Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine /

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, August 2015.
Series:	NASA technical memorandum ; 2015-218835.
Subjects:	Detonation. Computational fluid dynamics. Inlet flow. Convergent-divergent nozzles. Potential flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo62842 http://purl.fdlp.gov/GPO/gpo62842