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27145

SUPPRESSION OF VORTEX INDUCED VIBRATIONS ON CIRCULAR CYLINDER VIA BOUNDARY LAYER SUCTION

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Last updated: 04 Jan 2025

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Abstract

Marine risers used to convey oil from the sea bed to the sea level, marine cables, heat exchanger pipes, civil engineering structures and aircraft wings vibrate due to the formation of the vortex streets behind these structures. The interactions between the flow oscillations and the structure give rise to complicated vibrations of the structure which could cause structural damage due to the fatigue. Numerical simulation of the vortex-induced vibrations on circular cylinders is used to investigate the possibility of suppressing these vibrations for different engineering applications. The unsteady, incompressible, two-dimensional Navier-Stokes equations are solved numerically on a structured grid using the finite difference method. The effect of flow control using the boundary layer suction for fixed or moving cylinder is investigated by applying the appropriate boundary conditions on the cylinder surface. In the current study, natural motion of the cylinder is not considered. Flow oscillations are investigated only for fixed cylinder and for forced motion of the cylinder. The results indicate that the flow oscillations are completely damped for a fixed cylinder using suction on the cylinder surface. For forced motion of the cylinder, the vortex shedding from the surface is eliminated using the boundary layer suction. The flow oscillates only due to the forced motion of the body vibrations which means that the flow oscillations can be damped completely if the cylinder is left to oscillate naturally.

DOI

10.21608/asat.2011.27145

Keywords

Fluid structure interaction, Flow control, vortex shedding, upwind schemes, incompressible flow and numerical simulation

Authors

First Name

FAROUK

Last Name

OWIS

MiddleName

M.

Affiliation

Assistant Professor, Cairo University, Aerospace Engineering Department.

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Volume

11

Article Issue

ASAT Conference, 17-19 May 2005

Related Issue

4906

Issue Date

2011-05-01

Receive Date

2019-02-14

Publish Date

2011-05-01

Page Start

165

Page End

178

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_27145.html

Detail API

https://asat.journals.ekb.eg/service?article_code=27145

Order

10

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

SUPPRESSION OF VORTEX INDUCED VIBRATIONS ON CIRCULAR CYLINDER VIA BOUNDARY LAYER SUCTION

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Article

Created At

22 Jan 2023