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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Bibliographic Details
Author / Creator:	Pittman, Jimmy L., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Description:	1 online resource (113 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1767 NASA technical paper ; 1767.
Subject:	Aerodynamics, Supersonic. Hypersonic planes. Mach number. Supersonic wind tunnels.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914244

Hidden Bibliographic Details
Other authors / contributors:	Riebe, Gregory D., author. Langley Research Center. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 19, 2016). "December 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page. Includes bibliographical references (pages 14-15). Technical paper. National Aeronautics and Space Administration 505-31-73-01 L-13868
Other form:	Print version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 Microfiche version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1767

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