Passive control of the onset of vortex shedding in flow past a circular cylinder using Slit

TL;DR

This study explores a passive flow control method using a slit on a circular cylinder to delay vortex shedding, employing numerical simulations, stability analysis, and flow visualization to understand the effects of slit parameters.

Contribution

It introduces a novel passive control technique with a slit geometry and provides a detailed analysis of how slit parameters influence vortex shedding onset.

Findings

Increasing slit width ratio raises the critical Reynolds number.

Slit angle affects the stability and vortex shedding behavior.

A correlation model estimates critical Reynolds number based on slit parameters.

Abstract

The present study investigates the passive flow control phenomena over a two-dimensional circular cylinder using numerical simulations in the laminar regime. The aim is to explore one of the passive control techniques, which involves the introduction of a slit to the geometry of the cylinder. The two parameters, slit width ratio S/D (slit width/diameter) and slit angle (measured with respect to the incoming flow direction), play an essential role in determining the trend of critical Reynolds number (Rec). Most of the analysis invokes flow visualization and saturation amplitude methods to obtain the critical Reynolds number (indicative of the onset of vortex shedding) for different cases. Further, Hopf bifurcation analysis using Stuart-Landau equation and global stability analysis confirm the accuracy and consistency in the predicted solutions. The additional amount of flow through slit increases the pressure downstream of the cylinder, which consequently leads to an increase in Rec of the modified cylinder. The critical Reynolds number increases with S/D of the modified cylinder at 0 deg slit angle (as an additional amount of flow grows with S/D). The critical Reynolds number shows an increasing trend with the slit angle in the range of S/D (0.05-0.15) as the fluctuation intensity reduces with slit angle in this range. For S/D= 0.15-0.25, the extra amount of flow through slit induces the instability in wake which causes a decrease in Rec with slit angle. A correlation is obtained that estimates the critical Reynolds number for a given S/D and slit angle.