Recorded airfoil sections
North American Aviation NA-162 B-45C Tornado
The UIUC airfoil-usage tables record the North American Aviation NA-162 B-45C Tornado 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 66(2)-215 | NACA | 15.0% | 46% | 1.10% | 50% |
| NACA 66(1)-212 | NACA | 12.0% | 46% | 1.10% | 50% |
NACA 66(2)-215
NACA series · 15.0% thick at 46% chord · 1.10% camber at 50% chord
Also recorded on 6 other aircraft
- North American Aviation NA-130 XB-45 Tornado
- North American Aviation NA-147 B-45A Tornado
- North American Aviation NA-153 B-45C Tornado
- Panstwowe Zaklady Lotnicze PZL Mielec M-17
- Szybowcowy Zaklad Doswiadczalny SZD-29 Zefir 3
- Szybowcowy Zaklad Doswiadczalny SZD-31 Zerfir 4
NACA 66(1)-212
NACA series · 12.0% thick at 46% chord · 1.10% camber at 50% chord
Also recorded on 3 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