Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance
By: Louis A. Povinelli.
Contributors: NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-211080.; NASA technical memorandum -- 211080.
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: Gas turbine engines.; Heat transfer.; Pulse detonation engines.; Thermal dissociation.
Notes: Shipping list no.: 2002-0336-M.

Also available via Internet from the NASA web site. Address as of 10/16/02: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-211080.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.