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...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Journal of Applied Fluid Mechanics
2020
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/76419/ http://irep.iium.edu.my/76419/ http://irep.iium.edu.my/76419/ http://irep.iium.edu.my/76419/3/29738_090219035335.pdf |