Recorded airfoil sections
Horikawa H-23B-2
The UIUC airfoil-usage tables record the Horikawa H-23B-2 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 |
|---|---|---|---|---|---|
| GOE 532 | Goettingen | 12.6% | 26% | 4.87% | 37% |
| GOE 676 (= M 12) | Goettingen | 12.0% | 33% | 2.02% | 31% |
GOE 532
Goettingen series · 12.6% thick at 26% chord · 4.87% camber at 37% chord
Also recorded on 8 other aircraft
- Schleicher Ka-8B
- Tainan TN-1
- Horikawa H-22B-2
- PIK-12
- Schleicher Condor 4
- Schleicher SG-38
- Taylorcraft 20 Zephyr 400
- Zlin 23 Honza
GOE 676 (= M 12)
Goettingen series · 12.0% thick at 33% chord · 2.02% camber at 31% chord
Also recorded on 5 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