Surface and thermal load effects on the buckling of curved nanowires

This paper investigates the impact of surface energy and thermal loading on the static stability of nanowires. We model nanowires as curved fixed–fixed Euler-Bernoulli beams and use Gurtin-Murdoch model to represent surface energy. The model takes into account both von Kármán strain and axial strain. We derive the nanowire equilibrium equations and deploy it to investigate the buckling of nanowires. We report the wire rise, critical buckling loads, and buckled wire configurations as functions of axial load in the presence of thermal loads. We found that surface energy has significant effect on the behaviour of silicon nanowires of diameter less than 4 nm. We also found that critical buckling load increases with increase in surface tensile stress and decreases with thermal loading

Sandwich composite laminate with intraply hybrid woven CFRP/dyneema core for enhanced impact damage resistance and tolerance

The present paper investigates the response a sandwich composite laminate that involves intraply hybrid carbon fiber reinforced polymer (CFRP)/Dyneema core under impact and post-impact tests. This intraply hybrid core was designed to gain the high elasticity and high stiffness/weight ratio of Dyneema fibers while maintaining the structural integrity of CFRP at the laminate core. Low-velocity impact and compression after impact tests were employed to evaluate the damage resistance and tolerance of the laminates. Micro-computed tomography was deployed to inspect the different modes of damage and their propagation during low-velocity impact. The results showed that the damage started in the sandwich composite as localized matrix cracks and delaminations at CFRP impacted face. However, it was distributed through the whole laminate thickness in the monolithic CFRP composites. The fiber cut initiated at 70 J impact energy for the sandwich composite at the impacted CFRP face plies as fiber kinking due to compressive stresses. However, it was initiated at the lower plies of the CFRP composite at 30 J due to high bending and normal strains. This delayed fiber breakage revealed the better residual compression after impact (CAI) strength of the sandwich composite, where it showed 33.5% improved specific CAI strength compared to the monolithic CFRP composite