Abstract
Fatigue damage growth mechanisms in [0]16 and [0, 90]4s laminates of APC-2 subjected to three-point flexure were studied using scanning electron microscopy. Building on an understanding gained from the study of statically tested samples, specific fatigue mechanisms were identified. For each laminate geometry a coherent progression of damage build-up is proposed.
Original language | English (US) |
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Pages (from-to) | 355-370 |
Number of pages | 16 |
Journal | Composites |
Volume | 26 |
Issue number | 5 |
DOIs | |
State | Published - May 1995 |
All Science Journal Classification (ASJC) codes
- General Materials Science