Evolution of NACA23012 wake vortices structure using PIV

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Evolution of NACA23012 wake vortices structure using PIV

The formation and development of a wing‐tip vortex in a near and extended near field were studied experimentally. A swept‐back tapered wing with a NACA23012 cross‐section was used as a vortex generator. Particle image velocimetry as a whole field velocity measurement technique was used in a low‐spee...

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Bibliographic Details
Main Authors:	Elsayed, Omer Ali, Asrar, Waqar, Omar, Ashraf Ali, Kwon, Kijung
Format:	Article
Language:	English
Published:	American Society of Civil Engineers (ASCE) 2012
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/2105/ http://irep.iium.edu.my/2105/1/Evolution_of_NACA23012_Wake_Vortices_Structure_Using_PIV.pdf

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