Abstract
Composite degradation was investigated by measuring weight loss using quantitative methods. Weight loss experiments were performed on carbon fiber/epoxy laminates under both isothermal and dynamic conditions using various fiber directions and lay-up sequences in the laminate specimens. Weight loss rates were specimen geometry dependent, implying an anisotropic degradation behavior. A model was used to describe the sample weight loss at isothermal temperatures. The model was also used in combination with time-temperature superposition theory to predict the effect of thermal cycling on weight loss to understand the long-term properties of composites. It was found that the model successfully quantified the thermal degradation behavior observed under thermal cycling conditions.
| Original language | English |
|---|---|
| Pages (from-to) | 945-957 |
| Number of pages | 13 |
| Journal | Composites Part A: Applied Science and Manufacturing |
| Volume | 31 |
| Issue number | 9 |
| DOIs | |
| State | Published - Sep 2000 |