A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior (Record no. 76340)

000 -LEADER
fixed length control field 03337nam a22005415i 4500
001 - CONTROL NUMBER
control field 978-3-662-60276-8
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801214430.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 190829s2020 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783662602768
-- 978-3-662-60276-8
082 04 - CLASSIFICATION NUMBER
Call Number 621
100 1# - AUTHOR NAME
Author Seemann, Ralf.
245 12 - TITLE STATEMENT
Title A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2020.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XVII, 201 p. 143 illus., 95 illus. in color.
490 1# - SERIES STATEMENT
Series statement Produktentwicklung und Konstruktionstechnik,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 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.
520 ## - SUMMARY, ETC.
Summary, etc 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. .
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-662-60276-8
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg :
-- Imprint: Springer Vieweg,
-- 2020.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mechanical engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Materials.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Building materials.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mechanical Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Materials Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Structural Materials.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2662-7485 ;
912 ## -
-- ZDB-2-ENG
912 ## -
-- ZDB-2-SXE

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