Multiple-cycle simulation of a pulse detonation engine ejector /

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Bibliographic Details
Author / Creator:Yungster, Shaye.
Imprint:[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
Description:1 v.
Series:NASA/TM ; 2002-211888
NASA technical memorandum ; 211888.
Subject:Pulse detonation engines.
Unsteady reacting flows.
Computational fluid dynamics.
Fluid dynamics.
Unsteady flow (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
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Varying Form of Title:Multiple cycle simulation of a pulse detonation engine ejector
Other authors / contributors:Perkins, Hugh Douglas.
NASA Glenn Research Center.
Notes:"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."
Available via Internet from the NASA Web site. Address as of 8/25/04:; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online) classification:NAS 1.15:211888 NAS 1.15:2002-211888