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A new Experiment of a turbulent boundary layer flow at adverse pressure gradient for validation and improvement of RANS turbulence models

Knopp, Tobias and Schanz, Daniel and Novara, Matteo and Schröder, Andreas and Schülein, Erich and Reuther, Nico and Kähler, Christian (2016) A new Experiment of a turbulent boundary layer flow at adverse pressure gradient for validation and improvement of RANS turbulence models. STAB Symposium 2016 in Braunschweig, 2016-11-08 - 2016-11-09, Braunschweig, Deutschland.

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Item URL in elib:https://elib.dlr.de/110330/
Document Type:Conference or Workshop Item (Speech)
Title:A new Experiment of a turbulent boundary layer flow at adverse pressure gradient for validation and improvement of RANS turbulence models
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Knopp, TobiasUNSPECIFIEDhttps://orcid.org/0000-0002-3161-5353UNSPECIFIED
Schanz, DanielUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Novara, MatteoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schröder, AndreasUNSPECIFIEDhttps://orcid.org/0000-0002-6971-9262UNSPECIFIED
Schülein, ErichUNSPECIFIEDhttps://orcid.org/0000-0002-1125-8504UNSPECIFIED
Reuther, NicoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kähler, Christianunibw münchenUNSPECIFIEDUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Turbulent boundary layer, log-law, RANS, RSM
Event Title:STAB Symposium 2016 in Braunschweig
Event Location:Braunschweig, Deutschland
Event Type:national Conference
Event Start Date:8 November 2016
Event End Date:9 November 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Institute of Aerodynamics and Flow Technology > Experimental Methods
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Bachmann, Barbara
Deposited On:10 Jan 2017 16:11
Last Modified:24 Apr 2024 20:15

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