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- W3002537021 abstract "Composite sandwich constructions are now widely used in primary aircraft airframe structures and outstand by their high bending and stability performance. These structures are typically characterized by a continuous core which extends over the entire structural bay perimeter confined by adjacent framework structural members. This paper presents a novel design approach of asymmetric sandwich structures which is based upon a tailored discretization of the core area over the bay perimeter and enables an important increase of the weight efficiency of traditional sandwich shells. The discretization pattern of the core is a result of a topographic optimization of the bending stiffness with respect to an in-plane loading. The paper describes the basic rationale of the design approach and demonstrates its technological feasibility. The mechanical behavior is predicted by standard linear and non-linear numerical tools and verified by shear tests. Furthermore, the design approach is exemplarily applied within the context of real helicopter airframe structures hence proving its functional and practical suitability." @default.
- W3002537021 created "2020-01-30" @default.
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- W3002537021 date "2020-04-01" @default.
- W3002537021 modified "2023-09-30" @default.
- W3002537021 title "Discrete tailored asymmetric sandwich structures" @default.
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- W3002537021 doi "https://doi.org/10.1016/j.compstruct.2020.111990" @default.
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