Impact of an exhaust throat on semi-idealized rotating detonation engine performance /

Bibliographic Details
Main Author:	Paxson, Daniel E. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.
Series:	NASA technical memorandum ; 2016-219076.
Subjects:	Computational fluid dynamics. Exhaust flow simulation. Fuel flow. Inviscid flow. Propulsion system performance.
Online Access:	https://purl.fdlp.gov/GPO/gpo68694 http://purl.fdlp.gov/GPO/gpo68694

Description
Item Description:	Title from title screen (viewed on June 8, 2016). "April 2016." "Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016." "AIAA-2016-11647."
Physical Description:	1 online resource (12 pages) : color illustrations.
Bibliography:	Includes bibliographical references (pages 11-12).