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

id	iium-2377
recordtype	eprints
spelling	iium-23772011-10-11T08:25:46Z http://irep.iium.edu.my/2377/ Experimental investigation of the vortical flow around a reverse delta wing using PIV Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar TL500 Aeronautics 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. 2010-11-24 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/2377/1/conference_paper_1.pdf 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. http://orion.kez.tul.cz/efm/old/2010/index.php?x=i
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Experimental investigation of the vortical flow around a reverse delta wing using PIV
description	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.
format	Conference or Workshop Item
author	Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar
author_facet	Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar
author_sort	Altaf, Afaq
title	Experimental investigation of the vortical flow around a reverse delta wing using PIV
title_short	Experimental investigation of the vortical flow around a reverse delta wing using PIV
title_full	Experimental investigation of the vortical flow around a reverse delta wing using PIV
title_fullStr	Experimental investigation of the vortical flow around a reverse delta wing using PIV
title_full_unstemmed	Experimental investigation of the vortical flow around a reverse delta wing using PIV
title_sort	experimental investigation of the vortical flow around a reverse delta wing using piv
publishDate	2010
url	http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/1/conference_paper_1.pdf
first_indexed	2023-09-18T20:09:58Z
last_indexed	2023-09-18T20:09:58Z
_version_	1777407412091748352

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

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