Recorded airfoil sections
Mylius MY 102 Tornado
The UIUC airfoil-usage tables record the Mylius MY 102 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 64(3)-218 | NACA | 18.0% | 35% | 1.10% | 50% |
| NACA 64(1)-212 | Other | 12.0% | 37% | 1.10% | 50% |
NACA 64(3)-218
NACA series · 18.0% thick at 35% chord · 1.10% camber at 50% chord
NACA 64(1)-212
Other series · 12.0% thick at 37% chord · 1.10% camber at 50% chord
Also recorded on 39 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