Evaluation of aircraft wing-tip vortex using PIV
The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. Particle image velocimetry was used in a wind tunnel to measure the tip vortex velocity field and hence investigate the flow structure in a wake of aircraft half-wing model. The purpose...
| Main Authors: | , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2009
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/6529/ http://irep.iium.edu.my/6529/ http://irep.iium.edu.my/6529/1/Evaluation_of_aircraft_wing-tip_vortex_using_PIV.pdf |