elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Experimental characterisation of a high Reynolds number turbulent boundary layer subjected to an adverse pressure gradient

Srinath, S. and Cuvier, C. and Foucaut, J. M. and Laval, J. P. and Stanislas, Michel and Kähler, Christian and Hain, Rainer and Scharnowski, Sven and Schröder, Andreas and Geisler, Reinhard and Agocs, Janos and Röse, Anni and Willert, Christian and Klinner, Joachim and Soria, Julio and Amili, Omid and Atkinson, Callum (2017) Experimental characterisation of a high Reynolds number turbulent boundary layer subjected to an adverse pressure gradient. Congrès Français de Mécanique - CFM 2017, 28. Aug. - 01. Sep. 2017, Lille, Frankreich.

[img] PDF (Proceedings paper)
3MB

Official URL: https://cfm2017.sciencesconf.org/130909/document/

Abstract

A turbulent boundary layer over a given geometry was studied experimentally in the framework of a EUHIT project. The geometry consists of a specifically designed ramp model, which is approximately 7m long. The model used is the LML-AVERT ramp on which the final flap was replaced by a 3.5m long flat plate. Several PIV experiments were conducted including one covering the full boundary layer thickness over a length of more than 10 boundary layer thicknesses with a good spatial resolution. The statistics show the development of a second peak characteristic of this type of flow with adverse pressure gradient and probably associated to the enhancement of very large scale motions.

Item URL in elib:https://elib.dlr.de/116917/
Document Type:Conference or Workshop Item (Speech)
Title:Experimental characterisation of a high Reynolds number turbulent boundary layer subjected to an adverse pressure gradient
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Srinath, S.LML UMR CNRS 8107, Villeneuve d'Ascq, FranceUNSPECIFIED
Cuvier, C.LML UMR CNRS 8107, Villeneuve d'Ascq, FranceUNSPECIFIED
Foucaut, J. M.LML UMR CNRS 8107, Villeneuve d'Ascq, FranceUNSPECIFIED
Laval, J. P.LML UMR CNRS 8107, Villeneuve d'Ascq, FranceUNSPECIFIED
Stanislas, MichelLaboratoire de Mécanique de Lille, FranceUNSPECIFIED
Kähler, ChristianUniBw MünchenUNSPECIFIED
Hain, RainerUni BW München, Inst f Strömungsmechanik und AerodynamikUNSPECIFIED
Scharnowski, SvenUni BW MünchenUNSPECIFIED
Schröder, Andreasandreas.schroeder (at) dlr.dehttps://orcid.org/0000-0002-6971-9262
Geisler, Reinhardreinhard.geisler (at) dlr.deUNSPECIFIED
Agocs, Janosjanos.agocs (at) dlr.deUNSPECIFIED
Röse, AnniAS-EXVUNSPECIFIED
Willert, ChristianChris.Willert (at) dlr.dehttps://orcid.org/0000-0002-1668-0181
Klinner, JoachimJoachim.Klinner (at) dlr.dehttps://orcid.org/0000-0003-2709-9664
Soria, JulioMonash UniversityUNSPECIFIED
Amili, OmidMonash UniversityUNSPECIFIED
Atkinson, CallumMonash Universityhttps://orcid.org/0000-0003-3726-2103
Date:2017
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:turbulent boundary layer, adverse pressure gradient, particle image velocimetry, PIV
Event Title:Congrès Français de Mécanique - CFM 2017
Event Location:Lille, Frankreich
Event Type:national Conference
Event Dates:28. Aug. - 01. Sep. 2017
Organizer:Association Française de Mécanique (AFM)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Virtual Engine and Validation methods, L - Simulation and Validation
Location: Göttingen , Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Measurement Systems
Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Willert, Dr.phil. Christian
Deposited On:14 Dec 2017 16:02
Last Modified:31 Jul 2019 20:14

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.