Abstract
Recent efforts in the finite element modelling of delamination have concentrated on the development of cohesive interface elements. These are characterised by a bilinear constitutive law, where there is an initial high positive stiffness until a threshold stress level is reached, followed by a negative tangent stiffness representing softening (or damage evolution). Complete decohesion occurs when the amount of work done per unit area of crack surface is equal to a critical strain energy release rate. It is difficult to achieve a stable, oscillation-free solution beyond the onset of damage, using standard implicit quasi-static methods, unless a very refined mesh is used. In the present paper, a new solution strategy is proposed based on a pseudo-transient formulation and demonstrated through the modelling of a double cantilever beam undergoing Mode I delamination. A detailed analysis into the sensitivity of the user-defined parameters is also presented. Comparisons with other published solutions using a quasi-static formulation show that the pseudo-transient formulation gives improved accuracy and oscillation-free results with coarser meshes.
| Original language | English |
|---|---|
| Pages (from-to) | 698-708 |
| Number of pages | 11 |
| Journal | Finite Elem Anal Des |
| Volume | 42 |
| Issue number | 8-9 |
| DOIs | |
| Publication status | Published - 2006 |
| Externally published | Yes |
Notes
WIP AS TBAKeywords
- Composite laminates Delamination Interface elements Non-linear analysis Transient solution Cantilever beams Composite materials Cracks Energy dissipation Finite element method Laminates Stability Stiffness Stresses Coarser meshes Oscillation-free results Pseudo-transient formulation Quasi-static methods