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

Author: Jimmy L Pittman; Gregory D Riebe; Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch,
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series: NASA technical paper, 1767.
Edition/Format:   eBook : Document : National government publication : EnglishView all editions and formats
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Genre/Form: Online resources
Electronic books
Electronic government information
Additional Physical Format: 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
(OCoLC)7325143
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
(OCoLC)711544698
Material Type: Document, Government publication, National government publication, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Jimmy L Pittman; Gregory D Riebe; Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch,
OCLC Number: 761078951
Notes: Title from title screen (viewed on Aug. 19, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Description: 1 online resource (113 pages) : illustrations.
Series Title: NASA technical paper, 1767.
Responsibility: Jimmy L. Pittman and Gregory D. Riebe.

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