Technical note 1257-1423 (with omissions). 1406. High-speed wind-tunnel tests of NACA 16-009 airfoil having 32.9-percent chord flap with overhang 20.7 percent of flap chord [having list of references]; by David B. Stevenson and Robert W. Byrne.
Publication Title:
High-speed wind-tunnel tests of NACA 16-009 airfoil having 32.9-percent chord flap with overhang 20.7 percent of flap chord [having list of references]; by David B. Stevenson and Robert W. Byrne.
Display Title:
Technical note 1257-1423 (with omissions). 1406. High-speed wind-tunnel tests of NACA 16-009 airfoil having 32.9-percent chord flap with overhang 20.7 percent of flap chord [having list of references]; by David B. Stevenson and Robert W. Byrne.
Series Title:
Technical note 1257-1423 (with omissions).
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Stevenson, David B. and Byrne, Robert W.
Date:
Aug. 1947
Publish Date ISO Format:
1947-08-01T00:00:00Z
Publication Start:
19470801
Publication End:
19470831
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
5
Publication year:
1947
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/1257, etc.
Description:
cover title, 8 p. 2 pl. 28 p. of pl. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.