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003			ES-MaUEC
005			20230102114149.0
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007			cr nn nnnaamaa
008			200629s2020 gw a o |||| 0|eng d
020			_a9783030429300
024	7		_a10.1007/978-3-030-42930-0 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTA357 _b2020 EB
100	1		_aWeiland, Claus _eautor _4http://id.loc.gov/vocabulary/relators/aut _1http://viaf.org/viaf/47306809 _9675577
245	1	0	_aMechanics of Flow Similarities _cby Claus Weiland
250			_aFirst edition
264		1	_aCham _bSpringer International Publishing _c2020
300			_a1 recurso en línea (XIV, 199 páginas) _b157 ilustraciones, 55 ilustraciones a color
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_aarchivo de texto _bPDF
490	0		_aEngineering (SpringerNature-11647)
490	0		_aEngineering (R0) (SpringerNature-43712)
505	0		_aIntroduction -- Dimensional Analysis - Buckingham's II Theorem -- The Fractional Analysis Method -- Method of Differential Equations -- Classification of Dimensionless Numbers - Similarity Parameters -- Dimensionless Numbers - Similarity Parameters -- The Gasdynamic Similarity -- Model Technology.
520	3		_aThe mechanics of similarity encompasses the analysis of dimensions, performed by various procedures, the gasdynamic similarity and the model technology. The analysis of dimensions delivers the dimensionless numbers by which specific physical challenges can be described with a reduced number of variables. Thereby the assessment of physical problems is facilitated. For fluid dynamics and all sorts of heat transfer the discipline of the mechanics of similarity was so important in the past, that the historical background is highlighted of all the persons who have contributed to the development of this discipline. The goal of the classical gasdynamic similarity was to find rules, which enables the aerodynamic engineer to perform transformations from existing flow fields to others, which meet geometrical and other specific flow field parameters. Most of these rules and findings do no longer play a role today, because a lot of potent experimental and theoretical/numerical methods are now available. This problem is addressed in the book. A recent investigation regarding the longitudinal aerodynamics of space vehicles has revealed, that there exist other astonishing similarities for hypersonic and supersonic flight Mach numbers. It seems, that obviously most of the longitudinal aerodynamics is independent from the geometrical configurations of the space vehicle considered, if a simple transformation is applied. A section of this book is devoted to these new findings.
988			_aSpringer_Engineering_03082020
650		7	_2embne _aMecánica de fluidos _9138336
776	0	8	_iPrinted edition: _z9783030429294
776	0	8	_iPrinted edition: _z9783030429317
776	0	8	_iPrinted edition: _z9783030429324
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-42930-0 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
942			_2lcc _cLE
998			_b08/2020 _dz _ek _zSI