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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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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/2377/1/conference_paper_1.pdf
http://irep.iium.edu.my/2377/
http://orion.kez.tul.cz/efm/old/2010/index.php?x=i
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spelling my.iium.irep.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 REM 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
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
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/2377/1/conference_paper_1.pdf
http://irep.iium.edu.my/2377/
http://orion.kez.tul.cz/efm/old/2010/index.php?x=i
_version_ 1643604958346477568
score 13.159267

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