Yaw (aircraft). Experimental determination of yawing moment due to yawing contributed by wing, fuselage, and vertical tail of midwing airplane model [with list of references]; by John P. Campbell and Ward O. Mathews.
Publication Title:
Yaw (aircraft). Experimental determination of yawing moment due to yawing contributed by wing, fuselage, and vertical tail of midwing airplane model [with list of references]; by John P. Campbell and Ward O. Mathews.
Display Title:
Yaw (aircraft). Experimental determination of yawing moment due to yawing contributed by wing, fuselage, and vertical tail of midwing airplane model [with list of references]; by John P. Campbell and Ward O. Mathews.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Campbell, John P. and Mathews, Ward O.
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-387
Description:
cover title, 12 p. 5 pl. 4°
Notes:
(Wartime report L-387.) [Processed. Originally issued June 1943 as Advance restricted report 3F28.]
Notes:
(Wartime report L-387.) [Processed. Originally issued June 1943 as Advance restricted report 3F28.] † Distribution Made by Issuing Office.