Wake Stabilization and Force Modulation via Surface Dimples on an Airfoil at Low-Reynolds-Numbers
Putu Brahmanda Sudarsana, Jagmohan Singh, Anchal Sareen

TL;DR
This paper explores how surface dimples on an airfoil influence unsteady aerodynamics and wake stability at low Reynolds numbers, showing potential for passive flow control to reduce force fluctuations or induce wake stabilization.
Contribution
It demonstrates that surface dimples can passively modulate unsteady forces and wake dynamics, with effects varying depending on Reynolds number, through detailed numerical simulations and flow visualization.
Findings
Dimples reduce force fluctuations at Re_c=5300 by over 25%.
At Re_c=10,000, dimples stabilize wake and increase periodicity.
Flow visualizations show dimples generate vortices that stabilize wake structures.
Abstract
This study investigates the effect of surface dimples on the unsteady aerodynamics of a National Advisory Committee for Aeronautics airfoil (NACA0012) at a chord-based Reynolds numbers of and using direct numerical simulations. Dimples were placed on the suction side at non-dimensional chordwise locations of and , and the flow response was studied at a fixed angle of attack . At , dimples placed at reduced lift and drag fluctuations by and , respectively, with minimal change in mean forces. At , the same configuration led to a seven-fold increase in force fluctuations, while the mean remained unchanged. The smooth airfoil exhibited irregular, aperiodic force signals at this , whereas the dimpled case showed highly periodic behavior, indicating wake…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Plasma and Flow Control in Aerodynamics · Particle Dynamics in Fluid Flows
