Recorded airfoil sections

Tainan TN-1

The UIUC airfoil-usage tables record the Tainan TN-1 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 533	Goettingen	13.7%	27%	4.70%	37%
GOE 532	Goettingen	12.6%	26%	4.87%	37%

GOE 533

Goettingen series · 13.7% thick at 27% chord · 4.70% camber at 37% chord

Coordinates, polars & DXF

Also recorded on 10 other aircraft

Schleicher Ka-8B
New Standard D-24
New Standard D-25
New Standard D-26
New Standard D-27
PIK-5
Scheibe SF-28 Tandem-Falke
Schleicher Ka-2 Rhonschwalbe
Schleicher Ka-4 Rhonlerche
Schleicher Ka-7

GOE 532

Goettingen series · 12.6% thick at 26% chord · 4.87% camber at 37% chord

Coordinates, polars & DXF

Also recorded on 8 other aircraft

Horikawa H-23B-2
Schleicher Ka-8B
Horikawa H-22B-2
PIK-12
Schleicher Condor 4
Schleicher SG-38
Taylorcraft 20 Zephyr 400
Zlin 23 Honza

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