Ailerons. Theoretical analysis of effect of aileron inertia and hinge moment on maximum rolling acceleration of airplanes in abrupt aileron rolls; by F. J. Bailey, jr. and William J. O'Sullivan.
Publication Title:
Ailerons. Theoretical analysis of effect of aileron inertia and hinge moment on maximum rolling acceleration of airplanes in abrupt aileron rolls; by F. J. Bailey, jr. and William J. O'Sullivan.
Display Title:
Ailerons. Theoretical analysis of effect of aileron inertia and hinge moment on maximum rolling acceleration of airplanes in abrupt aileron rolls; by F. J. Bailey, jr. and William J. O'Sullivan.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Bailey, F. J. jr. and O'Sullivan, William J.
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-302
Description:
cover title, 13 p. 3 pl. 4°
Notes:
(Wartime report L-302.) [Processed. Originally issued Feb. 1942 as Advance restricted report.]
Notes:
(Wartime report L-302.) [Processed. Originally issued Feb. 1942 as Advance restricted report.] † Distribution Made by Issuing Office.