Crack growth life calculation approach of surface cracked landing gear strut under eccentric compression load by bulging effect-Reference-Cited by-同舟云学术

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Crack growth life calculation approach of surface cracked landing gear strut under eccentric compression load by bulging effect

Published:2023-08 Issue: Volume:173 Page:107652
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Zhang Lin^ORCID,Wei Xiaohui

Publisher

Elsevier BV

Reference35 articles.

1. Failure analysis of landing gears strut bearings;Turan;Eng Fail Anal,2017

2. Effect of selective laser treatment on initiation of fatigue crack in the main part of an undercarriage drag strut;Bien;Chin J Aeronaut,2019

3. Noise characterization of a full-scale nose landing gear;Bennett;J Aircr,2018

4. Initial position optimization of preform for large-scale strut forging;Zhang;Int J Adv Manuf Technol,2018

5. On the mixed mode II/III fatigue threshold behaviour for aluminium alloys 2014-T6 and 7075-T6;Merati;Fatigue Fract Eng Mater Struct,2012

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1. Deformation behavior and microstructure-property evolution of high-strength ultra-thin NC NiCo alloys under high-energy laser shock;Journal of Materials Processing Technology;2025-08

2. Efficient multidisciplinary modeling of aircraft undercarriage landing gear using data-driven Naïve Bayes and finite element analysis;Multiscale and Multidisciplinary Modeling, Experiments and Design;2024-03-16

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