Abstract
The response of thermoplastic AS-4/PEEK composite laminates of two lay-ups, such as cross-ply and quasi-isotropy, subjected to tension-tension (T-T) fatigue loading at elevated temperatures was investigated. It is found that the ultimate strength of cross-ply laminate is higher than that of quasi-isotropic laminate at various temperatures, so does the fatigue strength. However, the slope of normalized stress vs. cycles curves in the quasi-isotropic laminates is higher than that of the cross-ply laminates at elevated temperatures. Finally, the simple semi-empirical predictive models in statistical analysis and multiple regressions are proposed and provided for design and application purposes.
| Original language | English |
|---|---|
| Pages (from-to) | 1142-1146 |
| Journal | Composites Part B: Engineering |
| Volume | 39 |
| Issue number | 7-8 |
| Online published | 8 Apr 2008 |
| DOIs | |
| Publication status | Published - Oct 2008 |
| Externally published | Yes |
Research Keywords
- A. Laminates
- B. Fatigue
- B. Mechanical properties
- C. Statistical properties/methods
Fingerprint
Dive into the research topics of 'Fatigue response of APC-2 composite laminates at elevated temperatures'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver