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

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

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 direct...

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Bibliographic Details
Main Authors:	Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar
Format:	Proceeding Paper
Language:	English
Published:	2010
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/1/conference_paper_1.pdf

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