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008			210831s2022 sz | s |||| 0|eng d
020			_a9783030789992
024	7		_a10.1007/978-3-030-78999-2 _2doi
040			_aTR-AnTOB _beng _cTR-AnTOB _erda
041			_aeng
050		4	_aTL900
072		7	_aTRP _2bicssc
072		7	_aTTDS _2bicssc
072		7	_aTEC002000 _2bisacsh
072		7	_aTRP _2thema
072		7	_aTTDS _2thema
090			_aTL900EBK
100	1		_aAppel, Simon. _eauthor. _0(orcid)0000-0002-2897-4072 _4aut _4http://id.loc.gov/vocabulary/relators/aut
245	1	0	_aSimulation of Thermoelastic Behaviour of Spacecraft Structures _h[electronic resource] : _bFundamentals and Recommendations / _cby Simon Appel, Jaap Wijker.
250			_a1st ed. 2022.
264		1	_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2022.
300			_a1 online resource
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	1		_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.
650		0	_aAerospace engineering.
650		0	_aAstronautics.
650		0	_aThermodynamics.
650		0	_aHeat engineering.
650		0	_aHeat transfer.
650		0	_aMass transfer.
650		0	_aMechanics, Applied.
650		0	_aSolids.
650		0	_aOuter space _xExploration.
650	1	4	_aAerospace Technology and Astronautics.
650	2	4	_aEngineering Thermodynamics, Heat and Mass Transfer.
650	2	4	_aSolid Mechanics.
650	2	4	_aSpace Exploration and Astronautics.
653		0	_aSpace vehicles -- Thermodynamics
653		0	_aThermoelasticity
700	1		_aWijker, Jaap. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut
710	2		_aSpringerLink (Online service)
830		0	_aSpringer Aerospace Technology, _x1869-1749
856	4	0	_uhttps://doi.org/10.1007/978-3-030-78999-2 _3Springer eBooks _zOnline access link to the resource
942			_2lcc _cEBK