Aman Garg , Neeraj Kumar Shukla , Mohamed-Ouejdi Belarbi , Debasis Mukherjee , M. Pushpavalli , Roshan Raman , Mehmet Avcar , Mandeep Singh Narula , Li Li
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引用次数: 0
Abstract
Bird strikes can potentially damage the aerospace and aeronautics structures and cause serious damage to the structure. In the present work, damage due to bird-strike in bio-inspired helicoidal laminated composite plates with circular and elliptical holes is predicted using Smoothed Particle Hydrodynamics (SPH)-Finite Element Method (FEM) model in ABAQUS. The Hashin failure model within ABAQUS has been implemented to model the impact-induced damage. The bird is modelled using the concepts of SPH to handle the mesh deformation problem effectively. Helicoidal recursive, exponential, semi-circular, linear, and Fibonacci helicoidal are studied during the present study. The plate is considered with two holes located at a quarter distance along the middle vertical axis of the plate. The damage in exponential, recursive, and linear helicoidal laminates is lesser than in conventional cross-ply and quasi-isotropic laminates. The plate with small dimensions of circular holes tends to deflect the failure in fibres towards the corners, while the plate with many holes arrests the cracks themselves. The plate with elliptical holes deflects the cracks towards themselves thus preventing the damage near the edges but damages the laminate in its vicinity.
期刊介绍:
Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to:
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