The effect of magnetorheological fluid and aerodynamic damping on the flutter boundaries of MR fluid sandwich plates in supersonic airflow

DOI10.1016/J.EUROMECHSOL.2020.103997zbMath1477.74050OpenAlexW3013584061MaRDI QIDQ2190110

Mehdi Eshaghi

Publication date: 18 June 2020

Published in: European Journal of Mechanics. A. Solids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.euromechsol.2020.103997

zbMATH Keywords

magnetorheological fluidflutter suppressionHamilton principlecantilevered plateaeroelastic stabilitylinear first-order piston theory

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Composite and mixture properties (74E30) Stability of dynamical problems in solid mechanics (74H55) Magnetohydrodynamics and electrohydrodynamics (76W05) Supersonic flows (76J20)

Related Items (1)

Meshless analysis for modal properties and stochastic responses of heated laminated rectangular/sectorial plates in supersonic airflow

Cites Work

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• Optimal locations of magnetorheological fluid pockets embedded in an elastically supported honeycomb sandwich beams for supersonic flutter suppression
• Size-dependent vibration analysis of an axially moving sandwich beam with MR core and axially FGM faces layers in yawed supersonic airflow
• A Simple Higher-Order Theory for Laminated Composite Plates
• Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
• The free vibration of rectangular plates

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