Numerical investigation of the bevelled effects on shock structure and screech noise in planar supersonic jets
Author:
Affiliation:
1. Department of Modern Mechanics, University of Science and Technology of China, Hefei 230027, China
2. Key Laboratory of Aerodynamic Noise Control, China Aerodynamics Research and Development Center, Mianyang 621000, China
Funder
Open Fund of Key Laboratory of Aerodynamic Noise Control
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0013263
Reference31 articles.
1. Supersonic Jet Noise
2. Numerical simulation of the three-dimensional screech phenomenon from a circular jet
3. Instability modes excited by natural screech tones in a supersonic rectangular jet
4. Antisymmetric Oscillation Modes in Rectangular Screeching Jets
5. Structure of a screeching rectangular jet: a stereoscopic particle image velocimetry study
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