Abstract
The applicability range of toughness-and strength-based criteria for progressive cracking of a transverse layer in a cross-ply composite laminate subjected to tensile loading is considered. Using a deterministic cracking model, approximate relations for the crack density as a function of stress are derived for initiation-and propagation-controlled types of cracking. The master-curve approach is applied to progressive cracking in glass/epoxy laminates. The accuracy of estimation of laminate stiffness reduction by using crack density master curves is evaluated.
| Original language | English |
|---|---|
| Pages (from-to) | 441-450 |
| Number of pages | 10 |
| Journal | Mechanics of Composite Materials |
| Volume | 44 |
| Issue number | 5 |
| DOIs | |
| Publication status | Published - Sept 2008 |
Keywords
- Intralaminar cracking
- Laminate
- Polymer-matrix composite
- Stiffness
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