Sentence examples for behaviour of laminated composite from inspiring English sources

Most of the literature concentrated on low-velocity impact behaviour of laminated composite materials without any preloads.

The paper deals with structural behaviour of laminated composite plates under low velocity impact loading conditions.

The nonlinear free vibration behaviour of laminated composite shells subjected to hygrothermal environments is investigated using the finite element method.

As a case study, the mechanical behaviour of laminated composite beam (90°/0°/0°/90°) is examined from both a static and dynamic point of view.

In this paper, the Generalized Differential Quadrature (GDQ) method is applied to study the dynamic behaviour of laminated composite doubly-curved shells of revolution.

Numerical examples are presented to illustrate the effects of nonlocality, anisotropy, and the von Kármán type nonlinearity on the bending behaviour of laminated composite plates.

In this paper, a refined and simple theory of plates is presented and applied to the investigation of static, buckling, and free vibration behavior of laminated composite plates.

With the proposed model, one can accurately determine the behaviour of laminated composites with different material properties, straight or curvilinear fibres.

The present study concerns with the air damping influence on the dynamic behaviour of laminated composites plates with moderate damping level.

The ultimate objective of this study is to provide further understanding of the behaviour of laminated composites of varying lamina orientations and stacking sequences, when under high-velocity impact.

Robust buckling optimal design of laminated composite structures is conducted in this work.