Numerical simulation of a Rotating Detonation with a realistic injector designed for separate supply of gaseous hydrogen and oxygen-Reference-Cited by-同舟云学术

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Numerical simulation of a Rotating Detonation with a realistic injector designed for separate supply of gaseous hydrogen and oxygen

Published:2017-12 Issue: Volume:141 Page:64-78
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gaillard T.,Davidenko D.,Dupoirieux F.

Funder

General Scientific Direction of ONERA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Stationary spin detonation;Voitsekhovskii;Sov. J. Appl. Mech. Tech. Phys.,1960

2. The Feasability of a Rotating Detonation Wave Rocket Motor, Tech. Rep;Nicholls,1964

3. Perfomance analysis of a rotating detonation wave rocket engine;Adamson;Acta Astronaut.,1967

4. Detonative propulsion;Wolanski;Proc. Combust. Inst.,2013

5. Rotating detonation wave propulsion: experimental challenges, modeling, and engine concepts;Lu;J. Propuls. Power,2014

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