Numerical investigation of wall-pressure fluctuations for Mach 2 turbulent shock-wave boundary layer interactions
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, New Mexico State University , JH-104 1040 S. Horseshoe Street, Las Cruces, New Mexico 88003-8001, USA
Abstract
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://pubs.aip.org/aip/pof/article-pdf/doi/10.1063/5.0174397/18216395/116113_1_5.0174397.pdf
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2. Dynamic interaction between shock wave turbulent boundary layer and flexible panel;J. Fluids Struct.,2022
3. Shock induced fluid-structure interaction on a flexible wall in supersonic turbulent flow;Prog. Flight Phys.,2013
4. Full-field, dynamic pressure and displacement measurements of a panel excited by shock boundary-layer interaction,2013
5. Experiments on a thin panel excited by turbulent flow and shock/boundary-layer interactions;AIAA J.,2021
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1. Direct numerical simulation of turbulence amplification in a strong shock-wave/turbulent boundary layer interaction;Physics of Fluids;2024-01-01
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