Thermoacoustic Instabilities in an Annular Rotating Detonation Combustor Under Off-Design Condition-Reference-Cited by-同舟云学术

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Thermoacoustic Instabilities in an Annular Rotating Detonation Combustor Under Off-Design Condition

Published:2019-01 Issue:1 Volume:35 Page:141-151
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Xie Qiaofeng¹,Wang Bing¹,Wen Haocheng¹,He Wei¹

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Tsinghua University Initiative Scientific Research Program

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B37044

Reference33 articles.

1. Recent Developments in the Research on Pulse Detonation Engines

2. Experimental Investigation of H2-Air Mixtures in a Rotating Detonation Combustor

3. Detonative propulsion

4. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts

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1. Air-breathing rotating detonation engine supplied with liquid kerosene: propulsive performance and combustion stability;Shock Waves;2024-04

2. Experimental investigation on rotating detonation engine with full/half inner cylinder;Acta Astronautica;2023-11

3. On the Potentials of the Integration of Pressure Gain Combustion with a Hybrid Electric Propulsion System;Aerospace;2023-08-15

4. Predicting combustion behavior in rotating detonation engines using an interpretable deep learning method;Physics of Fluids;2023-07-01

5. Experimental investigation of ethylene-fueled ramjet rotating detonation engine with an annular combustor;Journal of Physics: Conference Series;2023-06-01

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