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Assessment of scale resolving turbulence models in the TAU code for canonical shock-turbulence interaction

Hoste, Jimmy-John (2023) Assessment of scale resolving turbulence models in the TAU code for canonical shock-turbulence interaction. DLR-Forschungsbericht. DLR-FB-2020-28. 169 S. doi: 10.57676/tq7r-en64.

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Official URL: https://doi.org/10.57676/tq7r-en64

Abstract

This report contains the detailed description of the study of the canonical shock-turbulence interaction (STI) problem performed with the DLR’s TAU CFD solver. STI studies reported in the literature are typically performed with high-order (> 2nd) accurate numerical schemes for space- and time discretizations. Instead, TAU, being a code used for both industrial and academic purposes, contains second-order accurate numerics. The motivation of this work is to understand how such a solver copes with the canonical STI setup which requires low dissipation to describe the turbulence accurately while higher dissipation is needed to avoid numerical issues in the shock capturing process. To this end, the scale-resolving capability of TAU has been carefully investigated for several STI’s where turbulence has been described with a Large Eddy Simulations (LES) method.

Item URL in elib:https://elib.dlr.de/193435/
Document Type:Monograph (DLR-Forschungsbericht)
Title:Assessment of scale resolving turbulence models in the TAU code for canonical shock-turbulence interaction
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hoste, Jimmy-JohnDLR AS-RFZUNSPECIFIEDUNSPECIFIED
Date:2 January 2023
Refereed publication:No
Open Access:Yes
DOI:10.57676/tq7r-en64
Number of Pages:169
ISSN:1434-8454
Status:Published
Keywords:shock, turbulence, les
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Karl, Dr. Sebastian
Deposited On:10 Mar 2023 08:21
Last Modified:29 Mar 2023 15:22

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