Computational analysis of the combustion process in an axisymmetric RBCC flowpath
By: Christopher J. Steffen, Shaye Yungster.
Contributors: Shaye Yungster.; NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210679.; NASA technical memorandum -- 210679.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2001
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Numerical analysis.; Combustion physics.; Three dimensional models.; Supersonic combustion ramjet engines.; Simulation.
Notes: Shipping list no.: 2002-0157-M.

Also available via Internet from the NASA web site. Address as of 10/8/02: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210679.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001?] 1 microfiche.