Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /

Bibliographic Details
Main Author:	Spearman, M. Leroy
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Series:	NASA technical memorandum ; 87645.
Subjects:	Space vehicles. Aerodynamics, Supersonic. Angle of attack. Cambered wings. Circular cones. Delta wings. Mach number. Planforms. Reentry vehicles. Supersonic airfoils. Transatmospheric vehicles.
Online Access:	https://purl.fdlp.gov/GPO/LPS85587

Description
Item Description:	Microform.
Physical Description:	1 volume Also available via Internet from the NTRS web site. Address as of 8/39/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006773%5F1986006773.pdf ; current access is available via PURL.