Active Flutter Control of a Supersonic Honeycomb Sandwich Beam Resting on Elastic Foundation with Piezoelectric Sensor/Actuator Pair

DOI10.1142/S0219455414500527zbMath1359.74233MaRDI QIDQ2972377

Mohammad Nezami, Behnam Gholami

Publication date: 7 April 2017

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

zbMATH Keywords

honeycomb structuresmart materialslinear-quadratic regulator (LQR)active flutter control (AFC)direct proportional feedback control (PFC)piezoelectric patch sensors and actuators

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Electromagnetic effects in solid mechanics (74F15)

Related Items (1)

Optimal locations of magnetorheological fluid pockets embedded in an elastically supported honeycomb sandwich beams for supersonic flutter suppression

Cites Work

• A finite element study of the transverse shear in honeycomb cores
• Advances in the linear/nonlinear control of aeroelastic structural systems
• BUCKLING AND FLUTTER OF A COLUMN ENHANCED BY PIEZOELECTRIC LAYERS AND LUMPED MASS UNDER A FOLLOWER FORCE
• L¹group consensus of multi-agent systems with stochastic inputs under directed interaction topology
• SMART CONTROL OF NONLINEAR VIBRATIONS OF LAMINATED PLATES USING ACTIVE FIBER COMPOSITES
• Flutter control of a composite plate with piezoelectric multilayered actuators
• The forced vibration of a three-layer, damped sandwich beam with arbitrary boundary conditions

This page was built for publication: Active Flutter Control of a Supersonic Honeycomb Sandwich Beam Resting on Elastic Foundation with Piezoelectric Sensor/Actuator Pair