Stability analysis and active control of a nonlinear composite laminated plate with piezoelectric material in subsonic airflow

DOI10.1007/s10665-014-9708-3zbMath1359.74329OpenAlexW2170355885MaRDI QIDQ521210

Feng-Ming Li, Guo Yao

Publication date: 7 April 2017

Published in: Journal of Engineering Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10665-014-9708-3

zbMATH Keywords

stability analysisactive controlpiezoelectric materialinstability flow velocitynonlinear composite laminated platesubsonic airflow

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Structured surfaces and interfaces, coexistent phases (74A50) Electromagnetic effects in solid mechanics (74F15) Random materials and composite materials (74A40)

Related Items (4)

Nonlinear global resonance analysis of an embedded plate interacting with outside subsonic airflow ⋮ Stability analysis and vibration characteristics of an axially moving plate in aero-thermal environment ⋮ Nonlocal dynamic response of embedded single-layered graphene sheet via analytical approach ⋮ Aeroelastic stability analysis of a pyrotechnic separation plate in subsonic airflow

Cites Work

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• On the aeroelastic stability and bifurcation structure of subsonic nonlinear thin panels subjected to external excitation
• Dynamical analysis of axially moving plate by finite difference method
• Nonlinear dynamics analysis of a two-dimensional thin panel with an external forcing in incompressible subsonic flow
• The acceleration potential in fluid-body interaction problems
• Vibration analysis of rectangular plates coupled with fluid
• Limit cycle oscillations of two-dimensional panels in low subsonic flow
• On the instability of an axially moving elastic plate
• Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material
• Flutter of a viscoelastic strip
• Unified aeroelastic flutter theory for very low aspect ratio panels

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