Multiple-cycle simulation of a pulse detonation engine ejector /

Bibliographic Details
Main Authors:	Yungster, Shaye (Author), Perkins, Hugh Douglas (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
Series:	NASA technical memorandum ; 2002-211888.
Subjects:	Detonable gas mixtures. Ejectors. Impulses. Mass flow rate. Pulse detonation engines. Shock waves.
Online Access:	https://purl.fdlp.gov/GPO/LPS53266

Description
Item Description:	"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." "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. "ICOMP-2002-05." "AIAA-2002-3630."
Physical Description:	1 online resource (10 pages) : illustration.
Bibliography:	Includes bibliographical references (pages 4-5).