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Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing

Konrath, Robert and Klein, Christian and Schröder, Andreas and Kompenhans, Jürgen (2006) Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing. Experiments in Fluids, Vol. 44 (3), pp. 357-366. Springer Verlag Berlin/Heidelberg. DOI: 10.1007/s00348-007-0445-5. ISSN 0723-4864 (print), 1432-1114 (online).

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Official URL: http://www.springer.com

Abstract

The pressure sensitive paint (PSP) and particle image velocimetry (PIV) techniques are applied to the flow around a delta wing. These investigations are a contribution to the International Vortex Flow Experiment 2 (VFE-2). The delta wing is equipped with rounded as well as with sharp leading edges. To demonstrate the advantages of a combined application of PSP and PIV for flow investigation the results of a specific case are discussed, where an inner and outer primary vortex above the delta wing with rounded leading edges develop.

Document Type:Article
Title:Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing
Authors:
AuthorsInstitution or Email of Authors
Konrath, RobertUNSPECIFIED
Klein, ChristianUNSPECIFIED
Schröder, AndreasUNSPECIFIED
Kompenhans, JürgenUNSPECIFIED
Date:15 December 2006
Journal or Publication Title:Experiments in Fluids
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:Vol. 44
DOI:10.1007/s00348-007-0445-5
Page Range:pp. 357-366
Editors:
EditorsEmail
Rockwell, D.UNSPECIFIED
Tropea, C.UNSPECIFIED
Publisher:Springer Verlag Berlin/Heidelberg
Series Name:Experimental Methods and their Applications to Fluid Flow
ISSN:0723-4864 (print), 1432-1114 (online)
Status:Published
Keywords:PSP, PIV, Delta-wing, VFE-2
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:24 Apr 2008
Last Modified:15 Jan 2010 00:00

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