Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine-Reference-Cited by-同舟云学术

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Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine

Published:2021-11 Issue: Volume:118 Page:107042
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Zhiwu,Wang Yafei,Huang Jingjing,Qin Weifeng^ORCID,Wei Lisi,Liu Zhi,Peng Changxin

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Pulse Detonation Engine Principle and Key Issues of Technology;Yan,2005

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

3. Single-head detonation propagation in a partially obstructed channel;Kellenberger;Combust. Flame,2020

4. Performance modeling of pulse detonation engines using the method of characteristics;Peace;Aerosp. Sci. Technol.,2019

5. Experimental research on vector control features of a pulse detonation tube with fluidic nozzle;Zhang;Aerosp. Sci. Technol.,2021

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1. Influence of aerodynamic valve structural parameters on detonation initiation and back pressure characteristics of air-breathing pulse detonation engine;Aerospace Science and Technology;2024-08

2. Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model;International Journal of Aeronautical and Space Sciences;2024-05-23

3. Study on back-pressure propagation and suppression of single pulse detonation;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2023-12

4. Densely connected semi-Bayesian network for machinery fault diagnosis with non-ideal data;Mechanical Systems and Signal Processing;2023-11

5. Flow characteristics and stability of induced shock waves in the isolator of rotating detonation ramjet under flight Mach number 2.5 conditions;Aerospace Science and Technology;2023-02

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