Experimental investigation of the vortical flow around a reverse delta wing using PIV

Altaf, Afaq and Omar, Ashraf Ali E. and Asrar, Waqar (2010) Experimental investigation of the vortical flow around a reverse delta wing using PIV. In: Experimental Fluid Mechanics 2010, 24-26 November 2010, Liberec / Czech Republic.

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Abstract

Particle Image Velocimetry was used in a low speed wind tunnel to investigate the vortex structures of a slender reverse delta wing at various angles of attack and roll. This work investigates the characteristics of the vortices generated downstream in a plane perpendicular to the free stream direction and their dependence on angles of attack and roll angles at chord based Reynolds number.

Item Type:	Conference or Workshop Item (Full Paper)
Additional Information:	4441/2377
Uncontrolled Keywords:	Reverse Delta Wing, Particle Image Velocimetry (PIV), Vortex.
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Prof. Ashraf Omar
Date Deposited:	29 Sep 2011 05:02
Last Modified:	11 Oct 2011 16:25
URI:	http://irep.iium.edu.my/id/eprint/2377

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