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Application of PIV in fundamental fluid mechanics: boundary layers, delta wing cross flow and wake vortices

Kompenhans, J. and Raffel, M. and Dieterle, L. and Dewhirst, T. and Vollmers, H. (1998) Application of PIV in fundamental fluid mechanics: boundary layers, delta wing cross flow and wake vortices. Institute of Industrial Science, Tokyo/Japan, 14. Dezember 1998.

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Abstract

Particle image velocimetry (PIV) is increasingly used for aerodynamic research and development. The PIV technique allows the recording of a complete flow velocity field in a plane of the flow within a few microseconds. Thus, it provides information about unsteady flow fields, which is difficult to obtain with other experimental techniques, especially at the investigation of boundary layers, wake vortices, rotor flow fields and propeller slipstream. The development and application of a stereoscopic PIV system was described

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Application of PIV in fundamental fluid mechanics: boundary layers, delta wing cross flow and wake vortices
Authors:
AuthorsInstitution or Email of Authors
Kompenhans, J.UNSPECIFIED
Raffel, M.UNSPECIFIED
Dieterle, L.UNSPECIFIED
Dewhirst, T.UNSPECIFIED
Vollmers, H.UNSPECIFIED
Date:1998
Status:Published
Keywords:particle image velocimetry, PIV, industrial wind tunnels, aerodynamics, boundary layers, stereoscopic PIV, propeller, rotor, unsteady flow fields, wake vortices
Event Title:Institute of Industrial Science, Tokyo/Japan, 14. Dezember 1998
Organizer:University of Tokyo
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:35

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