Recorded airfoil sections
Supermarine 396 Seafang F 32
The UIUC airfoil-usage tables record the Supermarine 396 Seafang F 32 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 |
|---|---|---|---|---|---|
| Supermarine 371-I (root) | Selig | 13.0% | 42% | 0.93% | 48% |
| Supermarine 371-II (tip) | Selig | 8.4% | 48% | 0.94% | 48% |
Supermarine 371-I (root)
Selig series · 13.0% thick at 42% chord · 0.93% camber at 48% chord
Also recorded on 4 other aircraft
Supermarine 371-II (tip)
Selig series · 8.4% thick at 48% chord · 0.94% camber at 48% chord
Also recorded on 4 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