000			03461nam a22003615i 4500
001			289000
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007			cr nn 008mamaa
008			150903s2012 xxu| o |||| 0|eng d
020			_a9781461436096 _99781461436096
024	7		_a10.1007/9781461436096 _2doi
035			_avtls000341053
039		9	_a201509030832 _bVLOAD _c201405050223 _dVLOAD _y201402061050 _zstaff
040			_aMX-SnUAN _bspa _cMX-SnUAN _erda
050		4	_aQA319-329.9
100	1		_aBalakrishnan, AV. _eautor _9319019
245	1	0	_aAeroelasticity : _bThe Continuum Theory / _cby AV Balakrishnan.
264		1	_aNew York, NY : _bSpringer New York : _bImprint: Springer, _c2012.
300			_axii, 399 páginas 12 ilustraciones _brecurso en línea.
336			_atexto _btxt _2rdacontent
337			_acomputadora _bc _2rdamedia
338			_arecurso en línea _bcr _2rdacarrier
347			_aarchivo de texto _bPDF _2rda
500			_aSpringer eBooks
505	0		_aIntroduction -- Dynamics of Wing Structure -- The Air Flow Model -- The Steady State HStatic L Solution of the Aeroelastic Equation -- Linear Aeroelasticity Theory The Possio Integral Equation -- NonLinear Aeroelasticity Theory in 2 D Aerodynamics Flutter As LCO -- Viscous Flow Theory.-Optimal Control Theory : Flutter Suppression -- Aeroelastic Gust Response.-.
520			_aThe author's approach is one of continuum models of the aerodynamic flow interacting with a flexible structure whose behavior is governed by partial differential equations. Both linear and nonlinear models are considered although much of the book is concerned with the former while keeping the latter clearly in view. A complete chapter is also devoted to nonlinear theory. The author has provided new insights into the classical inviscid aerodynamics and raises novel and interesting questions on fundamental issues that have too often been neglected or forgotten in the development of the early history of the subject. The author contrasts his approach with discrete models for the unsteady aerodynamic flow and the finite element model for the structure. Much of the aeroelasticity has been developed with applications formerly in mind because of its enormous consequences for the safety of aircraft. Aeroelastic instabilities such as divergence and flutter and aeroelastic responses to gusts can pose a significant hazard to the aircraft and impact its performance. Yet, it is now recognized that there are many other physical phenomena that have similar characteristics ranging from flows around flexible tall buildings and long span bridges, alternate energy sources such as electric power generation by smart structures to flows internal to the human body.  From the foreword:  "For the theorist and applied mathematician who wishes an introduction to this fascinating subject as well as for the experienced aeroelastician who is open to new challenges and a fresh viewpoint, this book and its author have much to offer the reader." Earl Dowell, Duke University, USA
590			_aPara consulta fuera de la UANL se requiere clave de acceso remoto.
710	2		_aSpringerLink (Servicio en línea) _9299170
776	0	8	_iEdición impresa: _z9781461436089
856	4	0	_uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-1-4614-3609-6 _zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
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999			_c289000 _d289000