Tail (aircraft). Two-dimensional wind-tunnel investigation of 10.7-percent-thick symmetrical tail section with A 0.40 airfoil-chord control surface and A 0.20 controlsurface-chord tab [with list of references]; by Albert L. Braslow.
Publication Title:
Tail (aircraft). Two-dimensional wind-tunnel investigation of 10.7-percent-thick symmetrical tail section with A 0.40 airfoil-chord control surface and A 0.20 controlsurface-chord tab [with list of references]; by Albert L. Braslow.
Display Title:
Tail (aircraft). Two-dimensional wind-tunnel investigation of 10.7-percent-thick symmetrical tail section with A 0.40 airfoil-chord control surface and A 0.20 controlsurface-chord tab [with list of references]; by Albert L. Braslow.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Braslow, Albert L.
Date:
June 1947
Publish Date ISO Format:
1947-06-01T00:00:00Z
Publication Start:
19470601
Publication End:
19470630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1947
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/1228
Description:
cover title, 14 p. 2 pl. 22 p. of pl. 4°
Notes:
(Technical note 1228.) [Processed.]
Notes:
(Technical note 1228.) [Processed.] † Distribution Made by Issuing Office.