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