Theoretical and experimental investigation on interference fit in electromagnetic riveting-Reference-Cited by-同舟云学术

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Theoretical and experimental investigation on interference fit in electromagnetic riveting

Published:2019-06 Issue: Volume:156 Page:261-271
ISSN:0020-7403
Container-title:International Journal of Mechanical Sciences
language:en
Short-container-title:International Journal of Mechanical Sciences

Author:

Zhang Xu,Jiang Hao,Luo Tong,Hu Lin,Li Guangyao,Cui Junjia

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference31 articles.

1. Riveted lap joints in aircraft fuselage: design, analysis and properties;Skorupa,2012

2. An experimental study on mechanical response of single-lap bolted CFRP composite interference-fit joints;Hu;Compos Struct,2018

3. Effect of the clearance and interference-fit on failure of the pin-loaded composites;Binnur;Mater Des,2010

4. Effect of production variables on the fatigue behaviour of riveted lap joints;Skorupa;Inter J Fatigue,2010

5. The effect of interference fit size on the fatigue life of bolted joints in composite laminates;Wei;Compos Part B,2013

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1. An experimental and theoretical investigation on residual stress of 7075-T651 aluminum alloy hole under electromagnetic cold expansion;Engineering Failure Analysis;2024-11

2. Real-time modeling of the riveting process forces for aircraft panel structures;Journal of Manufacturing Processes;2024-08

3. Investigation on interference and damage behaviours of electromagnetic riveted double-sided countersunk 30CrMnSiA/CFRP joints;Composite Structures;2024-02

4. A dynamic installation method to improve the morphological characteristics of the bolt-hole contact interface in CFRP interference bolted structures;Engineering Failure Analysis;2024-02

5. Influence of bolt dynamic installation on topography characteristics and mechanical behaviors of CFRP interference-fit bolted joints;Chinese Journal of Aeronautics;2024-02

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