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Review on the Rotating Detonation Engine and It’s Typical Problems

Qiaofeng Xie Orcid Logo, Zifei Ji Orcid Logo, Haocheng Wen Orcid Logo, Zhaoxin Ren Orcid Logo, Piotr Wolanski Orcid Logo, Bing Wang Orcid Logo

Transactions on Aerospace Research, Volume: 2020, Issue: 4, Pages: 107 - 163

Swansea University Author: Zhaoxin Ren Orcid Logo

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DOI (Published version): 10.2478/tar-2020-0024

Abstract

Detonation is a promising combustion mode to improve engine performance, increase combustion efficiency, reduce emissions, and enhance thermal cycle efficiency. Over the last decade, significant progress has been made towards the applications of detonation mode in engines, such as standing detonatio...

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Published in: Transactions on Aerospace Research
ISSN: 2545-2835
Published: Walter de Gruyter GmbH 2020
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URI: https://cronfa.swan.ac.uk/Record/cronfa59346
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first_indexed 2022-02-22T11:54:18Z
last_indexed 2022-02-23T04:27:45Z
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spelling 2022-02-22T11:57:41.5803185 v2 59346 2022-02-11 Review on the Rotating Detonation Engine and It’s Typical Problems 62a1a0da0fa78e05c3deafcdee5551ce 0000-0002-6305-9515 Zhaoxin Ren Zhaoxin Ren true false 2022-02-11 AERO Detonation is a promising combustion mode to improve engine performance, increase combustion efficiency, reduce emissions, and enhance thermal cycle efficiency. Over the last decade, significant progress has been made towards the applications of detonation mode in engines, such as standing detonation engine (SDE), Pulse detonation engine (PDE) and rotating detonation engine (RDE), and the understanding of the fundamental chemistry and physics processes in detonation engines via experimental and numerical studies. This article is to provide a comprehensive overview of the progress in the knowledge of rotating detonation engine from the different countries. New observations of injection, ignition, and geometry of combustor, pressure feedback, and combustion modes of RDE have been reported. These findings and advances have provided new opportunities in the development of rotating detonation for practical applications. Finally, we point out the current gaps in knowledge to indicate which areas future research should be directed at. Journal Article Transactions on Aerospace Research 2020 4 107 163 Walter de Gruyter GmbH 2545-2835 Detonation; propulsion system; rotating detonation 31 12 2020 2020-12-31 10.2478/tar-2020-0024 COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University The authors thank the support from the National Natural Science Foundation of China (No. 51676111), the China Postdoctoral Science Foundation (No. 2018M640140) and the China Postdoctoral Science Special Foundation (No. 2019T120100). 2022-02-22T11:57:41.5803185 2022-02-11T01:05:54.6618771 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering Qiaofeng Xie 0000-0001-6807-7731 1 Zifei Ji 0000-0002-8729-3111 2 Haocheng Wen 0000-0002-5460-9247 3 Zhaoxin Ren 0000-0002-6305-9515 4 Piotr Wolanski 0000-0003-3963-7722 5 Bing Wang 0000-0003-3373-7351 6 59346__22422__0f630557fdb14d499539f2feb01c96c0.pdf 59346.pdf 2022-02-22T11:56:01.0611905 Output 21346716 application/pdf Version of Record true © 2020 Qiaofeng Xie et al., This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License true eng https://creativecommons.org/licenses/by-nc-nd/3.0/
title Review on the Rotating Detonation Engine and It’s Typical Problems
spellingShingle Review on the Rotating Detonation Engine and It’s Typical Problems
Zhaoxin Ren
title_short Review on the Rotating Detonation Engine and It’s Typical Problems
title_full Review on the Rotating Detonation Engine and It’s Typical Problems
title_fullStr Review on the Rotating Detonation Engine and It’s Typical Problems
title_full_unstemmed Review on the Rotating Detonation Engine and It’s Typical Problems
title_sort Review on the Rotating Detonation Engine and It’s Typical Problems
author_id_str_mv 62a1a0da0fa78e05c3deafcdee5551ce
author_id_fullname_str_mv 62a1a0da0fa78e05c3deafcdee5551ce_***_Zhaoxin Ren
author Zhaoxin Ren
author2 Qiaofeng Xie
Zifei Ji
Haocheng Wen
Zhaoxin Ren
Piotr Wolanski
Bing Wang
format Journal article
container_title Transactions on Aerospace Research
container_volume 2020
container_issue 4
container_start_page 107
publishDate 2020
institution Swansea University
issn 2545-2835
doi_str_mv 10.2478/tar-2020-0024
publisher Walter de Gruyter GmbH
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 1
active_str 0
description Detonation is a promising combustion mode to improve engine performance, increase combustion efficiency, reduce emissions, and enhance thermal cycle efficiency. Over the last decade, significant progress has been made towards the applications of detonation mode in engines, such as standing detonation engine (SDE), Pulse detonation engine (PDE) and rotating detonation engine (RDE), and the understanding of the fundamental chemistry and physics processes in detonation engines via experimental and numerical studies. This article is to provide a comprehensive overview of the progress in the knowledge of rotating detonation engine from the different countries. New observations of injection, ignition, and geometry of combustor, pressure feedback, and combustion modes of RDE have been reported. These findings and advances have provided new opportunities in the development of rotating detonation for practical applications. Finally, we point out the current gaps in knowledge to indicate which areas future research should be directed at.
published_date 2020-12-31T04:16:35Z
_version_ 1763754110398496768
score 11.01628

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