000			03195nam a22003255i 4500
001			103387
003			DE-He213
005			20230102113128.0
007			cr nn 008mamaa
008			150106s2015 gw | s |||| 0|eng d
020			_a9783319143736
024	7		_a10.1007/978-3-319-14373-6 _2doi
040			_aES-MaUEC _bspa
050		4	_aTL574.A45 _bH577 2015 EB
100	1		_aHirschel, Ernst Heinrich _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _1http://viaf.org/viaf/54435742/
245	1	0	_aBasics of Aerothermodynamics _bSecond, Revised Edition _cby Ernst Heinrich Hirschel.
250			_a2nd edition
264		1	_aCham _bSpringer International Publishing _c2015
300			_a1 recurso en línea (XVIII, 446 páginas 159 ilustraciones, 11 ilustraciones a color)
505	0		_aIntroduction -- The Flight Environment -- Thermal Radiation Cooling of External Vehicle Surfaces -- Transport of Momentum, Energy and Mass -- Real-Gas Aerothermodynamic Phenomena -- Inviscid Aerothermodynamic Phenomena -- Attached High-Speed Viscous Flow -- Laminar-Turbulent Transition and Turbulence in High-Speed Viscous Flow -- Strong Interaction Phenomena -- Viscous Thermal Surface Effects: Examples -- Solution Guide and Solutions of the Problems.
520	3		_aThis successful book gives an introduction to the basics of aerothermodynamics, as applied in particular to winged re-entry vehicles and airbreathing hypersonic cruise and acceleration vehicles. The book gives a review of the issues of transport of momentum, energy and mass, real-gas effects as well as inviscid and viscous flow phenomena. In this second, revised edition the chapters with the classical topics of aerothermodynamics more or less were left untouched. The access to some single topics of practical interest was improved. Auxiliary chapters were put into an appendix. The recent successful flights of the X-43A and the X-51A indicate that the dawn of sustained airbreathing hypersonic flight now has arrived. This proves that the original approach of the book to put emphasis on viscous effects and the aerothermodynamics of radiation-cooled vehicle surfaces was timely. This second, revised edition even more accentuates these topics. A new, additional chapter treats examples of viscous thermal surface effects. Partly only very recently obtained experimental and numerical results show the complexity of such phenomena (dependence of boundary-layer stability, skin friction, boundary-layer thicknesses, and  separation on the thermal state of the surface) and their importance for airbreathing hypersonic flight vehicles, but also for any other kind of hypersonic vehicle.
650		7	_aAerodinámica _9138151 _2embne
650		7	_9139804 _aTermodinámica _2embne
776	0	8	_iEdición impresa: _z9783319143743
776	0	8	_iEdición impresa: _z9783319143729
776	0	8	_iEdición impresa: _z9783319330402
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-3-319-14373-6 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
490	0		_aEngineering (Springer-11647)
998			_b03/2019 _dz _ek _feng _ggw _h0
999			_c103387 _d103387 _x1