A new multiaxial fatigue life prediction model for aircraft aluminum alloy-Reference-Cited by-同舟云学术

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A new multiaxial fatigue life prediction model for aircraft aluminum alloy

Published:2021-02 Issue: Volume:143 Page:105993
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Zhao Bingfeng^ORCID,Xie Liyang^ORCID,Wang Lei,Hu Zhiyong,Zhou Song,Bai Xin

Funder

Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

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

Reference59 articles.

1. Prediction of fatigue life in aircraft double lap bolted joints using several multiaxial fatigue criteria;Esmaeili;Mater Des,2014

2. Outcomes from the fatigue testing of seventeen centre fuselage structures;Molent;Int J Fatigue,2018

3. Computational-experimental approaches for fatigue reliability assessment of turbine bladed disks;Zhu;Int J Mech Sci,2018

4. On the fatigue crack growth analysis of spliced aircraft wing panels under sequential axial and shear loads;Yu;Eng Fract Mech,2014

5. Influence of solution treatment on the corrosion fatigue behavior of an as-forged Mg-Zn-Y-Zr alloy;Wang;Int J Fatigue,2019

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