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Publishing Language: Chinese | Open Access

Deep reinforcement learning based intelligent flow control of vortex-induced vibration for box girder

Xiaolong DENG1, Gang HU1( ), Wenli CHEN2
School of Intelligent Civil and Ocean Engineering, Harbin Institute of Technology(Shenzhen), Shenzhen 518055, China
School of Civil Engineering, Harbin Institute of Technology, Harbin 150096, China
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Abstract

An intelligent active flow control method based on deep reinforcement learning (DRL) was proposed to suppress vortex-induced vibrations and enhance the wind resistance of bridges. This method employed synthetic jets to disturb the wake vortex shedding of an aeroelastic bridge section model, effectively suppressing vortex-induced vibrations. Wind tunnel tests were conducted to validate the aerodynamic performance of the model under uniform and steady wind conditions. Additionally, the relationship between the control voltage and synthetic jet flow rate was established. A systematic analysis showed that the control voltage was approximately linearly and positively correlated with the average jet velocity, with higher control voltages significantly improving the suppression effect. Subsequently, the synthetic jet control strategy was optimized using the Soft Actor-Critic (SAC) algorithm, which converged rapidly to the optimal control voltage, resulting in a maximum reduction of 83% in vibration amplitude. These findings demonstrate that combining synthetic jet technology with DRL algorithms provides an efficient and intelligent solution for suppressing bridge vortex-induced vibrations and offers an intelligent approach for wind-resistant bridge design.

CLC number: V214.3;TP181;TU311.3 Document code: A

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Acta Aerodynamica Sinica
Pages 92-100

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Cite this article:
DENG X, HU G, CHEN W. Deep reinforcement learning based intelligent flow control of vortex-induced vibration for box girder. Acta Aerodynamica Sinica, 2025, 43(5): 92-100. https://doi.org/10.7638/kqdlxxb-2025.0016

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Received: 24 January 2025
Revised: 08 April 2025
Published: 28 May 2025
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).