Stability. Effects of static margin and rotational damping in pitch on longitudinal stability characteristics of airplane as determined by tests of model in NACA free-flight tunnel [with list of references]; by John P. Campbell and John W. Paulson.
Publication Title:
Stability. Effects of static margin and rotational damping in pitch on longitudinal stability characteristics of airplane as determined by tests of model in NACA free-flight tunnel [with list of references]; by John P. Campbell and John W. Paulson.
Display Title:
Stability. Effects of static margin and rotational damping in pitch on longitudinal stability characteristics of airplane as determined by tests of model in NACA free-flight tunnel [with list of references]; by John P. Campbell and John W. Paulson.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Campbell, John P. and Paulson, John W.
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-55
Description:
cover title, 12 p. 1 pl. 6 p. of pl. 4°
Notes:
(Wartime report L-55.) [Processed, originally issued June 1944 as Advance restricted report L4F02.]
Notes:
(Wartime report L-55.) [Processed, originally issued June 1944 as Advance restricted report L4F02.] † Distribution Made by Issuing Office.