Flow characteristics and stability of induced shock waves in the isolator of rotating detonation ramjet under flight Mach number 2.5 conditions-Reference-Cited by-同舟云学术

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Flow characteristics and stability of induced shock waves in the isolator of rotating detonation ramjet under flight Mach number 2.5 conditions

Published:2023-02 Issue: Volume:133 Page:108092
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wu Qianmin^ORCID,Lin Zhiyong^ORCID,Huang Xixuan^ORCID,Zhang Dingrui

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

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

2. Rotating detonation combustors and their similarities to rocket instabilities;Anand;Prog. Energy Combust. Sci.,2019

3. Recent progress, development trends, and consideration of continuous detonation engines;Ma;AIAA J.,2020

4. Prediction of detonation initiation in an air-breathing pulse detonation combustor utilizing a simplified ethylene-air reaction mechanism;Sun;Aerosp. Sci. Technol.,2022

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

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical study on the flow characteristics and stability in the isolator of rotating detonation ramjet engine by different combustion modes and structure parameters;Aerospace Science and Technology;2024-04

2. Experimental study on suppressing pressure feedback and combustion product backflow of the rotating detonation engine;Aerospace Science and Technology;2023-10

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