000			03571nam a2200409 c 4500
942			_2lcc _cLE
988			_aSpringer_Engineering_2019
999			_c114582 _d114582 _x1
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003			ES-MaUEC
005			20230110040227.0
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008			190723s2019 gw a o |||| 0|eng d
020			_a9783030168568
024	7		_a10.1007/978-3-030-16856-8 _2doi
040			_aES-MaUEC _bspa _cES-MaUEC _dES-MaUEC
050		4	_aTL574.S7 _b2019 EB
100	1		_aChudoba, Bernd _eautor _9671593
245	1	0	_aStability and Control of Conventional and Unconventional Aerospace Vehicle Configurations : _bA Generic Approach from Subsonic to Hypersonic Speeds _cby Bernd Chudoba.
250			_a1st ed. 2019.
264		1	_aCham _bSpringer International Publishing _c2019
300			_a1 recurso en línea (XXXIV, 392 páginas)
336			_2rdacontent _aTexto _btxt
337			_2rdamedia _aelectrónico _bc
338			_2rdacarrier _arecurso electrónico _bcr
347			_atext file _bPDF
490	0		_aSpringer Aerospace Technology _x1869-1730
490	0		_aEngineering (Springer-11647)
505	0		_aIntroduction and Objectives -- Generic Aircraft Design - Knowledge Utilization -- Assessment of the Aircraft Conceptual Design Process -- Generic Characterisation of Aircraft - Parameter Reduction Process -- 'AeroMech' - Conception of a Generic Stability and Control Methodology -- AeroMech Feasibility -- Conclusions -- Appendices.
520	3		_aThis book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a 'configuration stability & control' methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
650		7	_2embne _aAviones _xEstabilidad _9138154
776	0	8	_iPrinted edition: _z9783030168551
776	0	8	_iPrinted edition: _z9783030168575
776	0	8	_iPrinted edition: _z9783030168582
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-030-16856-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
998			_aSI _cm _dz _feng _ggw _h0 _b12/2019 _ek _zSI