Vortex shedding from two finite circular cylinders in a staggered configuration

Journal of Fluids and Structures

Volumn 25, Issue 3, 2009, Pages 479-505

  Li, H ^a   Sumner, D ^a  

^a UNIVERSITY OF SASKATCHEWAN   (Canada)

Author keywords

Bluff body aerodynamics; Finite circular cylinder; Multiple cylinders; Staggered cylinders; Vortex shedding; Wake interference

Indexed keywords

BLUFF-BODY AERODYNAMICS; BOUNDARY LAYER THICKNESS; CYLINDER DIAMETERS; DOWNSTREAM CYLINDERS; FINITE CIRCULAR CYLINDER; FINITE CYLINDERS; FLAT PLATES; FREE ENDS; GROUND PLANES; HOT-WIRE ANEMOMETRIES; INCIDENCE ANGLES; MULTIPLE CYLINDERS; PARTIALLY IMMERSED; PITCH RATIOS; POWER-SPECTRA; STAGGERED CONFIGURATIONS; STAGGERED CYLINDERS; TURBULENT BOUNDARY LAYERS; TWO CIRCULAR CYLINDERS; VORTEX SHEDDING FREQUENCIES; WALL JUNCTIONS; WIND TUNNEL EXPERIMENTS;

AERODYNAMICS; ASPECT RATIO; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLOW PATTERNS; REYNOLDS NUMBER; STROUHAL NUMBER; TURBULENCE; VORTEX FLOW; VORTEX SHEDDING; WAKES;

CIRCULAR CYLINDERS;

EID: 64949116614     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2008.11.001     Document Type: Article

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