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

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Bibliographic Details
Author / Creator:Spearman, M. Leroy.
Imprint:Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Description:1 volume.
Language:English
Series:NASA technical memorandum ; 87645
NASA technical memorandum ; 87645.
Subject:
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6808503
Hidden Bibliographic Details
Other authors / contributors:Langley Research Center.
Notes: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.
GPO item no.:0830-D (MF)
Govt.docs classification:NAS 1.15:87645

MARC

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245 1 0 |a Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /  |c M. Leroy Spearman. 
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650 0 |a Space vehicles. 
650 0 |a Aerodynamics, Supersonic. 
650 7 |a Angle of attack.  |2 nasat 
650 7 |a Cambered wings.  |2 nasat 
650 7 |a Circular cones.  |2 nasat 
650 7 |a Delta wings.  |2 nasat 
650 7 |a Mach number.  |2 nasat 
650 7 |a Planforms.  |2 nasat 
650 7 |a Reentry vehicles.  |2 nasat 
650 7 |a Supersonic airfoils.  |2 nasat 
650 7 |a Transatmospheric vehicles.  |2 nasat 
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