000			02964cam a2200445 i 4500
001			13205639
003			OSt
005			20190522143812.0
006			m d
007			cr n
008			170224s2017 flua sb 001 0 eng d
020			_a9781466595163
024			_c16955.00
035			_a(WaSeSS)ssj0001958022
040			_aDLC _beng _erda _cAUI _dWaSeSS
042			_apcc
050		4	_aTL709 _b.E42 2017
082	0	0	_a629.134/353 _223
100	1		_aEl-Sayed, Ahmed F., _eauthor. _93594
210	1	0	_aAircraft propulsion and gas turbine engines /
245	1	0	_aAircraft propulsion and gas turbine engines / _cAhmed F. El-Sayed.
250			_a2nd.ed
260			_aBoca Raton _bCRC _c2017.
300			_axxvii;1447 p.
504			_aIncludes bibliographical references and index.
505	0		_aHistory and classifications of aero-engine -- Performance parameters of jet engines -- Pulsejet and ramjet engines -- Turbojet engine -- Turbofan engines -- Shaft engines -- High speed supersonic and hypersonic engines -- Industrial gas turbines -- Power plant installation and intakes -- Combustion systems -- Exhaust system -- Centrifugal compressors -- Axial flow compressors and fans -- Axial turbines -- Radial inflow turbines -- Module matching -- Selected topics -- Introduction to rocketry -- Rocket engines.
506			_aLicense restrictions may limit access.
520			_a"AIRCRAFT PROPULSION and GAS TURBINE ENGINES, Second Edition, will be a significantly updated and expanded survey of today's aeronautical and aerospace propulsion. The book will be divided into three parts rather than two as in its 1st edition. The first two parts are devoted to air breathing engines, while the third part will handle non-air breathing or rocket engines. The first part investigates the performance of air/land gas turbines, while the second part deals with the description, analysis and design of gas turbine modules. This edition will exhibit major and minor changes compared with 1st edition. Major changes include the adding of three new topics; namely, piston engines together with integrated propeller coverage; pumps; and rocket propulsion. Rocket propulsion has been added, to serve courses that include aerospace topics as well as aircraft. A complete Solutions Manual and Exam Supplement will be available for qualified adopting instructors"--Provided by publisher.
650		0	_aAirplanes _xTurbojet engines. _93595
650		0	_aAircraft gas-turbines. _93596
773		0	_tENGnetBASE
773		0	_tMECHANICALENGINEERING netBASE
856	4	0	_uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio13205639.001 _zFull text available from ENGnetBASE
856	4	0	_uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio13205639.002 _zFull text available from MECHANICALENGINEERING netBASE
910			_aLibrary of Congress record
942			_2ddc _cBK
990			_aTL
999			_c12613 _d12613