NACA research memorandum RM (series). L50B09. Wing-flow measurements of longitudinal stability and control characteristics of supersonic airplane configuration having 42.8° swept-back circular are wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces [with list of references]; by Harold L. Crane and James J. Adams.
Publication Title:
Wing-flow measurements of longitudinal stability and control characteristics of supersonic airplane configuration having 42.8° swept-back circular are wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces [with list of references]; by Harold L. Crane and James J. Adams.
Display Title:
NACA research memorandum RM (series). L50B09. Wing-flow measurements of longitudinal stability and control characteristics of supersonic airplane configuration having 42.8° swept-back circular are wing with aspect ratio 4.0, taper ratio 0.50, and sweptback tail surfaces [with list of references]; by Harold L. Crane and James J. Adams.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Crane, Harold L. and Adams, James J.
Date:
Apr. 3, 1950
Publish Date ISO Format:
1950-04-03T00:00:00Z
Publication Start:
19500403
Publication End:
19500403
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
9
Publication year:
1950
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 40+[4] p. il. 4°
Notes:
[No longer confidential. Classification changed May 29, 1959.] and (National Advisory Committee for Aeronautics.) [Processed.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed.] † Distribution Made by Issuing Office.