Damage Analysis of Laminated Plates using Continuum Damage Mechanics
Publish place: 07th Conference of Iranian Aerospace Society
Publish Year: 1386
Type: Conference paper
Language: English
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Document National Code:
AEROSPACE07_174
Index date: 22 July 2008
Damage Analysis of Laminated Plates using Continuum Damage Mechanics abstract
In this paper, progressive damage and global failure of composite laminates under quasi-static, monotonic loading are investigated using 3D continuum damage mechanics. For this purpose, a finite element program has been developed using an eight-node 2D layered element including layer-wise plate theory. A number of laminate examples with diffuse damage under simply supported and distributed transverse loading conditions are analyzed using the developed method. The effects of various lay-up configurations and numerical modeling parameters on the progressive damage response are also investigated.
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Damage Analysis of Laminated Plates using Continuum Damage Mechanics authors
B Mohammadi
Aerospace Engineering Department & Centre of Excellence in Computational Aerospace Engineering Amirkabir University of Technology, PhD Student
H Hosseini-Toudeshky
Associate Professor, (corresponding author)
M.H Sar-Lahidjani
Associate Professor,
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