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

Seemann, Ralf.
2020
TL671.6
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Title
A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior / Ralf Seemann.
Author
Seemann, Ralf.
ISBN
9783662602768
3662602768
9783662602751
366260275X
Publication Details
Berlin, Germany : Springer Vieweg, ©2020.
Language
English
Description
1 online resource (210 pages)
Call Number
TL671.6
Dewey Decimal Classification
624.1/779
Summary
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.
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Access limited to authorized users.
Source of Description
Description based on print version record.
Series
Produktentwicklung und Konstruktionstechnik ; v. 16.
Available in Other Form
A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior.
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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.

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