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Computational analysis of the combustion process in an axisymmetric, RBCC flowpath / Christopher J. Steffen, Shaye Yungster.

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Format:
Book
Government document
Author/Creator:
Steffen, Christopher J., author.
Yungster, Shaye, author.
Contributor:
NASA Glenn Research Center, issuing body.
Series:
NASA technical memorandum ; 2001-210679.
NASA/TM ; 2001-210679
Language:
English
Genre:
Online resources.
Physical Description:
1 online resource (15 pages) : illustrations.
Other Title:
Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath
Place of Publication:
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
Notes:
"February 2001."
"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Includes bibliographical references (page 15).
Online resource; title from PDF title page (NASA, viewed Nov. 20, 2017).
Other Format:
Microfiche version: Steffen, Christopher J. Computational analysis of the combustion process in an axisymmetric RBCC flowpath
OCLC:
1012398455

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