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