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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
American Society of Civil Engineers (ASCE)
2012
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Subjects: | |
Online Access: | http://irep.iium.edu.my/2105/ http://irep.iium.edu.my/2105/ http://irep.iium.edu.my/2105/ http://irep.iium.edu.my/2105/1/Evolution_of_NACA23012_Wake_Vortices_Structure_Using_PIV.pdf |