An edition of Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 (1993)

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

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Experimental aerodynamic characteristics of a ...
Ira J. Walker
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Last edited by WorkBot
January 20, 2010 | History
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An edition of Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 (1993)

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

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Publish Date
Publisher
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, National Technical Information Service, distributor]
Language
English

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Subjects

Stabilizers (Fluid dynamics), Canard configurations, Hypersonics, Aerodynamic characteristics, Delta wings, Wind tunnel tests, Research vehicles, Mach number, Hypersonic vehicles, Tail assemblies

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Cover of: Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
1993, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, National Technical Information Service, distributor]
Microform in English
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Book Details

Edition Notes

Distributed to depository libraries in microfiche.

Shipping list no.: 95-0058-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.

Published in
[Washington, DC], [Springfield, Va
Series
NASA technical memorandum -- 4413.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15403234M

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January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page