scispace - formally typeset
S

S. Raja

Researcher at National Aerospace Laboratories

Publications -  72
Citations -  1025

S. Raja is an academic researcher from National Aerospace Laboratories. The author has contributed to research in topics: Finite element method & Active vibration control. The author has an hindex of 17, co-authored 68 publications receiving 840 citations. Previous affiliations of S. Raja include Council of Scientific and Industrial Research & Nagoya University.

Papers
More filters
Journal ArticleDOI

Active vibration control of composite sandwich beams with piezoelectric extension-bending and shear actuators

TL;DR: In this paper, a finite element formulation capable of modeling two different kinds of piezoelastically induced actuation in an adaptive composite sandwich beam is derived to couple certain piezoelectric constants to a transverse electric field to develop extension-bending actuation and shear-induced actuation.
Journal ArticleDOI

Vibro-acoustic response and sound transmission loss analysis of functionally graded plates

TL;DR: In this paper, an analytical study on the vibro-acoustic and sound transmission loss characteristics of functionally graded material (FGM) plates using a simple first-order shear deformation theory is presented.
Journal ArticleDOI

Flutter control of a composite plate with piezoelectric multilayered actuators

TL;DR: In this paper, an active flutter velocity enhancement scheme is presented for lifting surfaces, employing Linear Quadratic Gaussian based multi-input multi-output controller with multilayered piezoelectric actuators.
Journal ArticleDOI

Thermally induced vibration control of composite plates and shells with piezoelectric active damping

TL;DR: In this paper, a coupled piezoelectric field is modelled with an expansion strain in the numerical formulation to analyse piezohygrothermoelastic laminated plates and shells.
Journal ArticleDOI

Active vibration control of smart plates with partially debonded multilayered PZT actuators

TL;DR: In this article, the influence of actuator damage on the performance of closed loop vibration control is numerically evaluated and debonding is considered a damage mode and finite element procedures are subsequently developed to introduce its effect on system matrices, namely elastic and electro-elastic stiffness.