000			03620nam a22004335i 4500
001			978-3-540-89974-7
003			DE-He213
005			20201213203814.0
007			cr nn 008mamaa
008			100301s2009 gw | s |||| 0|eng d
020			_a9783540899747 _9978-3-540-89974-7
024	7		_a10.1007/978-3-540-89974-7 _2doi
050		4	_aTL1-483
072		7	_aTRC _2bicssc
072		7	_aTRCS _2bicssc
072		7	_aTEC009090 _2bisacsh
082	0	4	_a629.2 _223
100	1		_aHirschel, Ernst Heinrich. _eauthor.
245	1	0	_aSelected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles _h[electronic resource] / _cby Ernst Heinrich Hirschel, Claus Weiland.
264		1	_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg, _c2009.
300			_bonline resource.
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
347			_atext file _bPDF _2rda
505	0		_aShort Introduction to Flight Trajectories for Aerothermodynamicists -- Aerothermodynamic Design Problems of Winged Re-Entry Vehicles -- Aerothermodynamic Design Problems of Winged Airbreathing Vehicles -- Aerothermodynamic Design Problems of Non-Winged Re-Entry Vehicles -- Stabilization, Trim, and Control Devices -- Forces, Moments, Center-of-Pressure, Trim, and Stability in General Formulation -- Multidisciplinary Design Aspects -- The Thermal State of a Hypersonic Vehicle Surface -- The ?eff Approach and Approximate Relations for the Determination of Aerothermodynamic Parameters -- Solution Guide and Solutions of the Problems.
520			_aThis volume addresses selected aerothermodynamic design problems for three vehicle classes: winged reentry, non-winged reentry, and airbreathing hypersonic flight vehicles. Following an introductory chapter, the book presents the basics of flight trajectory mechanics, giving the aerothermodynamicist an understanding of the principal issues relevant to the field. In the following chapters, specific aerothermodynamic phenomena are discussed for the three vehicle classes, major simulation problems are singled out, and particular trends are examined. Available coefficients of longitudinal motion are presented for a variety of shapes of operational and studied vehicles, and aerothermodynamic issues of stabilization, trim, and control devices are treated. A full chapter is devoted to describing equations for aerodynamic forces, moments, center of pressure, trim, and stability. Another chapter focuses on multidisciplinary design aspects, presenting the mathematical models and the coupling procedures in detail. Other chapters address the thermal state of a vehicle surface, thermal loads, and thermal surface effects, which are among the major topics of hypersonic vehicle design. The governing equations for flow in thermo-chemical non-equilibrium are presented, along with properties of the earth’s atmosphere. Finally, constants and dimensions, symbol definitions, a glossary, acronyms, and a solution guide to problems are provided. This book will be a great boon to graduate students, doctoral students, design and development engineers, and technical managers alike.
650		0	_aEngineering.
650	1	4	_aEngineering.
650	2	4	_aAutomotive Engineering.
650	2	4	_aComputational Intelligence.
700	1		_aWeiland, Claus. _eauthor.
710	2		_aSpringerLink (Online service)
773	0		_tSpringer eBooks
776	0	8	_iPrinted edition: _z9783540899730
856	4	0	_uhttp://dx.doi.org/10.1007/978-3-540-89974-7
912			_aZDB-2-ENG
950			_aEngineering (Springer-11647)
999			_c22948 _d22948