Study on shear behavior of riveted lap joints of aircraft fuselage with different hole diameters and squeeze forces-Reference-Cited by-同舟云学术

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Study on shear behavior of riveted lap joints of aircraft fuselage with different hole diameters and squeeze forces

Published:2021-09 Issue: Volume:127 Page:105499
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Li Ming,Tian Wei,Hu Junshan,Wang Changrui,Liao Wenhe

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference53 articles.

1. The effect of residual stress due to interference fit on the fatigue behavior of a fastener hole with edge cracks;Zeng;Eng. Fail. Anal.,2016

2. Theoretical and experimental investigation on interference fit in electromagnetic riveting;Zhang;Int. J. Mech Sci.,2019

3. Riveting Process Modeling and Simulating for Deformation Analysis of Aircraft's Thin-walled Sheet-metal Parts;Zhang;Chin. J. Aeronaut.,2011

4. Fatigue life predictions for riveted lap joints;Skorupa;Int. J. Fatigue,2017

5. Study on analysis and prediction of riveting assembly variation of aircraft fuselage panel;Liu;Int. J. Adv. Manuf. Tech.,2014

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1. A prediction of crack propagation on aircraft wing via AK-TCN;Engineering Failure Analysis;2024-10

2. Stress, damage, and fatigue performance analysis of CFRP/Al double-sided countersunk riveted joints with variable rivet-hole clearance;International Journal of Fatigue;2024-09

3. Effect of ultrasonic amplitude and riveting speed on mechanical properties of Ti-45Nb riveted lap joints;Engineering Failure Analysis;2024-09

4. Effect of the countersunk rivet head dimensions on fatigue behavior of riveted specimens of 2024-T3 alloy;Aircraft Engineering and Aerospace Technology;2024-08-27

5. Static and fatigue performance of non-circular rivet joints: Comparison between numerical modelling and preliminary testing;Engineering Failure Analysis;2024-08

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