The important phenomenon of delamination buckling is examined subjected to the condition of frictionless contact. Buckled delamination is examined in particular, because in-plane compressive loading is typical and detrimental. Two types of contact can be distinguished, local and global. The latter may occur everywhere in the plate while the local contact is limited to the crack front (negative KI stress intensity factors). Both local and global contact conditions were considered using a finite element scheme which employed nonlinear plate theory. The global contact problem is formulated as it appears in post-buckling of delamination. The case of simultaneous buckling and contact is also addressed in this paper. Two particularly interesting examples of thin film delaminations are presented. In the first, the contact at buckling is due to the material anisotropy. In this case the bucking load and the post-bucking analysis were very well supported by experiments. In the second example, contact at buckling arises because of a pin that holds down the delaminated layer at its center. The treated cases indicated that contact may significantly affect the fracture parameters along the delamination front, and is, therefore, important for delamination arrest.
Skip Nav Destination
Article navigation
December 1995
Technical Papers
The Contact Problem at Delamination
A. E. Giannakopoulos,
A. E. Giannakopoulos
Department of Solid Mechanics, Royal Institute of Technology, S-10044 Stockholm, Sweden
Search for other works by this author on:
K.-F. Nilsson,
K.-F. Nilsson
Aeronautical Research Institute of Sweden, S-16111 Bromma, Sweden
Search for other works by this author on:
G. Tsamasphyros
G. Tsamasphyros
Department of Theoretical and Applied Mechanics, National Technical University of Athens, Athens 15774, Greece
Search for other works by this author on:
A. E. Giannakopoulos
Department of Solid Mechanics, Royal Institute of Technology, S-10044 Stockholm, Sweden
K.-F. Nilsson
Aeronautical Research Institute of Sweden, S-16111 Bromma, Sweden
G. Tsamasphyros
Department of Theoretical and Applied Mechanics, National Technical University of Athens, Athens 15774, Greece
J. Appl. Mech. Dec 1995, 62(4): 989-996 (8 pages)
Published Online: December 1, 1995
Article history
Received:
July 17, 1992
Revised:
June 20, 1994
Online:
October 30, 2007
Citation
Giannakopoulos, A. E., Nilsson, K., and Tsamasphyros, G. (December 1, 1995). "The Contact Problem at Delamination." ASME. J. Appl. Mech. December 1995; 62(4): 989–996. https://doi.org/10.1115/1.2896034
Download citation file:
Get Email Alerts
Interplay Between Nucleation and Kinetics in Dynamic Twinning
J. Appl. Mech (December 2024)
Elastic Localization With Particular Reference to Tape-Springs
J. Appl. Mech (December 2024)
Related Articles
On Interface Crack Growth in Composite Plates
J. Appl. Mech (September,1992)
Delamination of Compressively Stressed Orthotropic Functionally Graded Material Coatings Under Thermal Loading
J. Appl. Mech (September,2008)
Assessment of the Fracture Behavior of an Asymmetrically Loaded Cantilever Composite Structure
J. Eng. Mater. Technol (October,2003)
Local Delamination Buckling of a Laminated Beam due to Three-Point Bending
J. Eng. Mater. Technol (July,2010)
Related Proceedings Papers
Related Chapters
A Cumulative Damage Model for Continuous Fiber Composite Laminates with Matrix Cracking and Interply Delaminations
Composite Materials: Testing and Design (Eighth Conference)
Subsection NB—Class 1 Components
Companion Guide to the ASME Boiler and Pressure Vessel Code, Volume 1, Third Edition
Fatigue Fracture of Thin Plates Under Tensile and Transverse Shear Stresses
Fracture Mechanics: 26th Volume