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Active flow control for drag reduction through multi-agent reinforcement learning on a turbulent cylinder at $Re_D=3900$

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arxiv 2405.17655 v3 pith:3VKC3WXI submitted 2024-05-27 physics.flu-dyn

classification physics.flu-dyn
keywords cylinderflowcontroldragreductionturbulentactiveclassical
verification ladder T0 review T1 audit T2 compute T3 formal
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abstract

This study presents novel drag reduction active-flow-control (AFC) strategies} for a three-dimensional cylinder immersed in a flow at a Reynolds number based on freestream velocity and cylinder diameter of $Re_D=3900$. The cylinder in this subcritical flow regime has been extensively studied in the literature and is considered a classic case of turbulent flow arising from a bluff body. The strategies presented are explored through the use of deep reinforcement learning. The cylinder is equipped with 10 independent zero-net-mass-flux jet pairs, distributed on the top and bottom surfaces, which define the AFC setup. The method is based on the coupling between a computational-fluid-dynamics solver and a multi-agent reinforcement-learning (MARL) framework using the proximal-policy-optimization algorithm. This work introduces a multi-stage training approach to expand the exploration space and enhance drag reduction stabilization. By accelerating training through the exploitation of local invariants with MARL, a drag reduction of approximately 9% is achieved. The cooperative closed-loop strategy developed by the agents is sophisticated, as it utilizes a wide bandwidth of mass-flow-rate frequencies, which classical control methods are unable to match. Notably, the mass cost efficiency is demonstrated to be two orders of magnitude lower than that of classical control methods reported in the literature. These developments represent a significant advancement in active flow control in turbulent regimes, critical for industrial applications.

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Reviewed papers in the Pith corpus that reference this work. Sorted by Pith novelty score. Full citation record

  1. Separation control applied to the turbulent flow around a NACA4412 wing section

    physics.flu-dyn 2025-02 conditional novelty 5.0 of 10

    Uniform suction and blowing eliminate separation on a NACA4412 wing at 11 degrees angle of attack and increase lift up to 11.5 percent, but drag increases enough to reduce aerodynamic efficiency.

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