Paper Title:
Fatigue Delamination Analysis of Composite Laminates with a Central Hole Using Interface Elements
  Abstract

In this paper a solid like interface element along with a fatigue constitutive law is used to study the damage behaviour of holed composite laminates under cyclic loading. For this purpose a user element routine and a material routine was developed include the interface element and to handle the formulation of progressive fatigue damages. The developed procedure is used to predict delamination initiation and growth in mixed-mode condition for a typical composite laminate. The obtained results for damage and stresses are compared with the available results in the literature.

  Info
Periodical
Key Engineering Materials (Volumes 471-472)
Edited by
S.M. Sapuan, F. Mustapha, D.L. Majid, Z. Leman, A.H.M. Ariff, M.K.A. Ariffin, M.Y.M. Zuhri, M.R. Ishak and J. Sahari
Pages
568-571
DOI
10.4028/www.scientific.net/KEM.471-472.568
Citation
H. Hosseini-Toudeshky, A. Jasemzadeh, B. Mohammadi, "Fatigue Delamination Analysis of Composite Laminates with a Central Hole Using Interface Elements", Key Engineering Materials, Vols. 471-472, pp. 568-571, 2011
Online since
February 2011
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$32.00
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