期刊
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES
卷 28, 期 8, 页码 791-811出版社
TAYLOR & FRANCIS INC
DOI: 10.1080/15376494.2019.1600768
关键词
Adhesively bonded joints; design; modeling; finite element analysis; composite materials; sandwich; honeycomb core
类别
资金
- Space Technology Mission Directorate Composite Technologies (NASA)
- Aeronautics Research Directorate Transformational Tools and Technologies Project
- European Union [642121]
This study compared the predictive performance of five design models on local stress fields, and found that lower fidelity models have advantages in saving computational and user time.
Despite the proliferation of high fidelity finite-element (FE) models, lower fidelity models remain commonly used in adhesively bonded joint design. These design models can save both computational and user time due to their simplicity and ease of use. This study presents a detailed assessment of local stress fields predicted by five design models: A4EI, HyperSizer, Joint Element Designer, Carrera Unified Formulation, and a Continuum Solid Shell FE model. All models were compared with a high fidelity, dense mesh FE model. Six double lap joint cases with different combinations of features like different adhereds, a core, and tapers were compared.
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