Shear layer synchronization of aerodynamically isolated opposite cavities due to acoustic resonance excitation-Reference-Cited by-同舟云学术

Shear layer synchronization of aerodynamically isolated opposite cavities due to acoustic resonance excitation

Published:2021-05 Issue:5 Volume:33 Page:055112
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Abdelmwgoud Moamenbellah¹^ORCID,Shaaban Mahmoud¹^ORCID,Mohany Atef¹^ORCID

Affiliation:

1. Aeroacoustics and Noise Control Laboratory, University of Ontario Institute of Technology, 2000 Simcoe Street North, Oshawa, Ontario L1G 0C5, Canada

Funder

Natural Sciences and Engineering Research Council of Canada

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0051226

Reference58 articles.

1. Flow-Excited Acoustic Resonance Excitation Mechanism, Design Guidelines, and Counter Measures

2. A Theory on the Onset of Acoustic Resonance in a Multistage Compressor

3. Effects of modifying the blade trailing edge profile on unsteady pressure pulsations and flow structures in a centrifugal pump

4. Influence of Nozzle Cavity on Indirect Vortex- and Entropy-Sound Production

5. Characteristics of Acoustic Resonance Excitation by Flow Around Inline Cylinders

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