Evaluation of aircraft wing-tip vortex using PIV

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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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Bibliographic Details
Main Authors:	Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali
Format:	Proceeding Paper
Language:	English
Published:	2009
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/6529/ http://irep.iium.edu.my/6529/1/Evaluation_of_aircraft_wing-tip_vortex_using_PIV.pdf

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