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008			230318s2022 sz | s |||| 0|eng d
020			_a9783030789992
024	7		_a10.1007/978-3-030-78999-2 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL900 _b2022 EB
100	1		_aAppel, Simon _eautor _0(orcid)0000-0002-2897-4072 _1https://orcid.org/0000-0002-2897-4072 _4aut _4http://id.loc.gov/vocabulary/relators/aut _9687439
245	1	0	_aSimulation of Thermoelastic Behaviour of Spacecraft Structures : _bFundamentals and Recommendations _cby Simon Appel, Jaap Wijker
250			_a1st edition 2022
264		1	_aCham _bSpringer International Publishing _c2022
300			_a1 recurso en línea (XXIV, 399 páginas) _b243 ilustraciones, 165 ilustraciones a color
336			_atexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
347			_aarchivo de texto _bPDF
490	0		_aSpringer Aerospace Technology _x1869-1749
505	0		_aThermoelastic verification -- Occurrence of thermoelastic phenomenon in Spacecraft -- Physics of thermoelastics -- Modelling for thermoelastic -- Thermal modelling for thermo-elastic analysis -- Structural modelling for thermoelastic analysis -- Transfer of thermal analysis results to the structural model -- Prescribed Average Temperature Method -- Generation of linear conductors for lumped parameter thermal models -- Estimating uncertainties in the thermoelastic analysis process -- Solutions.
520			_aThis book provides recommendations for thermal and structural modelling of spacecraft structures for predicting thermoelastic responses. It touches upon the related aspects of the finite element and thermal lumped parameter method. A mix of theoretical and practical examples supports the modelling guidelines. Starting from the system needs of instruments of spacecraft, the reader is supported with the development of the practical requirements for the joint development of the thermal and structural models. It provides points of attention and suggestions to check the quality of the models. The temperature mapping problem, typical for spacecraft thermoelastic analysis, is addressed. The principles of various temperature mapping methods are presented. The prescribed average temperature method, co-developed by the authors, is discussed in detail together with its spin-off to provide high quality conductors for thermal models. The book concludes with the discussion of the application of uncertainty assessment methods. The thermoelastic analysis chain is computationally expensive. Therefore, the 2k+1 point estimate method of Rosenblueth is presented as an alternative for the Monte Carlo Simuation method, bringing stochastic uncertainty analysis in reach for large thermoelastic problems.
988			_aSpringer_Engineering_2022
650		7	_2embne _9139696 _aVehículos espaciales
650		7	_2embne _9138250 _aElasticidad
700	1		_9673571 _aWijker, Jaap J., _d1944- _eautor
776	0	8	_iPrinted edition: _z9783030789985
776	0	8	_iPrinted edition: _z9783030790004
776	0	8	_iPrinted edition: _z9783030790011
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-78999-2 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b03/2023 _dz _eIG _zSI