Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 /

Bibliographic Details

Main Author:	Foster, Gerald V. (Author)
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, [November 1959]
Series:	NASA technical memorandum ; X-134.
Subjects:	Aerodynamic characteristics. Hypersonic vehicles. Aerodynamics, Supersonic. Supersonic wind tunnels.
Online Access:	https://purl.fdlp.gov/GPO/gpo182862