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 vortex...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Isfahan University of Technology
2020-01-01
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| Series: | Journal of Applied Fluid Mechanics |
| Subjects: | |
| Online Access: | http://jafmonline.net/JournalArchive/download?file_ID=51290&issue_ID=1005 |