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The behaviour of balanced laminates (symmetric, antisymmetric and asymmetric) under repeated low energy hits of a 12.1 mm hemispheric impactor was evaluated.
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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.
Thermo-elastic constants of symmetric and balanced laminates with intralaminar cracks in 90-layers depend on the opening displacement (COD) of the crack.
This interaction function multiplied with COD of non-interactive crack is the input parameter in analytical model for thermo-elastic properties of damaged symmetric and balanced 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 general laminates substantially differs from that of laminates with a symmetric layup or isotropic materials.
Analytical and semi empirical models were evaluated and validated to predict the influence of the geometric parameters on the impact behaviour of the laminates.
The behaviour of composite laminates subject to transverse load introduction has been investigated experimentally and numerically.
In the present study, the low velocity impact behaviour of TRC laminates is investigated more closely and this by means of an instrumented drop weight test.
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