196-206A simple analytical formulation of laminated composite plates with integrated piezoelectric layer, used as sensor and actuators for the vibration suppression of intelligent composite and sandwich plates is presented. The first order shear deformation theory is employed to account for the transverse shear deformation. The equations are transformed into the state space form and solved by the linear quadratic regulator (LQR) based control algorithm. The effect of the state and control parameters on the system response is studied. The effect of the thickness ratio of the intelligent plate is also investigated
The advent of high strength and light weight composite materials and newly developed smart materials...
Vibration reduction possibilities in laminated composite with one of the plies as actuation layer, h...
A finite-element model is developed for the active buckling control of laminated composite plates us...
Summarization: A finite element analysis for the approximation of the dynamic response of laminate c...
This paper deals with the active vibration control of piezoelectric sandwich plate. The structure co...
ABSTRACT: This paper proposes an active vibration control technique, which is based on linear matrix...
ABSTRACT: This paper proposes an active vibration control technique, which is based on linear matrix...
Active vibration control of intelligent laminated composite plates is performed experimentally. Lami...
A finite element formulation is presented for modeling the behavior of laminated composites with int...
In aerospace engineering, sandwich construction is preferred not only for its great decrease in weig...
We have used a modal control approach to suppress the vibration amplitude of a laminated composite p...
We have used a modal control approach to suppress the vibration amplitude of a laminated composite p...
Summarization: In smart structural applications, multi-layered piezocomposite plates are very common...
Vibration reduction possibilities in laminated composite with one of the plies as actuation layer, h...
The advent of high strength and light weight composite materials and newly developed smart materials...
The advent of high strength and light weight composite materials and newly developed smart materials...
Vibration reduction possibilities in laminated composite with one of the plies as actuation layer, h...
A finite-element model is developed for the active buckling control of laminated composite plates us...
Summarization: A finite element analysis for the approximation of the dynamic response of laminate c...
This paper deals with the active vibration control of piezoelectric sandwich plate. The structure co...
ABSTRACT: This paper proposes an active vibration control technique, which is based on linear matrix...
ABSTRACT: This paper proposes an active vibration control technique, which is based on linear matrix...
Active vibration control of intelligent laminated composite plates is performed experimentally. Lami...
A finite element formulation is presented for modeling the behavior of laminated composites with int...
In aerospace engineering, sandwich construction is preferred not only for its great decrease in weig...
We have used a modal control approach to suppress the vibration amplitude of a laminated composite p...
We have used a modal control approach to suppress the vibration amplitude of a laminated composite p...
Summarization: In smart structural applications, multi-layered piezocomposite plates are very common...
Vibration reduction possibilities in laminated composite with one of the plies as actuation layer, h...
The advent of high strength and light weight composite materials and newly developed smart materials...
The advent of high strength and light weight composite materials and newly developed smart materials...
Vibration reduction possibilities in laminated composite with one of the plies as actuation layer, h...
A finite-element model is developed for the active buckling control of laminated composite plates us...