NASA technical notes. D-1203. 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 technical notes. D-1203. 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 technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Spearman, M. Leroy and Driver, Cornelius
Date:
Apr. 1962
Publish Date ISO Format:
1962-04-01T00:00:00Z
Publication Start:
19620401
Publication End:
19620430
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
9
Publication year:
1962
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 80 p. +[2] leaves, il. 4°
Notes:
[Supersedes declassified NASA memorandum 10-14-58L 1958.] and [Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 75c.