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

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