|
MECHANICS
Design of multi-wall composite shells
A. Sh. Kusyakov Perm State National Research
University, Perm, Russian Federation
Abstract:
This paper investigates a problem of optimal design of a multi-walled cylindrical shell under axial compressive loads. The multi-walled shell consists of two load-carrying layers connected by a set of composite walls. The main structural element of the load-carrying layer is a monolayer comprising parallel-laid fibers that are interconnected by a polymer binder — a matrix. The wall represents a unidirectional composite made from the same material as the load-carrying layers.
Both strength and stability constraints are taken into account during mathematical modeling. The critical load corresponding to a general form of buckling is determined by a classical formula for an orthotropic shell with “reduced” stiffnesses. The critical load corresponding to a local form of buckling is calculated using the well-known formula for a smooth orthotropic plate. The target function is the mass of the structure.
The solution to the problem of optimal design of a multi-walled structure is proved to be unique. The conditions ensuring the existence of the problem solution are formulated. The example of evaluating the efficiency of reinforcing elements in a shell structure is given. The presented research results can find application in design problems for modern composite structures in rocket and space industry.
Keywords:
multi-walled shell, composite, stability, strength, design.
Received: 26.11.2020
Citation:
A. Sh. Kusyakov, “Design of multi-wall composite shells”, Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2021, no. 74, 103–112
Linking options:
https://www.mathnet.ru/eng/vtgu892 https://www.mathnet.ru/eng/vtgu/y2021/i74/p103
|
Statistics & downloads: |
Abstract page: | 60 | Full-text PDF : | 32 | References: | 11 |
|