Elements of Gas Turbine Propulsion, Volume 1
This new text is designed to provide an introduction to the fundamentals of gas turbine engines and jet propulsion for aerospace or mechanical engineers. The book contains sufficient material for two sequential courses in propulsion (advanced fluid dynamics); an introductory course in jet propulsion; and a gas turbine engine components course. The text is divided into four parts: introduction to aircraft propulsion; basic concepts and one-dimensional gas dynamics analysis and performance of air breathing propulsion systems; and analysis and design of gas turbine engine components.
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adiabatic afterbumer afterburner aircraft airfoil altitude axial axial-ﬂow blade Brayton cycle Btu/(lbm bypass ratio Calculate calorically perfect gas combustion combustor component compressor pressure ratio constant control volume corrected mass ﬂow cycle analysis deﬁned deﬁnition determine drag duct efﬁciency eﬂiciency energy enthalpy entropy equation Example exhaust nozzle exit fan pressure ratio ﬁghter FIGURE ﬁnd ﬁrst ﬂight condition ﬂight Mach number ﬂuid ft/sec fuel/air ratio gas turbine engine heat interaction high-pressure ideal turbofan increases inlet isentropic kg/sec lbm/sec low-pressure turbine m/sec mass ﬂow rate maximum momentum normal shock nozzle oblique shock plotted polytropic propeller psia radius ramjet range factor rocket rotor shock wave shown in Fig speciﬁc fuel consumption speciﬁc heats speciﬁc thrust speed station stator steady ﬂow subsonic supercruise supersonic temperature ratio thermodynamic thrust speciﬁc fuel total temperature turbofan engine turbojet engine turboprop uninstalled thrust values variable variation velocity versus