Damage evolution characterization and performance evaluation under realistic conditions
are essential to ensure reliable operation of critical safety components. However, previous …

Titanium alloys are high-quality materials for aerospace parts with good thermal mechanical
properties. Fatigue failure has been the most prominent problem, so surface strengthening …

To simulate the variational working conditions of the titanium fastener in the aero-engine,
variable cycle fretting wear tests were carried out for normal loading (80/40 N), frequency …

The present work uses machine learning to predict fretting crack lengths and corresponding
stress intensity factors (SIF) under partial slip conditions resulting in crack arrest. Plain …

Improving fatigue properties of engineering alloys using conventional laser shock peening
(LSP) with protective coating frequently causes surface grain subdivision, which is …

Metallic materials are widely used in many applications of mechanical and aerospace
engineering. Due to severe environmental and loading conditions, components and …

The need for very-high-cycle fatigue (VHCF) testing up to 1010 cycles of aviation gas turbine
engine blade materials under combined mechanical loads and complex environments has …

This study proposes a novel approach based on the covalent structure of diamond–graphite–
graphene (CDGG) to integrate the outstanding properties of diamond, graphite, and …

Laser ultrasonic technique has been increasingly implemented for nondestructive testing
and structural health monitoring. However, the poor signal-to-noise ratio (SNR) and low …

Fretting fatigue is a destructive failure that usually occurs in the parts or components in the
aviation field. One of the important research topics in fretting fatigue is the prediction of crack …