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Experimental Study on Controlling Wake Vortex in Water-Towing-Tank

Bao, F. and Vollmers, H. and Mattner, H. (2003) Experimental Study on Controlling Wake Vortex in Water-Towing-Tank. In: ICIASF 2003 Record, Session 8.3, pp. 214-223. IEEE. ICIASF 2003, Göttingen, Germany, August 25 -29, 2003. ISBN 0-7803-8149-1.

Full text not available from this repository.

Abstract

An experimental study was carried out to establish a self-destructing vortex wake. Sets of horizontal tail plains were employed to generate an additional vortex sheet interacting with the wing vortex sheet of a rectangular wing. The study has been performed in the water towing tank in Göttingen (WSG) and exhibited that the interaction of tail vortices with tip vortices may result in a promising self-destructive mechanism within the wake system in the sense that the vortex core experiences an instability and decay abruptly. The possible influence from the finite movement in the water tank due to transient processes of the model was investigated.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003, monograph_id=IEEE Catalog Number: 03CH37501,
Title:Experimental Study on Controlling Wake Vortex in Water-Towing-Tank
Authors:
AuthorsInstitution or Email of Authors
Bao, F.UNSPECIFIED
Vollmers, H.UNSPECIFIED
Mattner, H.UNSPECIFIED
Date:2003
Journal or Publication Title:ICIASF 2003 Record
Volume:Session 8.3
Page Range:pp. 214-223
Publisher:IEEE
Series Name:20th International Congress on Instrumentation in Aerospace Simulation Facilities
ISBN:0-7803-8149-1
Status:Published
Keywords:PIV, measurement technique, end-effect, wake vortex
Event Title:ICIASF 2003, Göttingen, Germany, August 25 -29, 2003
Organizer:IEEE, DLR
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: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Ilka Micknaus
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:14

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