NASA memorandums. 10-14-58L. Effects of forebody length on stability and control characteristics at Mach number of 2.01 of canard airplane configuration with trapezoidal aspect-ratio-3 wing [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Publication Title:
Effects of forebody length on stability and control characteristics at Mach number of 2.01 of canard airplane configuration with trapezoidal aspect-ratio-3 wing [with list of references]; by M. Leroy Spearman and Cornelius Driver.
Display Title:
NASA memorandums. 10-14-58L. Effects of forebody length on stability and control characteristics at Mach number of 2.01 of canard airplane configuration with trapezoidal aspect-ratio-3 wing [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:
Nov. 1958
Publish Date ISO Format:
1958-11-01T00:00:00Z
Publication Start:
19581101
Publication End:
19581130
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
2
Publication year:
1958
SuDoc number:
NAS 1.10:(nos.)
Description:
cover title, 30 p. + [3] 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.