Opposition control applied to turbulent wings
Yuning Wang, Marco Atzori, Ricardo Vinuesa

TL;DR
This study uses high-resolution simulations to evaluate opposition control's effectiveness on turbulent boundary layers over wings with different pressure gradients, revealing limitations under strong adverse pressure gradients and exploring alternative control methods.
Contribution
First detailed analysis of opposition control applied to turbulent boundary layers over wings with nonuniform adverse pressure gradients.
Findings
OC effectiveness decreases with stronger APGs.
Wall-normal convection intensifies under strong APGs.
Spectral analysis shows impact on small-scale structures transport.
Abstract
We conducted high-resolution large-eddy simulations (LESs) to explore the effects of opposition control (OC) on turbulent boundary layers (TBLs) over a wing at a chord-based Reynolds number () of 200,000. Two scenarios were studied: flow over the suction sides of the NACA0012 wing section at a angle of attack, and the NACA4412 wing section at a angle of attack, representing TBLs under mild and strong nonuniform adverse pressure gradients (APGs), respectively. Our results show that the effectiveness of OC in reducing friction drag decreases significantly with increasing APG intensity. This reduction is linked to intensified wall-normal convection caused by the stronger APG. OC, designed to reduce near-wall fluctuations, attenuates the outer peak of streamwise velocity fluctuations and the production term of the turbulent kinetic energy budget. We also…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Plasma and Flow Control in Aerodynamics
