NASA memorandums. 4-4-59L. Effects of forebody deflection on stability and control characteristics of canard airplane configuration with high trapezoidal wing at Mach number of 2.01 [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Publication Title:
Effects of forebody deflection on stability and control characteristics of canard airplane configuration with high trapezoidal wing at Mach number of 2.01 [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Display Title:
NASA memorandums. 4-4-59L. Effects of forebody deflection on stability and control characteristics of canard airplane configuration with high trapezoidal wing at Mach number of 2.01 [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Series Title:
NASA memorandums.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Spearman, M. Leroy and Driver, Cornelius
Date:
Mar. 1959
Publish Date ISO Format:
1959-03-01T00:00:00Z
Publication Start:
19590301
Publication End:
19590331
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
10
Publication year:
1959
SuDoc number:
NAS 1.10:(nos.)
Description:
cover title, 28 p.+ [31 leaves, il. 4°
Notes:
[Processed. No longer confidential. Classification changed May 29, 1961.]
Notes:
[Processed. No longer confidential. Classification changed May 29, 1961.] † Distribution Made by Issuing Office.