Analysis of Cracks at Attachment Lugs
Author:
Affiliation:
1. Lockheed-Georgia Company, Marietta, Ga.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57558
Reference22 articles.
Cited by 24 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. Study on Non-linear Contact Stress and Prognosis Analysis of Lug Joints With Misfits;Journal of Aerospace Sciences and Technologies;2023-08-01
2. Modelling considerations for stress intensity factor solutions at pin‐loaded holes;Fatigue & Fracture of Engineering Materials & Structures;2020-05
3. Stress-Intensity Factor Solutions for Tapered Lugs with Oblique Pin Loads;ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing;2019-07-03
4. Fatigue Life Benefits of Cold Worked Holes in Fastener Joints;Procedia Structural Integrity;2019
5. Novel weight functions and stress intensity factors for quarterelliptical cracks in lug attachments;Frattura ed Integrità Strutturale;2018-12-01
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