Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63

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Experimental and theoretical aerodynamic char ...
Jimmy L. Pittman
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December 15, 2009 | History

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63

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Cover of: Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
Cover of: Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English

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Book Details


Edition Notes

"Langley Research Center."

Dec. 1980.

Includes bibliographical references.

Published in
[Washington, D.C.], [Springfield, Va
Series
NASA technical paper -- 1767.

The Physical Object

Pagination
113 p. :
Number of pages
113

ID Numbers

Open Library
OL17823250M

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December 15, 2009 Edited by WorkBot link works
October 1, 2008 Created by ImportBot Imported from Oregon Libraries MARC record