Numerical Investigation of Flow Acoustic Coupling in a Half-Dump Combustor
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology, Kanpur 208 016, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35629
Reference31 articles.
1. Combustion dynamics and control: Progress and challenges
2. Vortex-driven acoustically coupled combustion instabilities
3. Combustion instabilities coupled by pressure waves and their active control
4. Combustion instability related to vortex shedding in dump combustors and their passive control
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. The Rayleigh integral is always positive in steadily operated combustors;Proceedings of the Combustion Institute;2022-10
2. Numerical Investigation of Flow-Acoustics Coupling in a Half-Dump Combustor Using Hybrid CFD-CAA Methodology;Green Energy and Technology;2021-08-08
3. Effect of vortex and entropy sources in sound generation for compressible cavity flow;Physics of Fluids;2021-04
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