Abstract
In carrying out fatigue delamination propagation tests to assess the propagation rate versus a function of the energy release rate, the question arises as to the necessary number of cycles required to properly characterize the behavior. Tests were performed elsewhere on two different carbon/epoxy, multidirectional woven composite laminates containing a delamination using constant amplitude cycling by means of displacement control for various cycle ratios. The aim was to carry out the tests for (Formula presented.) cycles. Most specimens complied with this requirement. In this study, the fatigue data are analyzed including the first (Formula presented.) cycles, the first (Formula presented.) cycles, the first (Formula presented.) cycles, and (Formula presented.) cycles. It was seen that although the delamination length versus the cycle number could be quite similar between different cycle ranges, the Paris relation constants could be significantly different. It is suggested to carry out tests for as many cycles as possible.
| Original language | English |
|---|---|
| Pages (from-to) | 833-848 |
| Number of pages | 16 |
| Journal | Fatigue and Fracture of Engineering Materials and Structures |
| Volume | 47 |
| Issue number | 3 |
| DOIs | |
| State | Published - Mar 2024 |
Keywords
- constant amplitude
- energy release rate
- fatigue cycles
- fatigue delamination growth rate
- fiber reinforced polymer composites
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