Testing and simulation of a composite-aluminium wingbox subcomponent subjected to thermal loading
Author:
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference37 articles.
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3. A detailed finite element investigation of composite bolted joints with countersunk fasteners;Stocchi;Composites A,2013
4. Development of a connector element for multi-material bolted-joint under tensile loading;Omran;Mech Adv Mater Struct,2018
5. Effects of temperature on the bearing strength of CF/epoxy pinned joints;Hirano;J Compos Mater,2007
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. Influence of unidirectional composite failure envelope shape on predicting compressive failure of a laminate with a filled-hole;Composites Part B: Engineering;2024-05
2. Experimental and virtual testing of a composite-aluminium aircraft wingbox under thermal loading;Aerospace Science and Technology;2023-07
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