Damage tolerance assessment of aircraft attachment lugs-Reference-Cited by-同舟云学术

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Damage tolerance assessment of aircraft attachment lugs

Published:1986-01 Issue:6 Volume:23 Page:1067-1084
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Brussat T.R.,Kathiresan K.,Rudd J.L.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference19 articles.

1. Damage tolerance design requirements,1973

2. Analysis of cracks at attachment lugs;Hsu;J. Aircraft,1981

3. Analysis of cracks at an attachment lug having an interference-fit bushing;Hsu,1983

4. Crack growth behavior in attachment lugs with interference-fit bushings;Kathiresan,1984

Cited by 14 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. Residual Fatigue Life Analysis of Aircraft Structural Elements;2023 New Trends in Aviation Development (NTAD);2023-11-23

2. Damage Tolerance Evaluation of Wing Bottom Skin Panel of an Aircraft;Journal of Aerospace Sciences and Technologies;2023-08-11

3. A study on prognostic analysis of attachment lugs under off-axis loading;International Journal of Structural Integrity;2019-12-02

4. SHM—Prognostic Analysis of Tapered Attachment Lugs Under Fatigue Loading;Advances in Structural Integrity;2017-12-27

5. Prognostic analysis of fastener joints in straight attachment lugs;International Journal of Structural Integrity;2017-06-12

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