Impact of dissociation and sensible heat release on pulse detonation and gas turbine engine performance /

Bibliographic Details

Main Author:	Povinelli, Louis A.
Corporate Author:	NASA Glenn Research Center
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2001]
Series:	NASA technical memorandum ; 211080.
Subjects:	Gas turbine engines. HEAT TRANSFER. Pulse detonation engines. Thermal dissociation.
Online Access:	https://purl.fdlp.gov/GPO/LPS23289