Abstract
Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.
Original language | English (US) |
---|---|
Pages (from-to) | 191-198 |
Number of pages | 8 |
Journal | Composites |
Volume | 22 |
Issue number | 3 |
DOIs | |
State | Published - May 1991 |
All Science Journal Classification (ASJC) codes
- General Materials Science