Fiber bridging has a significant influence on the delamination propagation behavior in
multidirectional composite laminates. Traditional pure mode I bilinear cohesive zone models …

This article explores the experimental and numerical study in ABAQUS/explicit of the post-
impact damage progression in carbon/epoxy composite laminate under compression. LVI …

In this work, the synergistic effect of 3D orthogonal woven structure and asymmetric
carbon/glass hybridization on impact response was studied by experimental and numerical …

In this work, two numerical procedures based on Finite Elements Method (FEM) have been
developed in order to simulate the Lamb wave propagation in Low Velocity Impact (LVI) …

A comprehensive Isogeometric Analysis framework for damage modeling of laminated
composite structures is presented. The formulation is based on a multilayer approach that …

There is a lack of research available on how thin laminates respond to impact and post
impact loads, even though thin structures are used in present-day aircrafts. This …

This paper studied the effects of Z-pin insertion angles (60°, 75° and 90°) on the behavior
and failure modes of compression after impact (CAI) for composite laminates. Unpinned and …

Recent research has been devoted to thin laminates as a result of aeronautic industries
shifting to thinner and lighter structures. In an attempt to improve the out-of-plane response …

The manufacturing process of fiber reinforced polymer laminates could induce local
distortions from the nominal fiber architecture. Further, low-velocity impact events may …

The sensitivity of off-axial angle on impact response was investigated by experimental and
numerical methods in this work. Three types of braided laminates with different on/off-axial …