Cold expansion technology of connection holes in aircraft structures: A review and prospect-Reference-Cited by-同舟云学术

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Cold expansion technology of connection holes in aircraft structures: A review and prospect

Published:2015-08 Issue:4 Volume:28 Page:961-973
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Fu Yucan,Ge Ende,Su Honghua,Xu Jiuhua,Li Renzheng

Funder

National Engineering and Research Center for Commercial Aircraft Manufacturing of China

Funding of Jiangsu Innovation Program for Graduate Education of China

Fundamental Research Funds

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference108 articles.

1. Fatigue reliability assessment of riveted lap joint of aircraft structures;Huang;Int J Fatigue,2012

2. Theory of economic life Prediction and reliability assessment of aircraft structures;Yan;Chin J Aeronaut,2011

3. Fatigue crack location and fatigue life for riveted lap joints in aircraft fuselage;Skorupa;Int J Fatigue,2014

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. Effect of detail design on fatigue performance of fastener hole;Liu;Mater Des,2010

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2. Effect of cold expansion on the fatigue life of multi-hole 7075-T6 aluminum alloy structures under the pre-corrosion condition;Engineering Failure Analysis;2024-11

3. Effects of lubrication conditions on cold expansion fatigue strengthening performances of titanium alloy open hole structures;Ocean Engineering;2024-10

4. 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

5. Investigation of Residual Stress Distribution and Fatigue of 7050-T7451 Alloy Hole Components with Laser Shock and Ultrasonic Extrusion;Metals;2024-05-19

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