Effect of an adverse pressure gradient on hypersonic wall pressure fluctuations
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
2. School of Energy and Power Engineering, Beihang University, Beijing 100191, China
3. China Academy of Aerospace Aerodynamics, Beijing 100074, China
Funder
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
https://aip.scitation.org/doi/pdf/10.1063/5.0064594
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1. Experimental Passive Flutter Suppression Using a Linear Tuned Vibration Absorber
2. Experimental Characterization of the Flow-Induced Flutter of a Suspended Elastic Membrane
3. Aeroelastic structural acoustic coupling: Implications on the control of turbulent boundary-layer noise transmission
4. Experimental study of second-mode instability growth and breakdown in a hypersonic boundary layer using high-speed schlieren visualization
5. Experiments on the structure and scaling of hypersonic turbulent boundary layers
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