000			02998nam a22004095i 4500
988			_aSpringer_Engineering_2020
999			_c116858 _d116858 _x1
001			116858
003			ES-MaUEC
005			20230110040248.0
006			a||||fo|||| 00| 0
007			cr nn nnnaamaa
008			190829s2020 gw | s |||| 0|eng d
020			_a9783662602768
024	7		_a10.1007/978-3-662-60276-8 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL671.6 _b2020 EB
100	1		_aSeemann, Ralf _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9672031
245	1	2	_aA Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior _cby Ralf Seemann.
250			_a1st ed. 2020.
264		1	_aBerlin, Heidelberg _bSpringer Berlin Heidelberg Vieweg _c2020.
300			_a1 recurso en línea (XVII, 201 páginas) _b143 ilustraciones, 95 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aProduktentwicklung und Konstruktionstechnik ; _v16
490	0		_aEngineering (Springer-11647)
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		7	_2embne _9138154 _aAviones _xDiseño y construcción
776	0	8	_iPrinted edition: _z9783662602751
776	0	8	_iPrinted edition: _z9783662602775
776	0	8	_iPrinted edition: _z9783662602782
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-662-60276-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_aSI _cm _dz _feng _ggw _h0 _b01/2020 _eIG _zSI