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Applying compressible transformations to wall modeled LES of cold wall flat plate boundary layers

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

Existing near-wall turbulence models for WMLES are usually extended to cold wall, compressible flows with heat transfer by using empirical modifications to the algebraically defined eddy viscosity. This work seeks to define an alternative, rational modification supported by canonical compressible boundary layer scaling laws. Recently developed compressible velocity transformations have been shown to collapse data to the incompressible law of the wall. These transformations also imply a form for the compressible eddy viscosity. We propose to modify the eddy viscosity used by the wall model in accordance with the implied eddy viscosity of the compressible transformation.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2023
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106996
DOIs
StatePublished - 2023
EventAIAA SciTech Forum and Exposition, 2023 - Orlando, United States
Duration: Jan 23 2023 → Jan 27 2023

Publication series

NameAIAA SciTech Forum and Exposition, 2023

Conference

ConferenceAIAA SciTech Forum and Exposition, 2023
Country/TerritoryUnited States
CityOrlando
Period1/23/23 → 1/27/23

Bibliographical note

Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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