Evaluation of aircraft wing-tip vortex using PIV
The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. Particle image velocimetry was used in a wind tunnel to measure the tip vortex velocity field and hence investigate the flow structure in a wake of aircraft half-wing model. The purpose...
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| Main Authors: | , , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2009
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/6529/1/Evaluation_of_aircraft_wing-tip_vortex_using_PIV.pdf http://irep.iium.edu.my/6529/ http://seminar.spaceutm.edu.my/aicfm2009/index.aspx |
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| Institution: | Universiti Islam Antarabangsa Malaysia |
| Language: | English |
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