Study on Traveling Wave Wall Control Method for Suppressing Wake of Flow around a Circular Cylinder at Moderate Reynolds Number

In the present paper, the computational fluid dynamics (CFD) numerical simulation was utilized to investigate the effectiveness of the transverse traveling wave wall (TWW) method with the expectation of inhibiting the vortex shedding from a fixed circular cylinder. We mainly focused on the variation...

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Bibliographic Details
Main Authors: Bai, W. (Author), Liu, X. (Author), Xu, F. (Author)
Format: Article
Language:English
Published: MDPI 2022
Subjects:
CFD
Online Access:View Fulltext in Publisher
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008 220421s2022 CNT 000 0 und d
020 |a 20763417 (ISSN) 
245 1 0 |a Study on Traveling Wave Wall Control Method for Suppressing Wake of Flow around a Circular Cylinder at Moderate Reynolds Number 
260 0 |b MDPI  |c 2022 
856 |z View Fulltext in Publisher  |u https://doi.org/10.3390/app12073433 
520 3 |a In the present paper, the computational fluid dynamics (CFD) numerical simulation was utilized to investigate the effectiveness of the transverse traveling wave wall (TWW) method with the expectation of inhibiting the vortex shedding from a fixed circular cylinder. We mainly focused on the variations of four kinds of wave propagation directions, five different maximum wave amplitudes and ten different wave velocities for suppressing vortices shedding and aerodynamic forces. The aerodynamic coefficients and vortex structures under different propagation directions, wave amplitudes, wave numbers and wave velocities were investigated in detail. The results demonstrate that the alternate wake behind the cylinder can be effectively eliminated resorting to the “Downstream” propagating TWW. The mean drag coefficient is positively associated with wave velocity. Drag and lift coefficients remain relatively stable at different wave amplitudes. When the velocity ratio (wave velocity divided by incoming velocity) is 1.5, the lift coefficient fluctuation decreases to the minimum. In contrast, the optimal combination of control parameters under the present Reynolds number is concluded with “Downstream” propagating direction, maximum wave amplitude ratio of 0.02, and velocity ratio of 1.5. © 2022 by the authors. Licensee MDPI, Basel, Switzerland. 
650 0 4 |a CFD 
650 0 4 |a circular cylinder 
650 0 4 |a flow control 
650 0 4 |a numerical simulation 
650 0 4 |a traveling wave wall 
700 1 0 |a Bai, W.  |e author 
700 1 0 |a Liu, X.  |e author 
700 1 0 |a Xu, F.  |e author 
773 |t Applied Sciences (Switzerland)