Flow around two square cylinders near a wall

A numerical study is conducted on flow over two staggered cylinders near a plane wall. The downstream cylinder (DC) is square, of height D, positioned near a plane wall with a gap height of 0.5D. The upstream cylinder (UC) is also square, with height d = 0.5D and 1.0D. For both d values, the UC gap height L is varied from L* (=L/D) = 0.1 to 3.0, and the streamwise spacing S between the UC and DC is varied as S* (=S/D) = 0.5–7.0. We focus on the effect of L*, S*, and d/D on the flow physics and aerodynamic forces on the DC. Six distinct flow patterns (namely, I, II, III, IV, V, and VI) are identified. The positive shear layer of the UC has profound effects on the dynamics of the DC flow. The Strouhal number and forces are strongly correlated with upstream vortices, particularly at lower spacing ratios in patterns II and V. For unsteady flow conditions, both cylinders exhibit identical vortex shedding frequencies for all flow patterns, except in pattern V when d/D = 1.0. The optimal UC position (L*, S*) is identified for minimum mean drag and fluctuating lift coefficients.

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Publication Details

Journal
Physics of Fluids
Published
2025-03-01
DOI
https://doi.org/10.1063/5.0256028
Citations
4
Primary Topic
Fluid Dynamics and Vibration Analysis
Type
article
Field-Weighted Citation Impact
5.34

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article

Flow around two square cylinders near a wall

Dilip K. Maiti, Md. Mahbub Alam, Qiang Zhou, Rajesh Bhatt
4 citations
Physics of Fluids
Fluid Dynamics and Vibration Analysis
5.34
article

Flow around two square cylinders near a wall

Dilip K. Maiti, Md. Mahbub Alam, Qiang Zhou, Rajesh Bhatt
article en
4 citations

Abstract

A numerical study is conducted on flow over two staggered cylinders near a plane wall. The downstream cylinder (DC) is square, of height D, positioned near a plane wall with a gap height of 0.5D. The upstream cylinder (UC) is also square, with height d = 0.5D and 1.0D. For both d values, the UC gap height L is varied from L* (=L/D) = 0.1 to 3.0, and the streamwise spacing S between the UC and DC is varied as S* (=S/D) = 0.5–7.0. We focus on the effect of L*, S*, and d/D on the flow physics and aerodynamic forces on the DC. Six distinct flow patterns (namely, I, II, III, IV, V, and VI) are identified. The positive shear layer of the UC has profound effects on the dynamics of the DC flow. The Strouhal number and forces are strongly correlated with upstream vortices, particularly at lower spacing ratios in patterns II and V. For unsteady flow conditions, both cylinders exhibit identical vortex shedding frequencies for all flow patterns, except in pattern V when d/D = 1.0. The optimal UC position (L*, S*) is identified for minimum mean drag and fluctuating lift coefficients.

Physics of FluidsVol. 37(3)
Harbin Institute of Technology (CN), Vidyasagar University (IN), Southwest Jiaotong University (CN), Vellore Institute of Technology University (IN)
National Fund for Fostering Talents of Basic Science
Openalex Percentile: Top 5%
Fluid Dynamics and Vibration Analysis
5.34
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