Tensile fracture simulation of random heterogeneous asphalt mixture with cohesive crack model

The microstructure and high cycle fatigue behavior of the in-situ TiB2/7050 composite were investigated in this work. The results showed that with the addition of sub-micron size TiB2 particles, the in-situ TiB2/7050 composite exhibited the smaller grain size, higher elastic modulus, enhanced yield strength and ultimate tensile strength, and superior fatigue limit over the unreinforced 7050 alloy. Through the fatigue tests, most of the fatigue cracks initiated at inclusions near the surface of both the composite and unreinforced alloy testing samples. The fatigue cracks initiation was induced by the stress concentration that was caused by the pileup of dislocations. In consideration of the improved fatigue properties of composites, the finer grains and higher elastic modulus in the composite were benefited to such enhancement. Critically, a new viewpoint was proposed that the submicron TiB2 particles impeded dislocations from piling up at the inclusions and delayed the crack initiation there, which can improve the fatigue property efficiently in the composite.

High cycle fatigue behavior of the in-situ TiB2/7050 composite

Preparation, microstructures and deformation behavior of SiCP/6066Al composites produced by PM route

Composite layer reinforced with quasicrystalline (QC) Al63Cu25Fe12 particles was fabricated on the surface of Al–6 Mg alloy specimens by ultrasonic impact peening (UIP). Stress-controlled fatigue response of the specimens was studied and compared with those for the annealed and UIP-treated specimens. The notch effect of the UIP induced surface roughness calculated in terms of the stress concentration factor does not exceed∼10%. XRD, OM and SEM analyses were used to characterize formed surface layers and fatigue fracture surfaces. Surface composite layer of 40–50 μm thick contains the homogeneously dispersed QC particles (the volume fraction Vf∼0.15) trapped by high compressive residual stresses. The layer demonstrates almost triple increase in microhardness comparing to that for the annealed alloy and twice exceeding of that for the UIP-treated specimen. Superior fatigue endurance of Al–6 Mg alloy after the UIP process and the UIP-induced formation of the composite layer is explained by sub-surface fatigue cracks’ initiation promoted with high compressive residual stresses and tight interfacial bonding of QC reinforcement and the matrix alloy. The improved fatigue behavior of the UIP-treated specimens in both the low cycle and high cycle regimes can be ensured by combination of the following favorable characteristics: (i) sufficiently high ductility and resistance to fatigue damage and crack growth in the core parent material along with (ii) superior fatigue strength supported by high microhardness and compressive stresses in the surface layer, which contains fine grained matrix and/or uniformly distributed and tightly bonded QC reinforcements.

Enhanced fatigue durability of Al-6Mg alloy by applying ultrasonic impact peening: Effects of surface hardening and reinforcement with AlCuFe quasicrystalline particles

Z.Z Chen

Papers

Effects of particle size on fatigue crack initiation and small crack growth in SiC particulate-reinforced aluminium alloy composites