Stability. Investigation of effect of sideslip on lateral stability characteristics: 3, Rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface [with list of references]; by Thomas A. Hollingworth.
Publication Title:
Stability. Investigation of effect of sideslip on lateral stability characteristics: 3, Rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface [with list of references]; by Thomas A. Hollingworth.
Display Title:
Stability. Investigation of effect of sideslip on lateral stability characteristics: 3, Rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface [with list of references]; by Thomas A. Hollingworth.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Hollingworth, Thomas A.
Date:
[1946.]
Publish Date ISO Format:
1946-01-01T00:00:00Z
Publication Start:
19460101
Publication End:
19461231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1946
SuDoc number:
Y 3.N 21/5:11/L-17
Description:
cover title, 20 p. 3 pl. 24 p. of pl. 4°
Notes:
(Wartime report L-17.) [Processed. Originally issued Apr. 1945 as Advance restricted report L5C13a.]
Notes:
(Wartime report L-17.) [Processed. Originally issued Apr. 1945 as Advance restricted report L5C13a.] † Distribution Made by Issuing Office.