Residual Stress Intensity Factor Based Fatigue Crack Growth Life Prediction for Laser Peened Structures
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2010-01-01
Conference paper
Electronic Resource
English
Stress Intensity Factor Based Spot Welds Fatigue Life Prediction Model
SAE Technical Papers | 2013
|Fatigue Crack Growth in Laser Shock Peened Ti-6AL-4V Aerofoils Subjected to Foreign Object Damage
British Library Conference Proceedings | 2012
|Fatigue life prediction of composite suspension considering residual stress and crack propagation
SAGE Publications | 2023
|