Composite materials are becoming the most useful material for aircraft structures. Their main
advantage is connected to the possibility of deeply reducing weight and costs by …

This study investigates the interply hybridization of carbon fibre reinforced polymer (CFRP)
composite laminate to improve the flexural performance and cost efficiency. Carbon layers …

The objective of this work is the characterization and the assessment of the damage in
CFRP composite laminates with different stacking sequences subjected to low velocity …

Composite structures are particularly vulnerable to impact which drastically reduces their
residual strength [1–3]. In this work, the influence of laminate thickness, ply-stacking …

In this work, we design, manufacture, test and discuss the first bio-inspired microstructural
concept to enhance longitudinal compressive performance of multidirectional (MD) Carbon …

Tensile and compressive properties of interlayer and intralayer hybrid composites were
investigated in this paper. The tensile modulus and compression modulus of interlayer and …

The objective of this study is to characterize the damage in glass fiber reinforced composite
laminated reinforced with nanosilica particles subjected to tensile, flexural, and transverse …

Most of the composite materials that are used in aerospace structures have been
manufactured using a thermostable matrix, as epoxy resin. The region of stability of these …

The cement stabilized macadam base experiences tensile and compressive stresses
simultaneously in the actual pavement structures, resulting in the influence of stress states …

Tensile tests on bonded, bolted and hybrid bolted/bonded carbon fibre reinforced polymer
(CFRP) joints were designed with four stacking sequences. The force-displacement curves …