Preparation and Mechanical Properties of Ceramic Fiber Reinforced Titanium-Based Hybrid Laminated Composite

Figure 11

Failure mechanism schematic diagrams for the three-point bending of the composite: (a) initial loading stage; (b) stage of brittle fiber fracture under the load; (c) stage for the formation of crack sources on the surface; (d) initial stage of crack propagation; (e) cross-layer stage of crack propagation; and (f) failure stage of crack propagation.

(a)

(b)

(c)

(d)

(e)

(f)