Performance impact of deflagration to detonation transition enhancing obstacles /

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Bibliographic Details
Author / Creator:Paxson, Daniel E.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description:1 online resource (12 p.) : col. ill.
Language:English
Series:NASA/TM ; 2012-217629
NASA technical memorandum ; 2012-217629.
Subject:Pulse detonation engines.
Computational fluid dynamics.
Deflagration.
Heat transfer.
Aerodynamic drag.
Computational fluid dynamics.
Heat -- Transmission.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8951323
Hidden Bibliographic Details
Other authors / contributors:Schauer, Frederick F.
Hopper, David H. (David Henry), 1927-
NASA Glenn Research Center.
AIAA Aerospace Sciences Meeting (47th : 2009 : Orlando, Fla.)
Notes:Title from title screen (viewed on Dec. 3, 2012).
"July 2012."
"Prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 5-8, 2009."
"AIAA-2009-502."
Includes bibliographical references (p. 12).
Sponsored by National Aeronautics and Space Administration WBS 561581.02.08.03.17.02
E-18219
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2012-217629