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Rosenbrock-Wanner Methods for Scale-Resolving Simulations

Schmid, Anton (2023) Rosenbrock-Wanner Methods for Scale-Resolving Simulations. Bachelor's, Georg-August-Universität Göttingen.

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Abstract

Scale-resolving simulations in computational fluid dynamics (CFD) have become increasingly relevant in recent years due to ever improving computational capabilities of modern HPC clusters. Such simulations lead to a complex interplay of physical modeling and the spatial and temporal discretization used to compute a numerical solution to the model. In this thesis focus on implicit temporal discretizations, more specifically Rosenbrock-Wanner (ROW) methods and diagonally implicit RungeKutta (DIRK) methods. ROW methods have been added recently to the next generation CFD code jointly developed by ONERA, DLR and Airbus (henceforth referred to as CODA). In this thesis, we would like to offer a general understanding of the advantages and disadvantages of ROW methods. Furthermore, we would like to compare the ROW methods to DIRK methods in terms of accuracy and performance for scale-resolving simulations. We aim to provide a best practice choice of a time-discretization scheme for this application in CODA.

Item URL in elib:https://elib.dlr.de/197222/
Document Type:Thesis (Bachelor's)
Title:Rosenbrock-Wanner Methods for Scale-Resolving Simulations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Schmid, AntonUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:July 2023
Journal or Publication Title:Uni Göttingen
Refereed publication:No
Open Access:No
Number of Pages:70
Status:Published
Keywords:computational fluid dynamics, implicit time integration, Rosenbrock-Wanner methods, diagonally implicit RungeKutta methods
Institution:Georg-August-Universität Göttingen
Department:Institut für Dynamik komplexer Systeme
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > CASE, GO
Deposited By: Löwe, Johannes
Deposited On:14 Sep 2023 15:38
Last Modified:14 Sep 2023 15:38

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