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Flow field measurements above wing of high-lift aircraft configuration at high Reynolds number

Konrath, Robert (2018) Flow field measurements above wing of high-lift aircraft configuration at high Reynolds number. In: Particle Image Velocimetry Partical Image Velocimetry, A Practical Guide, 3 (15.5). Springer International Publishing. pp. 541-546. ISBN 978-3-319-68851-0.

Full text not available from this repository.

Official URL: https://doi.org/10.1007/978-3-319-68852-7

Abstract

Of special interest for the optimization of high-lift systems for starting and landing transport aircraft is the flow field above the wing that is directly impacted by the flow around the nacelle/pylon and the edges of retracted slats. To suppress flow separations, streaks are placed on the nacelle to generate vortices possessing a high amount of kinetic energy at high angles of attack. It is crucial to investigate the complex interaction between the streak vortices and the boundary layer of the wing at the correct Reynolds number. Therefore, flow field measurements has been conduced on a half-wing model of a real aircraft in the European Transonic Wind tunnel (ETW). To take account for the specific conditions existing inside this cryogenic wind tunnel facility a especially developed cryo-PIV system has been applied.

Item URL in elib:https://elib.dlr.de/122433/
Document Type:Book Section
Additional Information:eBook: ISBN978-3-319-68852-7, Seitenzahl: XXVI, 669
Title:Flow field measurements above wing of high-lift aircraft configuration at high Reynolds number
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Konrath, Robertrobert.konrath (at) dlr.deUNSPECIFIED
Date:2018
Journal or Publication Title:Particle Image Velocimetry
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:3
DOI :10.1007/978-3-319-68852-7
Page Range:pp. 541-546
Editors:
EditorsEmail
Raffel, MarkusDLR
Willert, Christian E.DLR
Scarano, FulvioDelft University of Technology
Kähler, Christian J.Uni BW München
Wereley, Steven T.Purdue University, USA
Kompenhans, JürgenDLR
Publisher:Springer International Publishing
Series Name:Partical Image Velocimetry, A Practical Guide
ISBN:978-3-319-68851-0
Status:Published
Keywords:Cryo PIV, ETW, high-lift wing, high Reynolds number
Institution:Deutsches Zentrum für Luft- und Raumfahrt e.V.
Department:AS-EXV GO
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
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Micknaus, Ilka
Deposited On:21 Nov 2018 12:05
Last Modified:21 Nov 2018 12:05

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