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

Ralf Seemann

ISBN 10: 366260275X / ISBN 13: 9783662602751

Published by Springer Fachmedien Wiesbaden, Weisbaden, 2019

About this Item

Hardcover. 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. Virtual test methods can contribute to reducing the great effort for physical tests in the development of lightweight products. Building on a multitude of physical tests on sandwich materials and joints, adequate sub-models are developed, validated and synthesized to top-level models. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.

Seller Inventory # 9783662602751

Bibliographic Details

• Title: A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior (Hardcover)
• Publisher: Springer Fachmedien Wiesbaden, Weisbaden
• Publication Date: 2019
• Language: English
• ISBN 10: 366260275X
• ISBN 13: 9783662602751
• Binding: Hardcover
• Condition: new

About this title

Synopsis

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.

About 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.