A 3D progressive failure model for crushing simulations in composite structures
Volume: 27, Issue: 2, Pages: 591 - 613
Published: Oct 23, 2020
Abstract
A constitutive damage model is proposed in order to investigate the crushing response of crossply and 0° plies composite laminates, using a VUMAT subroutine implemented in ABAQUS/Explicit. This damage model predicts five failure modes commonly observed in unidirectional (UD) carbon fibres reinforced composite structures: fibre failure in tension, fibre failure in compression, matrix cracking in tension, matrix cracking in compression and...
Paper Details
Title
A 3D progressive failure model for crushing simulations in composite structures
Published Date
Oct 23, 2020
Volume
27
Issue
2
Pages
591 - 613
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