Recorded airfoil sections
Kortenbach & Rauh Kora I
The UIUC airfoil-usage tables record the Kortenbach & Rauh Kora I 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 |
|---|---|---|---|---|---|
| FX 66-S-196 | Other | 19.7% | 37% | 3.78% | 44% |
| FX 66-S-161 | Other | 16.1% | 33% | 3.91% | 42% |
FX 66-S-196
Other series · 19.7% thick at 37% chord · 3.78% camber at 44% chord
Also recorded on 2 other aircraft
- Rolladen Schneider LS-1c
- Rolladen Schneider LSD-Omith
FX 66-S-161
Other series · 16.1% thick at 33% chord · 3.91% camber at 42% 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