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Wake structure of plunging finite wings
D.E. Calderon, D J Cleaver,
Z Wang
,
I Gursul
Department of Mechanical Engineering
Research output
:
Contribution to conference
›
Paper
4
Citations (SciVal)
Overview
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Dive into the research topics of 'Wake structure of plunging finite wings'. Together they form a unique fingerprint.
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Engineering
Vortex
100%
Aspect Ratio
100%
Trailing Edge
66%
Illustrates
33%
Angle-of-Attack
33%
Airfoil
33%
Edge Vortex
33%
Particle Image Velocimetry
33%
Two Dimensional
33%
Vortex Shedding
33%
Endplate
33%
Physics
Aspect Ratio
100%
Vortex Shedding
33%
Particle Image Velocimetry
33%
Airfoil
33%
Angle of Attack
33%
Velocity Measurement
33%