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...
| Main Authors: | , , |
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| Format: | Proceeding Paper |
| Language: | English |
| Published: |
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/1/conference_paper_1.pdf |
| _version_ | 1848775998356586496 |
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| author | Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar |
| author_facet | Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar |
| author_sort | Altaf, Afaq |
| building | IIUM Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-14T14:23:06Z |
| format | Proceeding Paper |
| id | iium-2377 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T14:23:06Z |
| publishDate | 2010 |
| recordtype | eprints |
| repository_type | Digital Repository |
| 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 Proceeding Paper 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 |
| spellingShingle | TL500 Aeronautics Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Experimental investigation of the vortical flow around a reverse delta wing using PIV |
| title | 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_short | 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 |
| topic | TL500 Aeronautics |
| url | http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/ http://irep.iium.edu.my/2377/1/conference_paper_1.pdf |