Low-Reynolds-number wake of three tandem elliptic cylinders

Author:

Duong Viet Dung1ORCID,Nguyen Van Duc1ORCID,Nguyen Van Tien2ORCID,Ngo Ich Long3ORCID

Affiliation:

1. School of Aerospace Engineering, University of Engineering and Technology, Vietnam National University, Ha Noi City, Vietnam

2. Department of Aerospace Engineering, Pusan National University, Busan, Republic of Korea

3. School of Mechanical Engineering, Hanoi University of Science and Technology, No. 01, Dai Co Viet, Hai Ba Trung, Hanoi, Vietnam

Abstract

The flow around three elliptic cylinders with equal spacing and aspect ratio in tandem arrangements was numerically investigated through direct numerical simulation. The spacing ratio ( L/ D, where D and L are the major axis and the center-to-center distance of two adjacent elliptic cylinders, respectively) ranging from 1.5 to 10 and the Reynolds numbers of [Formula: see text] (based on D) are examined. The analysis aims at the effects of L/ D and Re on wake structures, hydrodynamic forces, and Strouhal numbers and correlates them with the underlying flow physics. The flow is highly changeable to Re and L/ D, classifying into five distinct regimes, namely, meandering, overshoot, reattachment, quasi-coshedding, and coshedding. Two vortex shedding frequencies for middle and downstream cylinders are observed in the latter two regimes, indicating the significant wake interference, where three vortex shedding modes are spatially observed including primary, two-layered, and secondary. The transition between two adjacent modes forms two boundaries. At the first boundary, vortices divert from the cylinder centerline and follow two layers, while vortices converge the cylinder centerline at the second boundary. The first boundary location is not stationary at [Formula: see text], while it is stationary at Re = 160. Otherwise, the second boundary location moves upstream with an increase in L/ D, while the range of movement decreases with an increase in Re. The increase in Re advances the disturbance level and urges the transition between vortex shedding modes. The time-mean lift and drag coefficients for three cylinders are highly sensitive with an increase in L/ D.

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

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