Numerical analysis of a rotating detonation engine in the relative reference frame /

Bibliographic Details

Main Author:	Paxson, Daniel E. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2014.
Series:	NASA technical memorandum ; 2014-216634.
Subjects:	Computational fluid dynamics. Pulse detonation engines. Runge-Kutta method. Propellant combustion. Rotary engines.
Online Access:	https://purl.fdlp.gov/GPO/gpo57039 http://purl.fdlp.gov/GPO/gpo57039