The distortion in machining aeronautical aluminum alloy parts (AAAPs) is one of the serious
challenges in the aviation industry, and the residual stresses produced in …

Laser shock peening (LSP) is successfully applied to retard fatigue cracks in metallic
lightweight structures by introducing specific, in particular compressive, residual stress …

Engineering of component surfaces using Laser Shock Peening (LSP) requires optimisation
of key process parameters to enhance performance through the generation of beneficial …

Femtosecond laser shock peening (FsLSP) is performed on engineering alloys to improve
their wear resistance in dry and oil-lubricated sliding conditions. In this study, the influence …

In this study, the fretting wear test was performed on DD6 single-crystal superalloy after
femtosecond laser modification (FLM) to evaluate the influence of femtosecond laser …

Studying the distribution and history of residual stresses through different laser impact
strategies is essential to assess alloy components structure, failure mechanisms, and alloy …

Laser shock peening is a promising surface modification technology to improve the
properties of metal. In this work, the spatial distribution model of the shock wave pressure …

Laser shock peening (LSP) is an emerging technique for effectively forming metal sheets
due to its ability to produce higher and deeper compressive residual stress than …

Two sided laser shock processing (TSLSP) has been an innovative process to impart the
favorable compressive residual stresses into thin components without producing excessively …

An explicit 3D Finite Element (FE) model was developed in the LS-Dyna code to simulate
the laser shock paint strip** on aircraft aluminum substrates. The main objective of the …