Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
By: M. Leroy Spearman.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 87645.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1985
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Space vehicles.; Aerodynamics, Supersonic.; Angle of attack.; Cambered wings.; Circular cones.; Delta wings.; Mach number.; Planforms.; Reentry vehicles.; Supersonic airfoils.; Transatmospheric vehicles.
Notes: 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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.