Fatigue and failure mechanism in carbon fiber reinforced plastics/aluminum alloy single lap joint produced by electromagnetic riveting technique-Reference-Cited by-同舟云学术

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Fatigue and failure mechanism in carbon fiber reinforced plastics/aluminum alloy single lap joint produced by electromagnetic riveting technique

Published:2017-11 Issue: Volume:152 Page:1-10
ISSN:0266-3538
Container-title:Composites Science and Technology
language:en
Short-container-title:Composites Science and Technology

Author:

Jiang Hao,Li Guangyao,Zhang Xu,Cui Junjia

Funder

National Natural Science Foundation of China

State Key Program of National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference23 articles.

1. Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures;Chowdhury;Compos. Struct.,2015

2. Carbon nanotube-based health monitoring of mechanically fastened composite joints;Thostenson;Compos. Sci. Technol.,2008

3. Mechanics of mechanically fastened joints in polymer-matrix composite structures-A review;Thoppul;Compos. Sci. Technol.,2009

4. Interference-fit riveting technique in fiber composite laminates;Cao;Aerosp. Sci. Technol.,2006

5. Electromagnetic forming-A review;Psyk;J. Mater. Process. Technol.,2011

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3. Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints;Journal of Aircraft;2024-06-25

4. Surface-conformed approach for mechanical property analysis using ultrasonic welding of dissimilar metals;The International Journal of Advanced Manufacturing Technology;2024-04-10

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