4.4 Article

Quasi-static mechanical properties of novel generalized Resch-pattern composite foldcores

出版社

SAGE PUBLICATIONS LTD
DOI: 10.1177/0954406220940000

关键词

Foldcore sandwich structure; generalized Resch patterns; geometric design method; CFRP laminates; finite element analysis

资金

  1. National Natural Science Foundation of China [51408357]
  2. Shanghai Aerospace Science and Technology Innovation Fund

向作者/读者索取更多资源

A new geometric design method based on the generalized Resch patterns is proposed for foldcores, which allows bonding interfaces between the core and skins. A systematic numerical investigation on the mechanical properties of CFRP foldcores is performed using the finite element method, revealing relationships between mechanical properties and geometric parameters. The CFRP foldcores based on generalized Resch patterns outperform other types in terms of stability, compressive and shear stiffness, and energy absorption capacity.
A new geometric design method for foldcores based on the generalized Resch patterns that allow face-to-face bonding interfaces between the core and the skins is proposed. Based on the geometric design method, a systematic numerical investigation on the quasi-static mechanical properties of the generalized Resch-based foldcores made of carbon fiber-reinforced plastic (CFRP) woven fabrics subjected to compression and shear loads is performed using the finite element method that is validated by experiments. The relationships between the mechanical properties and various geometric parameters as well as laminate thickness of the generalized Resch-based CFRP foldcores are revealed. Additionally, the mechanical properties of the generalized Resch-based CFRP foldcore are compared to those of the standard Resch-based, Miura-based foldcore, the honeycomb core, and the aluminum counterpart. It is found that the generalized Resch-based CFRP foldcore performs more stably than the honeycomb core under compression and has higher compressive and shear stiffnesses than the standard Resch-based and Miura-based foldcores and absorbs as nearly twice energy under compression as the Miura-based foldcore does. When compared with the aluminum counterpart, the CFRP model has higher weight-specific stiffness and strength but lower energy absorption capacity under shearing. The results presented in this paper can serve as the useful guideline for the design of the generalized Resch-based composite foldcore sandwich structures for various performance goals.

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