Fatigue Life Extension of AA2024 Specimens and Integral Structures by Laser Shock Peening

Fatigue Life Extension of AA2024 Specimens and Integral Structures by Laser Shock Peening

The goal of the present study is to understand the effects of laser shock peening (LSP)-induced residual stresses on the fatigue crack propagation (FCP) behaviour of the commonly used aircraft aluminium alloy AA2024 in T3 heat treatment condition. LSP treatment was performed using a pulsed Nd:YAG la...

Full description

Bibliographic Details
Main Authors: Kashaev Nikolai, Chupakhin Sergey, Ventzke Volker, Horstmann Manfred, Riekehr Stefan, Barbini Alessandro, dos Santos Jorge. F., Keller Sören, Klusemann Benjamin, Huber Norbert
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201816518001

Internet

https://doi.org/10.1051/matecconf/201816518001

Similar Items