Evaluation of approaches for determining design allowables for bolted joints in laminated composites-Reference-Cited by-同舟云学术

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Evaluation of approaches for determining design allowables for bolted joints in laminated composites

Published:1998-02 Issue:2 Volume:41 Page:167-176
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Wang J.,Banbury A.,Kelly D.W.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference20 articles.

1. Federal Aviation Regulations;Airworthiness Standards,1991

2. Polymer Matrix Composites,1994

3. Metallic Materials and Elements for Aerospace Vehicle Structures,1983

4. Generation of design allowables;Tohlen,1986

5. Composite Airframe Structures;Niu,1992

Cited by 15 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. Comparative experimental investigation of design allowable of composite materials based on k-sample Anderson–Darling test;Journal of Reinforced Plastics and Composites;2023-09-11

2. Evaluation on the interval values of tolerance fit for the composite bolted joint;Composite Structures;2018-12

3. Design, analysis, and durability of composite repairs;Repair of Polymer Composites;2018

4. References;Handbook of Structural Life Assessment;2017-04-07

5. Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures;Composites Part B: Engineering;2016-09

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