Direct Simulation of Fluid-Structure Interaction in Compression Ramp with Embedded Compliant Panel
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Reference61 articles.
1. A Structures Perspective on the Challenges Associated with Analyzing a Reusable Hypersonic Platform
2. Full-field, dynamic pressure and displacement measurements of a panel excited by shock boundary-layer interaction
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1. Experimental Investigation on the Control of Hypersonic Shock Wave/Boundary Layer Interaction Using Surface Arc Plasma Actuators at Double Compression Corner;Aerospace;2023-12-06
2. Fluid–structural coupling of an impinging shock–turbulent boundary layer interaction at Mach 3 over a flexible panel;Flow;2022
3. Impact of Panel Vibrations on the Dynamic Field Properties in Supersonic flow;AIAA AVIATION 2021 FORUM;2021-07-28
4. Direct Simulation of Fluid–Structure Interaction in a Hypersonic Compression-Ramp Flow;AIAA Journal;2020-11
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