journal article·2002-08

Modeling of delamination using a discretized cohesive zone and damage formulation

Rikard Borg, Larsgunnar Nilsson, Kjell Simonsson

Composites Science and Technology· Volume 62· Issue 10-11
Publisher page

Abstract

Delamination initiation and growth are analyzed by using a discrete cohesive crack model. The delamination is constrained to grow along a tied interface. The model is derived by postulating the existence of a maximum load surface which limits the adhesive forces in the process zone of the crack. The size of this maximum load surface is made dependent on the amount of dissipated crack opening work, such that the maximum load surface shrinks to zero as a predefined amount of work is consumed. A damage formulation is used to reduce the adhesive forces. Mode I, II and III loading or any combined loading is possible. An analytical solution is obtained for a single mode opening and the implications of this result on the governing equations is discussed. The delamination model is implemented in the finite element code LS-DYNA and simulation results are shown to be in agreement with experimental results.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Fatigue and fracture mechanics

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (30)

Show source-provided references
1. Borg · 1998
2. Yielding of steel sheets containing slits10.1016/0022-5096(60)90013-2 ↗
3. The mathematical theory of equillibrium cracks in brittle fracture10.1016/S0065-2156(08)70121-2 ↗
4. Analysis of crack formation and crack growth in concrete by means of fracture mechanics and finite elements10.1016/0008-8846(76)90007-7 ↗
5. Analysis of a non-linear crack model10.1016/0022-5096(70)90011-6 ↗
6. Nilsson, L., Oldenburg, M. Nonlinear wave propagation in plastic fracturing materials—a constitutive modelling and finite element analysis. In: Nigual U, Engelbrecht J, editors. Nonlinear deformation waves. Berlin: Springer; 1983.10.1007/978-3-642-82006-9_20 ↗
7. Numerical simulations of quasibrittle fracture processes using the discrete cohesive crack model10.1016/S0020-7403(98)00115-5 ↗
8. A combined stress-based and fracture-mechanics-based model for predicting delamination in composites10.1016/0010-4361(93)90016-2 ↗
9. Modelling the effect of cracks on interlaminar shear strength10.1016/1359-835X(95)00007-O ↗
10. A continuum model for void nucleation by inclusion debonding10.1115/1.3173064 ↗
11. Effect of fiber debonding in a whisker-reinforced metal10.1016/0921-5093(90)90170-8 ↗
12. Numerical modeling of crack growth under dynamic loading conditions10.1007/s004660050194 ↗
13. Hybride finite element approach to quasi-brittle fracture10.1016/0045-7949(95)00444-0 ↗
14. Modelling of damage evolution in laminated viscoelastic composites10.1177/105678959700600103 ↗
15. Formulation of a three-dimensional cohesive zone model for application to a finite elements algorithm10.1016/S0045-7825(99)00211-X ↗
16. Crisfield M, Mi Y, Davies GAO, Hellweg HB. Finite element methods and the progressive failure-modelling of composites structures. In: Owen DRJ, Onate E, Hinton E, editors. Computational plasticity. Barcelona; 1997. p. 239–54.
17. Jansson N, Larsson R, Toll S. Finite element modelling of delamination progression under mixed mode loadings. In: Fiber reinforced composites 2000, composites for the millenium. Newcastle: 2000.10.1533/9780857093134.473 ↗
18. Modelling of splitting and delamination in notched cross-ply laminates10.1016/S0266-3538(00)00170-6 ↗
19. Delamination growth analysis in laminated structures with continuum-based 3d-shell elements and a viscoplastic softening model10.1016/S0045-7825(99)00255-8 ↗
20. Identification and forecast of delamination in composite laminates by an interlaminar interface model10.1016/S0266-3538(97)00144-9 ↗
21. Simulation of delamination in fiber composites by the use of a discrete cohesive-failure model10.1016/S0266-3538(00)00245-1 ↗
22. Hallquist · 1998
23. Fracture under combined loads by maximum energy release rate criterion10.1115/1.3424360 ↗
24. Greenhalgh G, Asp L, Singh S. Delamination resistance, failure criteria and fracture morphology of 0°/0°, 0°/5° and 0°/90° ply interfaces in CFRP. In: 5th International Conference on Deformation & Fracture of Composites, London, 1999.
25. Char · 1993
26. Hardening/softening plastic analysis of adhesive joints10.1061/(ASCE)0733-9399(1988)114:1(97) ↗
27. The effects of moisture and temperature on the interlaminar delamination toughness of a carbon/epoxy composite10.1016/S0266-3538(97)00222-4 ↗
28. Assessment of evaluation methods for the mixed-mode bending test10.1520/CTR10611J ↗
29. Numerical and experimental investigation of a composite enf-specimen10.1016/S0013-7944(99)00137-X ↗
30. LS-POST, a new post-processor from LS-DYNA. Livermore: Livermore Software Technology Corporation, 1999.