Nonlinear shock-induced flutter of a compliant panel using a fully coupled fluid-thermal-structure interaction model-Reference-Cited by-同舟云学术

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Nonlinear shock-induced flutter of a compliant panel using a fully coupled fluid-thermal-structure interaction model

Published:2024-01 Issue: Volume:124 Page:104047
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Shahriar Al^ORCID,Shoele Kourosh^ORCID

Funder

Defense Advanced Research Projects Agency

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference94 articles.

1. Zones of influence and shock motion in a shock/boundary-layer interaction;Agostini;AIAA J.,2012

2. Large-eddy simulation of broadband unsteadiness in a shock/boundary-layer interaction;Aubard;AIAA J.,2013

3. Shock Wave-Boundary-Layer Interactions, Vol. 32;Babinsky,2011

4. Numerical Experiments on the Flow Past a Circular Cylinder at Sub-Critical Reynolds Number;Beaudan,1994

5. Shock wave transitional boundary-layer interactions in hypersonic flow;Benay;AIAA J.,2006

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1. Numerical investigation of fluid-thermal-structural interaction of deployable control fin in hypersonic flow;Physics of Fluids;2024-08-01

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