Influence of riveting die configuration and squeeze force on the mechanical properties and fatigue behavior of aircraft lap joints-Reference-Cited by-同舟云学术

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Influence of riveting die configuration and squeeze force on the mechanical properties and fatigue behavior of aircraft lap joints

Published:2022-12 Issue: Volume:142 Page:106772
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^ORCID,Shi ZhangHu,Liao WenHe

Funder

National Key Research and Development Program of China

National Defense Basic Scientific Research Program of China

National Natural Science Foundation of China

Young Scientists Fund

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference41 articles.

1. Experimental and numerical investigation on the fretting fatigue behavior of cold expanded Al-alloy 2024–T3 plates;Chakherlou;Eng. Fail. Anal.,2021

2. Fractographic examination of coupons representing aircraft structural joints with and without hole cold expansion;Yanishevsky;Eng. Fail. Anal.,2013

3. An experimental and numerical investigation of clamping force variation in simple bolted and hybrid (bolted-bonded) double lap joints due to applied longitudinal loads;Esmaeili-Goldarag;Eng. Fail. Anal.,2018

4. The effect of bolt clamping force on the fracture strength and the stress intensity factor of a plate containing a fastener hole with edge cracks;Chakherlou;Eng. Fail. Anal.,2009

5. Finite element investigations of bolt clamping force and friction coefficient effect on the fatigue behavior of aluminum alloy 2024–T3 in double shear lap joint;Chakherlou;Eng. Fail. Anal.,2013

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

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

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

3. Study on the Mechanism of Cumulative Deformation and Method for Suppression in Aircraft Panel Riveting;Aerospace;2024-08-16

4. Fatigue properties of riveted joints under different hole perpendicularity errors and squeeze forces;Microscopy Research and Technique;2024-02-13

5. Effect of rivet arrangement on fatigue performance of electromagnetic riveted joint with Φ10 mm diameter rivet;International Journal of Fatigue;2023-11

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