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A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior/ by Ralf Seemann.
作者:	Seemann, Ralf.
面頁冊數:	XVII, 201 p. 143 illus., 95 illus. in color.online resource. :
Contained By:	Springer Nature eBook
標題:	Structural Materials. -
電子資源:	https://doi.org/10.1007/978-3-662-60276-8
ISBN:	9783662602768

A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
Seemann, Ralf.

A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior[electronic resource] /by Ralf Seemann. - 1st ed. 2020. - XVII, 201 p. 143 illus., 95 illus. in color.online resource. - Produktentwicklung und Konstruktionstechnik,162629-2157 ;. - Produktentwicklung und Konstruktionstechnik,15.

Introduction -- State of the art -- Overall concept of mechanical characterization -- Mechanical characterization on constituent level -- Mechanical characterization on structural element level -- Mechanical characterization on sub-component level -- Virtual testing approach for sandwich panel joints -- Development of novel sandwich panel joints -- Summary and outlook -- Literature -- Appendix A – Constituent level -- Appendix B – Structural element level -- Appendix C – Sub-component level.

Virtual test methods can contribute to reducing the great effort for physical tests in the development of lightweight products. The present work describes an approach for virtual testing of sandwich panel joints based on the Building Block Approach and the Finite Elements Method. Building on a multitude of physical tests on sandwich materials and joints, adequate sub-models are developed, validated and synthesized to top-level models. The developed approach is eventually applied for the development of a novel sandwich panel joint. The Author Ralf Seemann studied mechanical Engineering at TU Hamburg (TUHH) and at National University of Singapore. From 2011-2016 he worked as research engineer at the Institut of Product Development and Mechanical Engneering Design at TUHH. Since 2017 he works as stress & weight engineer at Diehl Aviation. .

ISBN: 9783662602768

Standard No.: 10.1007/978-3-662-60276-8doiSubjects--Topical Terms:

677176
Structural Materials.

LC Class. No.: TJ1-1570

Dewey Class. No.: 621

A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
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