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Phase-based analysis and control of low Reynolds number aeroelastic flows

2025/05/30 by Chathura Ranganath Sumanasiri, Sumanasiri, Chathura R., Tulsi Ram Sahu +3
Engineering · #Computational Fluid Dynamics and Aerodynamics #FOS: Physical sciences #Fluid Dynamics (physics.flu-dyn) #Fluid Dynamics and Turbulent Flows #Plasma and Flow Control in Aerodynamics

paper · pdf · doi:10.48550/arxiv.2506.00306

openalex publication_date 2025/05/30 · openalex created_date 2025/10/10 · openalex updated_date 2026/07/30

Abstract

Flutter in lightweight airfoils under unsteady flows presents a critical challenge in aeroelastic stability and control. This study uncovers phase-localized mechanisms that drive the onset and suppression of flutter in a freely pitching airfoil at low Reynolds number. By introducing targeted impulsive stiffness perturbations, we identify critical phases that trigger instability. Using phase-sensitivity functions, energy-transfer metrics, and dynamic mode decomposition, we show that flutter arises from phase lock-on between structural and fluid modes. Leveraging this insight, we design an energy-optimal, phase-based control strategy that applies transient heaving motions to disrupt synchronization and arrest unstable growth. This minimal, time-localized control suppresses subharmonic amplification and restores stable periodic motion.

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