Mechanics of Solids (about journal) Mechanics of Solids
A Journal of Russian Academy of Sciences
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IssuesArchive of Issues2025-2pp.1368-1386

Archive of Issues

Total articles in the database: 13205
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Xu Zhang, Shuaiqiang Zhang, Yan Fang, and Wei Li, "Study on the Bending Properties and Failure Behaviors of Scarf-Repaired Honeycomb Sandwich Structures Considering the Optimal Design of an Additional Layer," Mech. Solids. 60 (2), 1368-1386 (2025)
Year 2025 Volume 60 Number 2 Pages 1368-1386
DOI 10.1134/S002565442460692X
Title Study on the Bending Properties and Failure Behaviors of Scarf-Repaired Honeycomb Sandwich Structures Considering the Optimal Design of an Additional Layer
Author(s) Xu Zhang (School of Aeronautics and Astronautics, Tiangong University, Tianjin, 300387 China, zhangxu@tiangong.edu.cn)
Shuaiqiang Zhang (School of Mechanical Engineering, Tiangong University, Tianjin, 300387 China)
Yan Fang (School of Mechanical Engineering, Tiangong University, Tianjin, 300387 China)
Wei Li (School of Energy and Safety Engineering, Tianjin Chengjian University, Tianjin, 300384 China)
Abstract The stress concentration occurs at the junction of the patch and original structure when the scarf-repaired honeycomb sandwich structure is subjected to the secondary impact, thus causing the local delamination and debonding in Carbon Fiber Reinforced Polymer (CFRP) panels. The introduction of an additional layer improves the strength and stiffness of scarf-repaired structures, but poor surface smoothness and larger uneven stress distribution occur after the dimensions of the additional layer increase to a certain extent. Hence, the optimal design of an additional layer is considered in the scarf-repaired structure to improve the load-bearing performance. The finite element models of scarfrepaired structures with and without an additional layer are established based on the 3D Hashin failure criterion, and the bending performance analysis is performed to obtain the maximum bearing load. An optimization model with the side length, thickness, and carbon fiber ply angle of the additional layer as design variables and the maximum bearing load as the design objective is built, and then is solved by the Response Surface Method (RSM). Three-point bending tests are conducted on the scarf-repaired carbon fiber composite-aramid paper honeycomb sandwich structures with and without an optimized additional layer. The results indicate that the optimized additional layer has made the load-bearing performance and deformation capacity of the scarf-repaired honeycomb sandwich structure significantly improve, that is, has effectively alleviate the stress concentration in the connection area between the patch and original structure.
Keywords honeycomb sandwich structure, additional layer optimization, scarf repair
Received 09 December 2024Revised 20 March 2025Accepted 25 March 2025
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