Paper Title:
Cohesive Zone Parameters for the Interface between NiTi Shape Memory Alloy and CFRP
  Abstract

To explore the structural strength of CFRP shape memory alloy composites, it is necessary to evaluate the interface bonding strength. Jang and Kishi experimentally investigated the adhesive strength between NiTi fibers and CFRP composite [1]. In this paper, the interface de-decohesion behavior was simulated by three-dimensional cohesive zone method. The values of related numerical parameters were chosen to fit the experimental result.

  Info
Periodical
Key Engineering Materials (Volumes 321-323)
Edited by
Seung-Seok Lee, Joon Hyun Lee, Ik Keun Park, Sung-Jin Song, Man Yong Choi
Pages
196-199
DOI
10.4028/www.scientific.net/KEM.321-323.196
Citation
S. Y. Yang, "Cohesive Zone Parameters for the Interface between NiTi Shape Memory Alloy and CFRP", Key Engineering Materials, Vols. 321-323, pp. 196-199, 2006
Online since
October 2006
Authors
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Cedric Lequesne, A. Plumier, H. Degee, Anne Marie Habraken
Abstract:The fatigue behaviour of the welded beam-to-column connections of steel moment resisting frame in seismic area must be evaluated. The...
847
Authors: Felicia Stan
Abstract:This paper presents a computational framework for simulation of delamination that combines the features of the discontinuous Galerkin methods...
501
Authors: Vladislav Kozák, Zdeněk Chlup
Abstract:Ceramic matrix composites reinforced by unidirectional long ceramic fibre are very perspective materials. The only disadvantage of such...
231
Authors: Jin Chang Wang, Lei Zhang, Jia Min Zhang
Chapter 7: Road and Railway Engineering
Abstract:The research methods of Cohesive Zone Model (CZM) are introduced and the parameters of cohesive zone model in ABAQUS software are calibrated...
1503
Authors: Ai Min Jiang, Gao Chun Li, Ai Ping Tian
Chapter 4: Material Engineering and its Application Technology
Abstract:In order to analyze failure phenomena and mechanical properties of propellant-liner interface material, both experimental study and modeling...
291