A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.
|Title of host publication||Theoretical and Applied Mechanics|
|Publisher||Univ of Tokyo Press|
|Number of pages||9|
|Publication status||Published - Dec 1 1985|
|Name||Theoretical and Applied Mechanics|
All Science Journal Classification (ASJC) codes
- Mechanics of Materials