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Analysis of 3D separated flows in generic diffuser and multi-stage compressor configurations using differential Reynolds stress models

Morsbach, Christian and Matha, Marcel and Kügeler, Edmund (2021) Analysis of 3D separated flows in generic diffuser and multi-stage compressor configurations using differential Reynolds stress models. Workshop DFG PAK 948: Near-Wall Flow in Turbomachinery Blade Rows, 28.01.2021, Virtuell.

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Item URL in elib:https://elib.dlr.de/141600/
Document Type:Conference or Workshop Item (Speech)
Title:Analysis of 3D separated flows in generic diffuser and multi-stage compressor configurations using differential Reynolds stress models
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Morsbach, ChristianChristian.Morsbach (at) dlr.dehttps://orcid.org/0000-0002-6254-6979
Matha, Marcelmarcel.matha (at) dlr.deUNSPECIFIED
Kügeler, EdmundEdmund.Kuegeler (at) dlr.dehttps://orcid.org/0000-0002-9719-626X
Date:28 January 2021
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:turbulence modeling, reynolds stress model, diffuser, compressor, flow separation
Event Title:Workshop DFG PAK 948: Near-Wall Flow in Turbomachinery Blade Rows
Event Location:Virtuell
Event Type:Workshop
Event Dates:28.01.2021
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
Deposited By: Morsbach, Christian
Deposited On:13 Jan 2022 10:35
Last Modified:13 Jan 2022 10:35

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