Separation control applied to the turbulent flow around a NACA4412 wing section
Yuning Wang, Fermin Mallor, Carlos Guardiola, Raffaello Mariani,, Ricardo Vinuesa

TL;DR
This study uses high-resolution LES to evaluate the effectiveness of steady and periodic separation control methods on a NACA4412 wing, revealing that steady blowing/suction delays separation but has limited efficiency gains, while periodic control shows no significant benefits.
Contribution
First high-resolution LES study to comprehensively assess separation control strategies on a NACA4412 wing, analyzing flow physics and aerodynamic performance impacts.
Findings
Steady blowing/suction delays flow separation and increases lift by up to 11%.
Periodic control does not improve separation delay or aerodynamic efficiency.
Significant changes in turbulence statistics and spectral characteristics were observed.
Abstract
We carried out high-resolution large-eddy simulations (LESs) to investigate the effects of several separation-control approaches on a NACA4412 wing section with spanwise width of at an angle of attack of at a Reynolds number of based on chord length and free-stream velocity . Two control strategies were considered: (1) steady uniform blowing and/or suction on the suction and/or pressure sides, and (2) periodic control on the suction side. A wide range of control configurations were evaluated in terms of aerodynamic efficiency (i.e., lift-to-drag ratio) and separation delay. Uniform blowing and/or suction effectively delayed flow separation, leading to a lift increase of up to , but yielded only marginal improvements in aerodynamic efficiency. In contrast, periodic control neither enhanced separation delay nor improved…
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Taxonomy
TopicsPlasma and Flow Control in Aerodynamics
