Sentence examples for behaviour of laminates under from inspiring English sources

The behaviour of laminates under compression was always characterized by global buckling due to the small thickness.

Delamination responses among plies and fibre and/or matrix damage responses within plies are simulated to understand the behaviours of laminates under different impaction conditions.

The impact behaviour of composite laminates under low velocity impact load is investigated by considering the influence of stacking sequence and laminate thickness in terms of contact loads, absorbed energy and delamination extent.

The results presented in this investigation could be useful for a better understanding of the behaviour of sandwich laminates under free vibration conditions and potentially beneficial for designers of sandwich structures.

Results from a recent research project, presented here in two parts, aim to contribute to the better understanding of fatigue behaviour of GRP laminates under complex in-plane stress states.

This strategy is used as an identification scheme in the modelling of non-linear mechanical behaviour of laminate composites.

The behaviour of balanced laminates (symmetric, antisymmetric and asymmetric) under repeated low energy hits of a 12.1 mm hemispheric impactor was evaluated.

This paper presents an optimisation strategy for the design of postbuckling behaviour of VAT composite laminates under axial compression.

A set of equations is proposed to describe the fatigue behaviour of E-glass laminates under loads with various means and amplitudes.

In this work, the analysis of the impactor mass effect on the behaviour of carbon/epoxy woven laminates under low velocity impact is carried out.

In other space specimens we incorporate metal patch inside the laminate beam to see the influence of these patch on the behaviour of the laminates.