NASA memorandums. 4-21-59A. Longitudinal stability and control characteristics at Mach numbers from 0.70 to 2.22 of triangular wing configuration equipped with canard control, trailing-edge flap control, or cambered forebody [with list of references]; by John W. Boyd and Gene P. Menees.
Publication Title:
Longitudinal stability and control characteristics at Mach numbers from 0.70 to 2.22 of triangular wing configuration equipped with canard control, trailing-edge flap control, or cambered forebody [with list of references]; by John W. Boyd and Gene P. Menees.
Display Title:
NASA memorandums. 4-21-59A. Longitudinal stability and control characteristics at Mach numbers from 0.70 to 2.22 of triangular wing configuration equipped with canard control, trailing-edge flap control, or cambered forebody [with list of references]; by John W. Boyd and Gene P. Menees.
Series Title:
NASA memorandums.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Boyd, John W. and Menees, Gene P.
Date:
Apr. 1959
Publish Date ISO Format:
1959-04-01T00:00:00Z
Publication Start:
19590401
Publication End:
19590430
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
9
Publication year:
1959
SuDoc number:
NAS 1.10:(nos.)
Description:
cover title, 39 p.+[2] 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.