Observations of non-linear stress effects on crack growth in interference fit fasteners-Reference-Cited by-同舟云学术

Observations of non-linear stress effects on crack growth in interference fit fasteners

Published:2023-02 Issue: Volume:167 Page:107319
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Carroll Jordan^ORCID,Khatibi Akbar A.,Robertson Leigh,Barter Simon

Funder

RMIT University

State Government of Victoria

Defence Science and Technology Group

Defence Science Institute

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference52 articles.

1. Wanhill R, Barter S. and Molent L. Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components. Dordrecht: Springer Netherlands : Imprint: Springer, 2019.

2. Cook R. “The United Kingdom Contribution to the AGARD 'Fatigue-Rated Fastener Systems' Programme,” Royal Aerospace Establishment Farnborough (United Kingdom), 1989.

3. Cold expansion technology of connection holes in aircraft structures: A review and prospect;Fu;Chinese Journal of Aeronautics,2015

4. Stresses in a Uniaxially Loaded Sheet Containing an Interference-Fit Bolt; An Elastic Analysis;Crews,1972

5. Korsunsky AM. “Plastic Yielding of Cylinders”. In: A Teaching Essay on Residual Stresses and Eigenstrains, 2017. pp. 53-65.

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