NACA research memorandum RM (series). L56D04. Static longitudinal stability and control characteristics of model of 45° swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01 [with list of references]; by Cornelius Driver and Gerald V. Foster.
Publication Title:
Static longitudinal stability and control characteristics of model of 45° swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01 [with list of references]; by Cornelius Driver and Gerald V. Foster.
Display Title:
NACA research memorandum RM (series). L56D04. Static longitudinal stability and control characteristics of model of 45° swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01 [with list of references]; by Cornelius Driver and Gerald V. Foster.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Driver, Cornelius and Foster, Gerald V.
Date:
July 11, 1956
Publish Date ISO Format:
1956-07-11T00:00:00Z
Publication Start:
19560711
Publication End:
19560711
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
6
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 20 p. + [21 leaves. il. 4°
Notes:
[No longer confidential. Classification changed Sept. 1, 1959.] and (National Advisory Committee for Aeronautics.) [Processed.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed.] † Distribution Made by Issuing Office.