Abstract

This attempt proposes an engineering design approach to predict the high-cycle fatigue limit of shot-peened parts. The effects of the shot peening surface treatment on the high-cycle fatigue performance of Waspaloy, a nickel superalloy widely used in the airframe sector, are investigated. The proposed approach consists in (i) predicting the initial shot peening surface properties, (ii) simulating the evolution of the shot peening surface properties occurring during fatigue loading, and (iii) deducing the new fatigue limit of the shot-peened surface in the case of tensile, torsion, and combined tensile-torsion loading. The physical model is implemented and analyzed using the finite element analysis. The mathematical model sheds light on the evolution of the shot-peened surface performance. It allows determining the influence of the industrial parameters in order to optimize the shot peening process operating conditions. The prediction of the fatigue performance for different shot peening conditions leads to have physically consistent results.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.