Finite element design and analysis of a bolted patch repair for composites-Reference-Cited by-同舟云学术

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Finite element design and analysis of a bolted patch repair for composites

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Shi G.¹,Poon C.¹,Xiong Y.¹

Affiliation:

1. National Research Council of Canada, Ottawa

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1489

Reference13 articles.

1. element modeling of riveted lap joints in aircraft structure, AIAA-98-2062, 1998.

2. loaded fastener hole in finite composite laminate, ASME Journal of Applied Mechanics, Vol.65, No.3, 1998.

3. pp.4395-4409, 1996. 6. Crews, Jr., J. H., Hong, C. S. and Raju, I.S.

Cited by 2 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. A Complex Potential Methodology for Bolted Repair Analysis of Composite Laminates;AIAA SCITECH 2023 Forum;2023-01-19

2. Bolted patch repair of composite panels with a cutout;Composite Structures;2002-06

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