Abstract
The intent of this paper is to investigate the mechanics of delamination growth in an isotropic, ideally-brittle layered material under an impact load and to present guidelines for the design of more energy absorbent structures. Using a finite element model, both two- and three-layered configurations are considered. Prompted by the results from this model, closed-form solutions for the interlaminar shear strength and the interfacial fracture toughness corresponding to maximum energy absorption are derived for the two-layered laminate. These solutions were used to develop guidelines for the optimal design of two- and three-layered laminates.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 4181-4191 |
| Number of pages | 11 |
| Journal | Journal of Materials Science |
| Volume | 34 |
| Issue number | 17 |
| DOIs | |
| State | Published - 1999 |
All Science Journal Classification (ASJC) codes
- Ceramics and Composites
- Materials Science (miscellaneous)
- General Materials Science
- Mechanics of Materials
- Mechanical Engineering
- Polymers and Plastics
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