Optimizing Flow Control with Ensemble Kalman Method for Mitigating Flow-Induced Vibration

The ensemble Kalman method is introduced for optimizing flow control strategies in order to mitigate the flow-induced vibration of structures. Different types of control strategies such as passive control, open-loop active control, and closed-loop active control are tested, showing the flexibility of the method in flow control optimization. The ensemble Kalman method is first tested to mitigate vortex shedding of flows around a circular cylinder by optimizing the placement of small cylinders downstream. Further, the method is assessed to suppress shock buffeting over the NACA 0012 airfoil by optimizing the movement of a compliant aileron. Our results for all test cases show that the ensemble-based method can effectively find optimal control strategies that significantly reduce the vibrations of aerodynamic force, and can be a useful alternative for flow control optimization, due to its merits in nonintrusiveness and ease of implementation.

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Publication Details

Journal
AIAA Journal
Published
2025-04-11
DOI
https://doi.org/10.2514/1.j064850
Primary Topic
Wind and Air Flow Studies
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
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article

Optimizing Flow Control with Ensemble Kalman Method for Mitigating Flow-Induced Vibration

Shizhao Wang, Guowei He, Yi Liu, Xinlei Zhang
AIAA Journal
Wind and Air Flow Studies
article

Optimizing Flow Control with Ensemble Kalman Method for Mitigating Flow-Induced Vibration

Shizhao Wang, Guowei He, Yi Liu, Xinlei Zhang
article en

Abstract

The ensemble Kalman method is introduced for optimizing flow control strategies in order to mitigate the flow-induced vibration of structures. Different types of control strategies such as passive control, open-loop active control, and closed-loop active control are tested, showing the flexibility of the method in flow control optimization. The ensemble Kalman method is first tested to mitigate vortex shedding of flows around a circular cylinder by optimizing the placement of small cylinders downstream. Further, the method is assessed to suppress shock buffeting over the NACA 0012 airfoil by optimizing the movement of a compliant aileron. Our results for all test cases show that the ensemble-based method can effectively find optimal control strategies that significantly reduce the vibrations of aerodynamic force, and can be a useful alternative for flow control optimization, due to its merits in nonintrusiveness and ease of implementation.

AIAA JournalVol. 63(8)
State Key Laboratory of Nonlinear Mechanics
National Natural Science Foundation of China, China Postdoctoral Science Foundation
Openalex Percentile: Top 93%
Wind and Air Flow Studies
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