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Towards a numerical test rig: High fidelity simulations with TRACE

Morsbach, Christian and Berger, Michael and Bergmann, Michael and Buchmeier, Jonas and Klose, Björn and Möller, Felix (2026) Towards a numerical test rig: High fidelity simulations with TRACE. Virtual Engine Konferenz 2026, 2026-02-03 - 2026-02-04, Augsburg, Deutschland. (Unpublished)

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/222624/
Document Type:Conference or Workshop Item (Speech)
Title:Towards a numerical test rig: High fidelity simulations with TRACE
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Morsbach, ChristianChristian.Morsbach (at) dlr.dehttps://orcid.org/0000-0002-6254-6979UNSPECIFIED
Berger, Michaelmichael.berger (at) dlr.deUNSPECIFIEDUNSPECIFIED
Bergmann, MichaelMichael.Bergmann (at) dlr.dehttps://orcid.org/0000-0003-0553-5584UNSPECIFIED
Buchmeier, Jonasjonas.buchmeier (at) dlr.dehttps://orcid.org/0000-0002-7277-8810UNSPECIFIED
Klose, Björnbjoern.klose (at) dlr.dehttps://orcid.org/0000-0002-8069-7885UNSPECIFIED
Möller, Felixfelix.moeller (at) dlr.dehttps://orcid.org/0000-0002-0192-3873UNSPECIFIED
Date:4 February 2026
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:numerical test rig, large eddy simulation, compressor, turbine, shock-boundary layer interaction, high performance computing
Event Title:Virtual Engine Konferenz 2026
Event Location:Augsburg, Deutschland
Event Type:national Conference
Event Start Date:3 February 2026
Event End Date:4 February 2026
Organizer:DLR Institut für Test und Simulation für Gasturbinen
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Virtual Engine
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Institute of Test and Simulation for Gas Turbines > Virtual Engine and Numerical Methods
Deposited By: Morsbach, Christian
Deposited On:26 Feb 2026 14:48
Last Modified:26 Feb 2026 14:48

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