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A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft InteriorMechanical characterization on constituent level

A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior: Mechanical... [In composite sandwich construction, three main constituents are of primary interest on constituent level. These include core, face sheets and adhesives. In case plastics are used for load introduction elements, such as inserts, these materials may be also of interest on constituent level. Additionally, used metallic elements are usually the strongest component in sandwich construction. Therefore, they do not require a detailed analysis. In addition, elastic material properties are readily available for common metals. This chapter describes the mechanical characterization of the relevant constituents in the framework of the present thesis.] http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png

A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft InteriorMechanical characterization on constituent level

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Publisher
Springer Berlin Heidelberg
Copyright
© Springer-Verlag GmbH Germany, part of Springer Nature 2020
ISBN
978-3-662-60275-1
Pages
35 –72
DOI
10.1007/978-3-662-60276-8_4
Publisher site
See Chapter on Publisher Site

Abstract

[In composite sandwich construction, three main constituents are of primary interest on constituent level. These include core, face sheets and adhesives. In case plastics are used for load introduction elements, such as inserts, these materials may be also of interest on constituent level. Additionally, used metallic elements are usually the strongest component in sandwich construction. Therefore, they do not require a detailed analysis. In addition, elastic material properties are readily available for common metals. This chapter describes the mechanical characterization of the relevant constituents in the framework of the present thesis.]

Published: Aug 30, 2019

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