Abstract
The constituents in a composite tend to reorganize during service. This gives rise to internal friction and slippage at the interfaces due to misfit. Energy release rate expressions are derived to quantify debonding. Two examples are provided to illustrate the method of solution.
Original language | English |
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Pages (from-to) | 203-207 |
Number of pages | 5 |
Journal | Theoretical and Applied Fracture Mechanics |
Volume | 32 |
Issue number | 3 |
DOIs | |
Publication status | Published - 1 Jan 1999 |
ASJC Scopus subject areas
- General Materials Science
- Condensed Matter Physics
- Mechanical Engineering
- Applied Mathematics