Bursting and reformation cycle of the laminar separation bubble over a NACA-0012 aerofoil: The underlying mechanism
Eltayeb ElJack, Julio Soria

TL;DR
This study uncovers the vortex triad mechanism behind the quasi-periodic bursting and reformation of the laminar separation bubble on a NACA-0012 aerofoil, revealing flow oscillation dynamics and potential control strategies.
Contribution
It identifies the vortex triad and flow oscillation mechanism responsible for LSB bursting and reformation, advancing understanding of flow dynamics over aerofoils.
Findings
Flow oscillates between attached and separated states periodically.
A vortex triad drives the flow oscillation and bubble dynamics.
Flow direction influences transition location and flow attachment.
Abstract
The present investigation shows that a triad of three vortices, two co-rotating vortices (TCV) and a secondary vortex lies beneath them and counter-rotating with them, is behind the quasi-periodic self-sustained bursting and reformation of the laminar separation bubble (LSB) and its associated low-frequency flow oscillation (LFO). The upstream vortex of the TCV (UV) is driven by the gradient of the oscillating-velocity across the laminar portion of the separated shear layer and is faithfully aligned with it. The secondary vortex acts as a roller support that facilitates the rotation and orientation of the TCV. A global oscillation in the flow-field around the aerofoil is observed in all of the investigated angles of attack, including at zero angle of attack. The flow switches between an attached-phase against an adverse pressure gradient (APG) and a separated-phase despite a favourable…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Fluid Dynamics and Vibration Analysis · Aerodynamics and Fluid Dynamics Research
