Investigation of Harmonic Response in Non-Premixed Swirling Combustion to Low-Frequency Acoustic Excitations
Author:
Affiliation:
1. School of Mechanical Engineering, Tongji University, Shanghai 201804, China
2. Postdoctoral Station of Mechanical Engineering, Tongji University, Shanghai 201804, China
Abstract
Funder
National Natural Science Foundation of China
Science and Technology Commission of Shanghai Municipality
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/9/812/pdf
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2. Sun, Y., Zhao, D., and Zhu, X. (2021). Generation and Mitigation mechanism studies of nonlinear thermoacoustic instability in a modelled swirling combustor with a heat exchanger. Aerospace, 8.
3. A mechanism for high-frequency oscillation in ramjet combustors and afterburners;Rogers;J. Jet Propuls.,1956
4. The effects of highly exothermic chemical reaction on a two-dimensional mixing layer;Keller;AIAA J.,1985
5. A review of oscillation mechanisms and the role of the precessing vortex core (PVC) in swirl combustion systems;Syred;Prog. Energy Combust. Sci.,2006
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