In the present paper, an isogeometric analysis formulation along with the Nitsche technique
is implemented based on the first order shear deformation plate theory to investigate the …

In this paper, a novel iterative finite element method (FEM) for energy harvesting purpose is
presented. In this iterative FEM, the electromechanical coupling in the governing …

With the growing popularity of composite materials in aeronautics, the study of the influence
of their anisotropic properties has been extended from the classical structural problems to …

In this paper, a novel approach in assessing the structural integrity of cracked composite
plates under the aeroelastic condition by using XFEM is presented. To the authors' …

The multiphase composite with active structural fiber (ASF) has proven able to provide better
optimization between actuating and load bearing capability compared to a pure …

A finite element model for predicting the nonlinear aeroelastic behavior of composite panels
undergoing intralaminar and translaminar progressive damage in supersonic flow is …

A method based on fluid–structure coupling is used in this study to calculate the response of
a rocket fairing as it is falling. Some cases of vibration divergence of the fairing were found …

This article deals with the investigation of delamination effects on the flutter behavior of a
composite wing subjected to unsteady aerodynamic loads by providing an integrated …

The Effect of Fiber Orientation and Crack on Dynamic Characteristics of a Unidirectional
Composite Cantilevered Wing Plate title Title Author Issue Keywords Current Issue : Vol 15, No …

This paper deals with the investigation of the influence of edge surface crack on the flutter
behavior of unidirectional fiber-reinforced composite wing subjected to unsteady …