Yaw (aircraft). Wind-tunnel investigation of effect of yaw on lateral-stability characteristics: 4. Symmetrically tapered wing with circular fuselage having wedge-shaped rear and vertical tail [with list of references]; by I. G. Recant and Arthur R. Wallace.
Publication Title:
Yaw (aircraft). Wind-tunnel investigation of effect of yaw on lateral-stability characteristics: 4. Symmetrically tapered wing with circular fuselage having wedge-shaped rear and vertical tail [with list of references]; by I. G. Recant and Arthur R. Wallace.
Display Title:
Yaw (aircraft). Wind-tunnel investigation of effect of yaw on lateral-stability characteristics: 4. Symmetrically tapered wing with circular fuselage having wedge-shaped rear and vertical tail [with list of references]; by I. G. Recant and Arthur R. Wallace.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Recant, I. G. and Wallace, Arthur R.
Date:
[1947.]
Publish Date ISO Format:
1947-01-01T00:00:00Z
Publication Start:
19470101
Publication End:
19471231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1947
SuDoc number:
Y 3.N 21/5:11/L-520
Description:
cover title, 14 p. 10 pl. 4°
Notes:
(Wartime report L-520.) [Processed. Originally issued-Mar. 1942 as Advance restricted report]
Notes:
(Wartime report L-520.) [Processed. Originally issued-Mar. 1942 as Advance restricted report] † Distribution Made by Issuing Office.