NACA research memorandum RM (series). L58A20. Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Publication Title:
Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Display Title:
NACA research memorandum RM (series). L58A20. Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Spearman, M. Leroy and Driver, Cornelius
Date:
Mar. 10, 1958
Publish Date ISO Format:
1958-03-10T00:00:00Z
Publication Start:
19580310
Publication End:
19580310
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
10
Publication year:
1958
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 51 + [4] p. il. 4°
Notes:
[Classification changed Oct. 28, 1960.] and (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed. No longer confidential.] † Distribution Made by Issuing Office.