A low cycle fatigue life model for a shot peened gas turbine disc alloy-Reference-Cited by-同舟云学术

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A low cycle fatigue life model for a shot peened gas turbine disc alloy

Published:2019-07 Issue: Volume:124 Page:34-41
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Eriksson Robert,Moverare Johan,Chen Zhe^ORCID

Funder

the European Union’s Horizon 2020 research and innovation programme

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference35 articles.

1. The superalloys — fundamentals and applications;Reed,2008

2. Finite element modeling of shot peening residual stress relaxation in turbine disk assemblies;Meguid;J Eng Mater Technol,2015

3. Computational framework for multiaxial fatigue life prediction of compressor discs considering notch effects;Liao;Eng Fract Mech,2018

4. Strain energy gradient-based lcf life prediction of turbine discs using critical distance concept;Zhu;Int J Fatigue,2018

5. Fatigue crack initiation and propagation on shot-peened surfaces in A316 stainless steel;De los Rios;Int J Fatigue,1995

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