Parametric Investigation of Harnessed Power of Two Tandem Cylinders in Flow Induced Vibration
In transverse flow, cylinders respond in FIV (Flow Induced Vibrations); particularly VIV (Vortex Induced Vibrations) and galloping. Typically, in the galloping region, the hydrokinetic power converted to mechanical in the oscillators increases with increasing flow velocity and Reynolds number. Flow...
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Format: | Article |
Language: | English |
Published: |
Bursa Uludag University
2018-04-01
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Series: | Uludağ University Journal of The Faculty of Engineering |
Subjects: | |
Online Access: | https://dergipark.org.tr/tr/pub/uumfd/issue/36268/377444 |
Summary: | In transverse flow, cylinders respond in FIV (Flow
Induced Vibrations); particularly VIV (Vortex Induced Vibrations) and
galloping. Typically, in the galloping region, the hydrokinetic power converted
to mechanical in the oscillators increases with increasing flow velocity and
Reynolds number. Flow Induced Vibrations (FIVs) of two tandem, rigid and
circular cylinder with end-springs are studied for 30,000<Re <120,000 with different damping,
mass ratio and stiffness as parameters in the Low Turbulence Free Surface Water
(LTFSW) Channel of the Marine Renewable Energy Laboratory (MRELab). Typical
local drops and jumps in harnessed power were observed in the velocity range of
0.9<U<1.3 m/s within the galloping region. The main objective of this
paper is to explain the reason for the presence of these drops and jumps. To
achieve this objective, the points of changing in harnessed power in an
extensive set of data with spacing, damping, stiffness, and flow velocity as
parameters are identified. For both up and downstream cylinders, the harnessed
power, amplitude-ratio, frequency-ratio and time history graphs are obtained to
define the reason of these drop/jumps. Visualization with high-resolution
camera has been used and the assumption which may affect the phenomena were
studied and presented. As a conclusion, there is a big interaction between
cylinders. Galloping instability disappears at this drops and harnessed power
decreases sharply and amplitude as well. |
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ISSN: | 2148-4147 2148-4155 |