Abstract
The bending load-deflection curves and fracture characteristics of a range of laminated Ti. (TiBw/Ti) composites were investigated under five modes. The results show ductile-brittle transition with decreasing Ti layer thicknesses and increasing volume fractions of TiBw, which is attributed to the constrained plastic deformation mechanism accompanying with high stress traixiality and tensile stress. The laminated composites with weak interfaces display superior fracture toughness under notched crack arrested orientation, which is related to the delamination cracks and multiple tunnel cracks. Moreover, single tunnel crack propagation and periodic multiple tunnel cracks were observed in the laminated composites under mode IV, which depend on the thickness and ultimate strength ratio of ductile Ti layer and tough TiBw/Ti composite layer. There are many interfacial delamination cracks and multiple tunneling cracks presented under mode V, playing an effective role in toughening the laminated composites. In addition, with decreasing the Ti layer thickness, laminated composites reveal obvious size effect characterized by more tunnel cracks.
| Original language | English |
|---|---|
| Pages (from-to) | 94-105 |
| Number of pages | 12 |
| Journal | Composites Science and Technology |
| Volume | 126 |
| DOIs | |
| State | Published - 1 Apr 2016 |
| Externally published | Yes |
Keywords
- Damage mechanics
- Fracture
- Layered structures
- Scanning electron microscopy (SEM)
- Welding/joining
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