Fuel injector design optimization for an annular scramjet geometry
By: Christopher J. Steffen, Jr.
Contributors: NASA Glenn Research Center.
Series: NASA/TM -- 2003-212094.; NASA technical memorandum -- 212094.
Publisher: NASA Glenn Research Center
Published: 2003
Place of publication: [Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Computational fluid dynamics.; Design optimization.; Fuel injection.; Injectors.; Rocket-based combined-cycle engines.; Supersonic combustion ramjet engines.
Notes: Shipping list no.: 2004-0002-M.

"January 2003."

"AIAA-2003-0651."

Also available via Internet from the NTRS web site. Address as of 1/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030014706%5F2003018462.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003]