Stability. Effect of wing loading and altitude on lateral stability and control characteristics of airplane as determined by tests of model in free-flight tunnel [with list of references]; by John P. Campbell and Charles L. Seacord, jr.
Publication Title:
Stability. Effect of wing loading and altitude on lateral stability and control characteristics of airplane as determined by tests of model in free-flight tunnel [with list of references]; by John P. Campbell and Charles L. Seacord, jr.
Display Title:
Stability. Effect of wing loading and altitude on lateral stability and control characteristics of airplane as determined by tests of model in free-flight tunnel [with list of references]; by John P. Campbell and Charles L. Seacord, jr.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Campbell, John P. and Seacord, Charles L. jr.
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-522
Description:
cover title, 14 p. 7 pl. 4°
Notes:
(Wartime report L-522.) [Processed. Originally issued June 1943 as Advance restricted report 3F25.]
Notes:
(Wartime report L-522.) [Processed. Originally issued June 1943 as Advance restricted report 3F25.] † Distribution Made by Issuing Office.