Three-dimensional numerical thrust performance analysis of hydrogen fuel mixture rotating detonation engine with aerospike nozzle-Reference-Cited by-同舟云学术

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

Published:2019 Issue:3 Volume:37 Page:3443-3451
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Jourdaine Nicolas,Tsuboi Nobuyuki,Ozawa Kohei,Kojima Takayuki,Koichi Hayashi A.

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference27 articles.

1. Feasibility studies of a rotating detonation wave rocket motor.

2. Mathematical modeling of a rotating detonation wave in a hydrogen-oxygen mixture

3. Experimental research on the rotating detonation in gaseous fuels–oxygen mixtures

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