000			03313nam a22003615i 4500
001			84398
003			ES-MaUEC
005			20230207040421.0
007			cr nn 008mamaa
008			160525s2016 xxk| s |||| 0|eng d
020			_a9781447167969
040			_aES-MaUEC
050		4	_aTL709 _b.E473 2016
100	1		_aEl-Sayed, Ahmed F. _996534 _0Local
245	1	0	_aFundamentals of Aircraft and Rocket Propulsion _cby Ahmed F El-Sayed
260			_aLondon _bSpringer London _c2016
300			_a1 recurso en línea (XXI, 1010 páginas) _b571 ilustraciones, 242 ilustraciones en color
336			_aTexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
505	0		_aClassifications of Aircrafts and Propulsion Systems -- Basic Laws for Fluids; Performance Parameters of Jet Engines -- Piston Engines and Propellers -- Pulsejet, Ramjet, and Scramjet Engines -- Turbojet, Turbofan, and Turboramjet Engines -- Shaft Engines -- Stationary Modules of Airbreathing Engines -- Rotating Modules of Airbreathing Engines -- Special Topics -- Rockets; Rocket Engines.
520	3		_aThis book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained. Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of: thermodynamic cycles of shaft engines (piston, turboprop, turboshaft and propfan); jet engines (pulsejet, pulse detonation engine, ramjet, scramjet, turbojet and turbofan); chemical and non-chemical rocket engines; conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and conceptual design of different modules of aero-engines in their design and off-design state. Aimed at graduate and final-year undergraduate students, this textbook provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features of all the engines detailed, and particular consideration of special aircraft such as unmanned aerial and short/vertical takeoff and landing aircraft. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors.
710	2		_aSpringerLink (Online service) _0Local _9106996
942			_2lcc _cLE
988			_aEBOOK, asignarmaterias , EBSPRINGER,
650		7	_aLíquidos _9140721 _0comprobar BNE19900988757 _2embne
650		7	_9139804 _aTermodinámica _0comprobar BNE19900977115 _2embne
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://link.springer.com/book/10.1007/978-1-4471-6796-9 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
901			_ai9781447167969
907			_a.b12936765 _b10-10-17 _c21-11-16
998			_am _a_alco _a_vill _b - - _cm _dz _e- _feng _gxxk _h0
945			_aTL709 .E473 2016 EB _g1 _ieBOOK _j0 _lmae _o- _pEUR0.00 _q- _r- _sb _t15 _u0 _v0 _w0 _x0 _y.i11581682 _z06-04-17
999			_c84398 _d84398 _x1