 9.0% | 42% | 1.10% | 50% |
NACA 65(1)-212
NACA series · 12.0% thick at 39% chord · 1.10% camber at 50% chord
Also recorded on 8 other aircraft
- Viper Aircraft ViperJet II
- Frederick-Ames EOS/SFA
- Jacquet-Pottier JP-20-90 Impala
- SNCASE SE.210 Caravelle
- SNCASE SE.2410 Grognard I
- SNCASE SE.2415 Grognard II
- Vought V-340 F6U Pirate
- Westland Wyvern
NACA 65-209
NACA series · 9.0% thick at 42% chord · 1.10% camber at 50% 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