NASA memorandums. 10-2-58L. Aerodynamic characteristics for combined angles of attack and sideslip of low-aspect-ratio cruciform-wing missile configuration employing various canard and trailing-edge flap controls at Mach number of 2.01 [with list of references]; by Ross B. Robinson and M. Leroy Spearman.
Publication Title:
Aerodynamic characteristics for combined angles of attack and sideslip of low-aspect-ratio cruciform-wing missile configuration employing various canard and trailing-edge flap controls at Mach number of 2.01 [with list of references]; by Ross B. Robinson and M. Leroy Spearman.
Display Title:
NASA memorandums. 10-2-58L. Aerodynamic characteristics for combined angles of attack and sideslip of low-aspect-ratio cruciform-wing missile configuration employing various canard and trailing-edge flap controls at Mach number of 2.01 [with list of references]; by Ross B. Robinson and M. Leroy Spearman.
Series Title:
NASA memorandums.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Robinson, Ross B. and Spearman, M. Leroy
Date:
Oct. 1958
Publish Date ISO Format:
1958-10-01T00:00:00Z
Publication Start:
19581001
Publication End:
19581031
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
3
Publication year:
1958
SuDoc number:
NAS 1.10:(nos.)
Description:
cover title, 71+[1] p. il. 4°
Notes:
[Declassified Oct. 25, 1962.]
Notes:
[Declassified Oct. 25, 1962.] Φ For Sale by OTS, Commerce Dept. Paper, $2.00.