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飞机内部蜂窝夹芯板节点虚拟试验方法-A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interio

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上传于 2020-03-06 0次下载 921次围观
文件编号:11594
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标题(title):A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
飞机内部蜂窝夹芯板节点虚拟试验方法
作者(author):Ralf Seemann
出版社(publisher):Springer Berlin Heidelberg;Springer Vieweg
大小(size):20 MB (20950089 bytes)
格式(extension):pdf
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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.

Table of contents :
Front Matter ....Pages I-XVII
Introduction (Ralf Seemann)....Pages 1-3
State of the art (Ralf Seemann)....Pages 5-32
Overall concept of mechanical characterization (Ralf Seemann)....Pages 33-34
Mechanical characterization on constituent level (Ralf Seemann)....Pages 35-72
Mechanical characterization on structural element level (Ralf Seemann)....Pages 73-93
Mechanical characterization on sub-component level (Ralf Seemann)....Pages 95-103
Virtual testing approach for sandwich panel joints (Ralf Seemann)....Pages 105-153
Development of novel sandwich panel joints (Ralf Seemann)....Pages 155-161
Summary and outlook (Ralf Seemann)....Pages 163-164
Back Matter ....Pages 165-201
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