Recorded airfoil sections
Boeing 301 XCH-62 HLH
The UIUC airfoil-usage tables record the Boeing 301 XCH-62 HLH 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 |
|---|---|---|---|---|---|
| BOEING VERTOL V43012-1.58 | Other | 12.1% | 29% | 3.67% | 15% |
| BOEING-VERTOL VR-7 | Other | 12.0% | 33% | 3.12% | 31% |
BOEING VERTOL V43012-1.58
Other series · 12.1% thick at 29% chord · 3.67% camber at 15% chord
BOEING-VERTOL VR-7
Other series · 12.0% thick at 33% chord · 3.12% camber at 31% chord
Also recorded on 1 other aircraft
- Bell 301 XV-15 (Boeing ATB)
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