Investigations on the competition between acoustic and intrinsic thermoacoustic modes due to multi-flame interaction

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Siyi Zhang , Xiaokang Liu , Yu Tian , Dongbin Wang , Jingxuan Li , Lijun Yang
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引用次数: 0

Abstract

Thermoacoustic instabilities typically consist of two modes: the acoustic instability mode and the intrinsic thermoacoustic (ITA) mode. These modes can coexist and compete under certain conditions within a combustor. This paper investigates the impact of multi-flame interaction on mode competition within a model combustor – a length-adjustable Rijke tube. Mode competition was explored by independently varying the chamber's acoustic characteristics (via Rijke tube length) and the multi-flame response characteristics (through injector hole distribution). The thermoacoustic response of the multi-flame system was examined using an acoustic pressure sensor and CH* chemiluminescence technique. The dynamic properties of the multi-flame flow field were captured with a high-speed camera and particle image velocimetry (PIV). Results showed that different multi-flame interactions can alter the flame transfer function (FTF), leading to combustion instability dominated by either the acoustic mode or the ITA mode. The experimental results were combined with a low-order acoustic network model (LOM) to study the transition and competition between acoustic and ITA instability under multi-flame interactions. The predictions of the LOM for the eigenfrequencies and growth rates of the combustion system can accurately describe the occurrence trend of the acoustic and ITA modes.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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