Multi-disciplinary conceptual design of future jet engine systems

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Multi-disciplinary conceptual design of future jet engine systems ( multi-disciplinary-conceptual-design-future-jet-engine-syste )

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Nomenclature Konstantinos G. Kyprianidis T T13 T24 T26 T30 T31 T4 T41 T44 T46 Tf Tf lame Tin Tc,in Ts T133Q132 T26Q25 T308Q307 T601Q6 TF U V W1 W2 W24 W26 WA/C Wc Wf W131Q132 W132Q25 WAR x y Z α1 Total temperature in [K] Bypass duct inlet total temperature in [K] Intermediate pressure compressor inlet temperature in [K] High pressure compressor inlet temperature in [K] High pressure compressor delivery temperature in [K] Combustor inlet temperature in [K] Combustor outlet temperature in [K] High pressure turbine rotor inlet temperature in [K] Intermediate pressure turbine rotor inlet temperature in [K] Low pressure turbine rotor inlet temperature in [K] Fuel injection temperature in [K] Combustor primary zone flame temperature in [K] Component inlet total temperature in [K] Compressor inlet total temperature in [K] Static temperature in [K] Intercooler cold stream temperature change in [K] Intercooler hot stream temperature change in [K] Recuperator cold (air) stream temperature change in [K] Recuperator hot (gas) stream temperature change in [K] Technology Factor exponent in [-] Turbine blade speed in [m/s] Velocity in [m/s] Intake inlet mass flow in [kg/s] Fan inlet mass flow in [kg/s] Intermediate pressure compressor inlet mass flow in [kg/s] High pressure compressor inlet mass flow in [kg/s] Aircraft weight in [kg] Corrected mass flow in [kg/s] Fuel mass flow in [kg/s] Intercooler splitter bypass ratio in [-] Intercooler cold to hot mass flow ratio in [-] Water to Air Ratio in [-] Mass fraction in [-] Mole fraction in [-] Zweifel number in [-] Turbine stage inlet flow angle in [deg] xxxii

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