Three-dimensional numerical thrust performance analysis of hydrogen fuel mixture rotating detonation engine with aerospike nozzle

Published 2018 View Full Article

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Title
Three-dimensional numerical thrust performance analysis of hydrogen fuel mixture rotating detonation engine with aerospike nozzle
Authors
Keywords
Detonation engine, Numerical simulation, Aerospike nozzle, Shock wave
Journal
PROCEEDINGS OF THE COMBUSTION INSTITUTE
Volume -, Issue -, Pages -
Publisher
Elsevier BV
Online
2018-10-02
DOI
10.1016/j.proci.2018.09.024

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