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Direct numerical simulation of 45° oblique flow past surface-mounted square cylinder

Published online by Cambridge University Press:  27 August 2024

Dung Viet Duong*
Affiliation:
School of Aerospace Engineering, University of Engineering and Technology, Vietnam National University, 123105 Ha Noi City, Vietnam
Luc Van Nguyen
Affiliation:
Faculty of Aeronautical Engineering, Vietnam Aviation Academy, 726500 Hochiminh City, Vietnam
Duc Van Nguyen
Affiliation:
School of Aerospace Engineering, University of Engineering and Technology, Vietnam National University, 123105 Ha Noi City, Vietnam School of Mechanical, Aerospace, and Manufacturing Engineering, University of Connecticut, Storrs, CT 06269, USA
Truong Cong Dinh
Affiliation:
School of Mechanical Engineering, Hanoi University of Science and Technology, No. 01, Dai Co Viet, Hai Ba Trung, 112400 Hanoi, Vietnam
Lavi Rizki Zuhal
Affiliation:
Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung, 40116 Bandung, Indonesia
Long Ich Ngo*
Affiliation:
School of Mechanical Engineering, Hanoi University of Science and Technology, No. 01, Dai Co Viet, Hai Ba Trung, 112400 Hanoi, Vietnam
*
Email addresses for correspondence: duongdv@vnu.edu.vn, long.ngoich@hust.edu.vn
Email addresses for correspondence: duongdv@vnu.edu.vn, long.ngoich@hust.edu.vn

Abstract

Comprehensive coherent structures around a surface-mounted low aspect ratio square cylinder in uniform flow with an oblique angle of $45^{\circ }$ were investigated for cylinder-width-based Reynolds numbers of 3000 and 10 000 by direct numerical simulation based on a topology-confined mesh refinement framework. High-resolution simulations and the critical-point concept were scrutinized to reveal for the first time the reasonable and compatible topologies of flow separation and complete near-wall structures, due to their extensive impact on various engineering applications. Large-scale horseshoe vortices are observed at two notable foci in the viscous sublayer. Within this layer, a wall-parallel jet is formed by downflow intruding into the bottom surface at the half-saddle point, then deflecting in the upstream direction and finally penetrating the bottom surface until the half-saddle point. A pair of conical vortices on the cylinder's top surface switch themselves on two sides of the square cylinder, where the switching frequency is identical with that of the sway of the side shear layer. The undulation of the Kelvin–Helmholtz instability is identified in the instantaneous development of a conical vortex and side shear layer, where the scaling of the ratio of the Kelvin–Helmholtz and von Kármán frequencies follows the power-law relation obtained by Lander et al. (J. Fluid Mech., vol. 849, 2018, pp. 1096–1119). Large-scale arch-shaped vortex is often detected in the intermediate wake region of a square cylinder, involving two interconnected portions, such as the leg portion separated from leeward surfaces and head portion rolled up from the top surface. The leg portion of the arch-shaped vortex was rooted by two foci near the bottom-surface plane.

Type
JFM Papers
Copyright
© The Author(s), 2024. Published by Cambridge University Press

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Supplementary material: File

Duong et al. supplementary movie 1

Evolution of switching conical vortex at Reynolds number of 3000
Download Duong et al. supplementary movie 1(File)
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Supplementary material: File

Duong et al. supplementary movie 2

Evolution of switching conical vortex at Reynolds number of 10000
Download Duong et al. supplementary movie 2(File)
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