000 03337nam a22005415i 4500
001 978-3-662-60276-8
003 DE-He213
005 20220801214430.0
007 cr nn 008mamaa
008 190829s2020 gw | s |||| 0|eng d
020 _a9783662602768
_9978-3-662-60276-8
024 7 _a10.1007/978-3-662-60276-8
_2doi
050 4 _aTJ1-1570
072 7 _aTGB
_2bicssc
072 7 _aTEC009070
_2bisacsh
072 7 _aTGB
_2thema
082 0 4 _a621
_223
100 1 _aSeemann, Ralf.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_938327
245 1 2 _aA Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
_h[electronic resource] /
_cby Ralf Seemann.
250 _a1st ed. 2020.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer Vieweg,
_c2020.
300 _aXVII, 201 p. 143 illus., 95 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aProduktentwicklung und Konstruktionstechnik,
_x2662-7485 ;
_v16
505 0 _aIntroduction -- 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 _aVirtual 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. .
650 0 _aMechanical engineering.
_95856
650 0 _aMaterials.
_97549
650 0 _aBuilding materials.
_931878
650 1 4 _aMechanical Engineering.
_95856
650 2 4 _aMaterials Engineering.
_932311
650 2 4 _aStructural Materials.
_931883
710 2 _aSpringerLink (Online service)
_938328
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783662602751
776 0 8 _iPrinted edition:
_z9783662602775
776 0 8 _iPrinted edition:
_z9783662602782
830 0 _aProduktentwicklung und Konstruktionstechnik,
_x2662-7485 ;
_v16
_938329
856 4 0 _uhttps://doi.org/10.1007/978-3-662-60276-8
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c76340
_d76340