Experimental and numerical investigation on flame propagation and transition to detonation in curved channel-Reference-Cited by-同舟云学术

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Experimental and numerical investigation on flame propagation and transition to detonation in curved channel

Published:2021-11 Issue: Volume:118 Page:107036
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Pan Zhenhua,Zhang Zenghai,Yang Huaiyuan,Gui Mingyue,Zhang Penggang,Zhu Yuejin

Funder

State Key Laboratory of Engines

National Natural Science Foundation of China

Tianjin University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Pulse detonation propulsion: challenges, current status, and future perspective;Roy;Prog. Energy Combust.,2004

2. Investigation of pulse detonation combustors – axial turbine system;Anand;Aerosp. Sci. Technol.,2019

3. Effects of the combustor width on propagation characteristics of rotating detonation waves;Wang;Aerosp. Sci. Technol.,2020

4. Study on a liquid-fueled and valveless pulse detonation rocket engine without the purge process;Wang;Energy,2014

5. Numerical study of the influence of annular width on the rotating detonation wave in a non-premixed combustor;Zhao;Aerosp. Sci. Technol.,2020

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