Skip to main navigation Skip to search Skip to main content

Laser shock peening process modelling and experimental validation of AA2198-T3 and AA2198-T8

Research output: Journal contributionsConference article in journalResearchpeer-review

Abstract

Laser shock peening (LSP) is a surface treatment which improves the fatigue life of metallic structures by laser‐induced compressive residual stresses. The purpose of this work is the prediction of the measured residual stresses after LSP in sheets consisting of AA2198. Therefore, a finite element model is set‐up. The Johnson‐Cook material model is used to model the strain rate depend material behaviour during plastic deformations. Stress averaging enables the comparison between measured and predicted residual stresses. Residual stress measurements are performed using the incremental hole drilling method. The initially unknown pressure pulse is identified for AA2198‐T3 and validated with AA2198‐T8. (© 2017 Wiley‐VCH Verlag GmbH & Co. KGaA, Weinheim)

Bibliographical note

Volume 17 (2017) of PAMM “Proceedings in Applied Mathematics and Mechanics” assembles the contributions to the 88th Annual Meeting of the Gesellschaft für Angewandte Mathematik und Mechanik (GAMM), held 6 – 10 March 2017 at Weimar. Issue Online 15 March 2018

Research areas and keywords

  • Engineering

Fingerprint

Dive into the research topics of 'Laser shock peening process modelling and experimental validation of AA2198-T3 and AA2198-T8'. Together they form a unique fingerprint.

Cite this