Numerical study on wide gap Taylor Couette flow with flow transition
Md Abdur Razzak, Boo Cheong Khoo, Kim Boon Lua

TL;DR
This paper uses direct numerical simulation to analyze flow transitions and disturbance sources in wide gap Taylor Couette flow, revealing how flow separation and viscous layer changes lead to non-axisymmetric disturbances and flow pattern shifts.
Contribution
It provides new insights into the origin and propagation of non-axisymmetric disturbances in wide gap Taylor Couette flow through detailed analysis of viscous layer behavior and flow transition mechanisms.
Findings
Flow transitions from axisymmetric to non-axisymmetric occur between Re 425 and 575.
Sudden increase in viscous layer thickness at the outer wall indicates disturbance sources.
Transition flow shows reduced torque compared to axisymmetric Taylor-vortex flow.
Abstract
This study aims to investigate the possible sources of non-axisymmetric disturbances and their propagation mechanism in Taylor Couette flow (TCF) for wide gap problems using direct numerical simulation with a radius ratio of 0.5 and Reynolds number (Re) ranging from 60 to 650. Here, attention is focused on the viscous layer (VL) thickness in near-wall regions and its spatial distribution along the axial direction to gain an insight into the origin and propagation of non-axisymmetric disturbances. The results show that an axisymmetric Taylor-vortex flow occurs when Re is between 68 and 425. Above Re = 425, transition from axisymmetric to non-axisymmetric flow is observed up to Re = 575 before the emergence of wavy-vortex flow. From the variation of VL thickness with Re, the VL does not experience any significant changes in the flow separation region of the inner wall, as well as jet…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Aeolian processes and effects · Particle Dynamics in Fluid Flows
