Three-dimensional numerical study on rotating detonation engines using reactive Navier-Stokes equations-Reference-Cited by-同舟云学术

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Three-dimensional numerical study on rotating detonation engines using reactive Navier-Stokes equations

Published:2019-10 Issue: Volume:93 Page:105271
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Li-Feng,Ma John Z.,Zhang Shu-Jie,Luan Ming-Yi,Wang Jian-Ping

Funder

National Natural Science Foundation of China

State Key Laboratory of High Temperature Gas Dynamics

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Detonative propulsion;Wolański;Proc. Combust. Inst.,2013

2. Airbreathing rotating detonation wave engine cycle analysis;Braun;Aerosp. Sci. Technol.,2013

3. Recent developments in the research on rotating-detonation-wave engines;Kailasanath,2017

4. Experimental research on ignition, quenching, reinitiation and the stabilization process in rotating detonation engine;Ma;Int. J. Hydrog. Energy,2018

5. Experimental research on rotating detonation in liquid fuel–gaseous air mixtures;Kindracki;Aerosp. Sci. Technol.,2015

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