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: | Conference or Workshop Item |
| Language: | English |
| Published: |
2010
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| Subjects: | |
| 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 |
| Summary: | 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. |
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