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＜journal article＞
Initiation Characteristics of Rotating Supersonic Combustion Engine

Creator
Creator Name
Muhammad Amri Mazlan
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Creator Name
Mohd Fairus Mohd Yasin
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Creator Name
Aminuddin Saat
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Creator Name
Mazlan Abdul Wahid
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Creator Name
Ahmad Dairobi Ghazali
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Creator Name
Mohammad Nurizat Rahman
Affiliation
Affiliation Name
High Speed Reacting Flow Laboratory, School of Mechanical Engineering, Universiti Tecknologi Malaysia
Language
English
Publisher
Transdisciplinary Research and Education Center for Green Technologies, Kyushu University
九州大学グリーンテクノロジー研究教育センター
Date
2021-03
Source Title
Evergreen
Vol
8
Issue
1
First Page
177
Last Page
181
Publication Type
Version of Record
Access Rights
open access
Crossref DOI
https://doi.org/10.5109/4372275
Rights
Creative Commons Attribution-NonCommercial 4.0 International
Abstract A rotating supersonic combustion engine (RSCE) is tested with various initiator tube positions along the combustion chamber to determine its impact on the ignition process. The type of fuel used is me...thane with oxygen as the oxidizer. The initiation of RSCE is assessed for nearstoichiometric methane-oxygen mixture to slightly rich mixture. Successful initiation of rotating supersonic combustion in the RSCE was obtained when the position of the initiator tube is located higher end of the combustion chamber that indicates a proper mixing of reactants. The mixing of reactants improves further up the annulus chamber of the RSCE.show more

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pdf Pages_177-181 pdf 1.21 MB 401  

Details

PISSN
2189-0420
EISSN
2432-5953
Record ID
4372275
Peer-Reviewed
Refereed
Subject Terms
evergreen
rotating detonation engine
pre-detonator
supersonic combustion
Created Date 2021.04.02
Modified Date 2024.02.21

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