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Three-dimensional direct numerical simulation of wake transitions of a circular cylinder
148
Citations
22
References
2016
Year
AeroacousticsEngineeringFluid MechanicsMechanical EngineeringComputational MechanicsUnsteady FlowDislocation CycleNumerical SimulationVortex DynamicWake TransitionsHydrodynamic StabilityFlow PhysicMultiphysics ProblemMultiphase FlowTransition ProcessMechanical SystemsCircular CylinderAerodynamicsVortex Induced VibrationMultiscale Modeling
This paper presents three-dimensional (3D) direct numerical simulations (DNS) of flow past a circular cylinder over a range of Reynolds number ( $Re$ ) up to 300. The gradual wake transition process from mode A* (i.e. mode A with large-scale vortex dislocations) to mode B is well captured over a range of $Re$ from 230 to 260. The mode swapping process is investigated in detail with the aid of numerical flow visualization. It is found that the mode B structures in the transition process are developed based on the streamwise vortices of mode A or A* which destabilize the braid shear layer region. For each case within the transition range, the transient mode swapping process consists of dislocation and non-dislocation cycles. With the increase of $Re$ , it becomes more difficult to trigger dislocations from the pure mode A structure and form a dislocation cycle, and each dislocation stage becomes shorter in duration, resulting in a continuous decrease in the probability of occurrence of mode A* and a continuous increase in the probability of occurrence of mode B. The occurrence of mode A* results in a relatively strong flow three-dimensionality. A critical condition is confirmed at approximately $Re=265{-}270$ , where the weakest flow three-dimensionality is observed, marking a transition from the disappearance of mode A* to the emergence of increasingly disordered mode B structures.
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