A DNS study of detonation in <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" altimg="si1.svg" display="inline" id="d1e527"><mml:mrow><mml:msub><mml:mrow><mml:mi mathvariant="normal">H</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mrow><mml:mi mathvariant="normal">O</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:math> mixture with variable-intensity turbulences-Reference-Cited by-同舟云学术

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A DNS study of detonation in H2/O2 mixture with variable-intensity turbulences

Published:2024 Issue:1-4 Volume:40 Page:105337
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Suzuki Sou^ORCID,Iwata Kazuya,Kai Reo^ORCID,Kurose Ryoichi^ORCID

Publisher

Elsevier BV

Reference24 articles.

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

2. Flight demonstration of detonation engine system using sounding rocket S-520-31: System design;Kawasaki,2022

3. Flight demonstration of detonation engine system using sounding rocket S-520-31: performance of rotating detonation engine;Goto,2022

4. Overview of performance, application, and analysis of rotating detonation engine technologies;Rankin;J. Propuls. Power,2017

5. Simulations of cellular detonation interaction with turbulent flows;Jin;AIAA J.,2016

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