Sentence examples for behaviour of general laminates from inspiring English sources

The behaviour of general laminates substantially differs from that of laminates with a symmetric layup or isotropic materials.

As the failure of fibre-reinforced angle-ply composite laminates involves basic features of failure of general laminates, its understanding and prediction are of fundamental importance.

This framework is based on invariant-based approaches to predict the stiffness and the strength of general laminates, and an analytical model to estimate the R-curve of balanced laminates.

This paper summarises recent theoretical modelling developed by the authors on stiffness property degradation and mechanical behaviour of general symmetric laminates with off-axis ply cracks and crack-induced delaminations.

Good agreements between DEM, Finite Element and theoretical results prove the capability of this developed DEM approach for modelling the elastic behaviour of general FRP composite lamina and laminates.

The present paper deals with the buckling and post-buckling behaviour of plates made of coupling laminates (the so-called general laminates).

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.

Behaviour of fibre metal laminates subjected to localised blast loading: part II – quantitative analysis.

The paper presented deals with the fracture behaviour of ceramic laminates.

Behaviour of fibre metal laminates subjected to localised blast loading: part I – experimental observations and failure analysis.

The behaviour of composite laminates subject to transverse load introduction has been investigated experimentally and numerically.