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Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 / by Robert J. McGhee and James A. Martin.

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Format:
Book
Government document
Author/Creator:
McGhee, Robert J., author.
Martin, James A., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Langley Research Center
Series:
NASA technical note ; D-5030.
NASA technical note ; D-5030
Language:
English
Subjects (All):
Aerodynamics, Supersonic.
Supersonic nozzles.
Mach number.
Physical Description:
1 online resource (39 pages) : illustrations.
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, March 1969.
Notes:
"March 1969."
Includes bibliographical references (page 11).
Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 16, 2020).
Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2024.
Other Format:
Print version: McGhee, Robert J. Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0.
OCLC:
761185708
Access Restriction:
Use copy Restrictions unspecified

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