Introduction

Gennadi I. Mikhasev; Holm Altenbach

doi:10.1007/978-3-030-12761-9_1

Introduction

Gennadi I. Mikhasev^*
, Holm Altenbach

^*Corresponding author for this work

Belarusian State University
Otto von Guericke University Magdeburg

Research output: Contribution to journal › Editorial

Abstract

Laminates and sandwiches belong to lightweight structures of rather thin cross sections in comparison with the other structural dimensions. Both have a layered structure. The first one are composed of many layers (in modern structures up to 40 - 60) each of them have as usual the same thickness and properties. The second one are composed of three layers and in classical applications the outer layers are made of uniform (homogeneous) materials, while the inner layer consists either of a soft, relatively continuous material (different foams) or of a structurally complicated, inhomogeneous material (cellular fillers, corrugations). However, in multilayered structures each layer is a composite material itself. A short introduction into the modelling of composite structures is given in Chapt. 1. In Sect. 1.1 some general formulation approaches of plate and shell theories are presented. In Sect. 1.2 an introduction to composite modelling is given. Section 1.3 is devoted to modeling of laminated and sandwich plates and shells.

Original language	English
Pages (from-to)	1-28
Number of pages	28
Journal	Advanced Structured Materials
Volume	106
DOIs	https://doi.org/10.1007/978-3-030-12761-9_1
State	Published - 2019
Externally published	Yes

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abstract = "Laminates and sandwiches belong to lightweight structures of rather thin cross sections in comparison with the other structural dimensions. Both have a layered structure. The first one are composed of many layers (in modern structures up to 40 - 60) each of them have as usual the same thickness and properties. The second one are composed of three layers and in classical applications the outer layers are made of uniform (homogeneous) materials, while the inner layer consists either of a soft, relatively continuous material (different foams) or of a structurally complicated, inhomogeneous material (cellular fillers, corrugations). However, in multilayered structures each layer is a composite material itself. A short introduction into the modelling of composite structures is given in Chapt. 1. In Sect. 1.1 some general formulation approaches of plate and shell theories are presented. In Sect. 1.2 an introduction to composite modelling is given. Section 1.3 is devoted to modeling of laminated and sandwich plates and shells.",

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AB - Laminates and sandwiches belong to lightweight structures of rather thin cross sections in comparison with the other structural dimensions. Both have a layered structure. The first one are composed of many layers (in modern structures up to 40 - 60) each of them have as usual the same thickness and properties. The second one are composed of three layers and in classical applications the outer layers are made of uniform (homogeneous) materials, while the inner layer consists either of a soft, relatively continuous material (different foams) or of a structurally complicated, inhomogeneous material (cellular fillers, corrugations). However, in multilayered structures each layer is a composite material itself. A short introduction into the modelling of composite structures is given in Chapt. 1. In Sect. 1.1 some general formulation approaches of plate and shell theories are presented. In Sect. 1.2 an introduction to composite modelling is given. Section 1.3 is devoted to modeling of laminated and sandwich plates and shells.

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Introduction

Abstract

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