Effect of a directionally porous wing tip on tip vortex

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Effect of a directionally porous wing tip on tip vortex

This paper presents an experimental study of the effect of a directionally porous wing tip on the tip vortex using particle image velocimetry (PIV) on a half wing model with NACA 653218 as its airfoil section. Four different configurations of the directionally porous wing tip are tested. The vorte...

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Bibliographic Details
Main Authors:	Mohammed Aldheeb, Mohammed Abdulmalek, Asrar, Waqar, Omar, Ashraf Ali, Altaf, Afaq, Sulaeman, Erwin
Format:	Article
Language:	English English English
Published:	Journal of Applied Fluid Mechanics 2020
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/76419/ http://irep.iium.edu.my/76419/1/76419_Effect%20of%20a%20directionally%20porous.pdf http://irep.iium.edu.my/76419/2/76419_Effect%20of%20a%20directionally%20porous_SCOPUS.pdf http://irep.iium.edu.my/76419/3/76419_Effect%20of%20a%20directionally%20porous_WOS.pdf

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