Input/output analysis of hypersonic boundary layers using hybridizable discontinuous Galerkin methods

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

We investigate hypersonic boundary layer instability and receptivity for using Input/Output (I/O) analysis. Our approach directly incorporates of effects of multiple modes of instability as well as a model of shock/perturbation interaction to capture receptivity to freestream perturbations. While I/O analysis removes restrictive assumptions underpinning other stability analyses, it requires the solution of large (but sparse) linear systems, and the computational expense remains a pacing challenge. To address this issue, we develop I/O analysis based upon hybridizable discontinuous Galerkin (HDG) methods. HDG provides high-order accuracy and optimal static condensation on unstructured meshes that together significantly reduce the number of degrees of freedom required. We also investigate HDG methods applied to non-conforming meshes that often result from adaptive mesh refinement.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107115
StatePublished - 2024
EventAIAA SciTech Forum and Exposition, 2024 - Orlando, United States
Duration: Jan 8 2024Jan 12 2024

Publication series

NameAIAA SciTech Forum and Exposition, 2024

Conference

ConferenceAIAA SciTech Forum and Exposition, 2024
Country/TerritoryUnited States
CityOrlando
Period1/8/241/12/24

Bibliographical note

Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

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