Multiple-cycle simulation of a pulse detonation engine ejector
By: S. Yungster [and] H.D. Perkins.
Contributors: Perkins, Hugh Douglas.; NASA Glenn Research Center.
Series: NASA/TM -- 2002-211888; NASA technical memorandum -- 211888.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2002
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Pulsed detonation engine.; Unsteady reacting flows.; Computational fluid dynamics.
Other titles: Multiple cycle simulation of a pulse detonation engine ejector
Notes: Shipping list no.: 2003-0323-M.

"October 2002."

"Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002."

Also available via Internet from the NASA Web site. Address as of 8/25/04: http://gltrs.grc.nasa.gov/reports/2002/TM-2002-211888.pdf; current access available via PURL.

Microfiche. [Washington, D.C.] : Supt. of Docs., U.S. G.P.O., [2003]. 1 microfiche.