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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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Konstantinos G. Kyprianidis Nomenclature IC Eff IC Wcold/Whot L/D LHV m M M0 Mcr N OPR P P2 P13 P24 P26 P3 P31 P41 P44 P46 Pc,in P13Q2 P23Q2 P25Q24 P3Q26 PR PRc PW PWX4 PWX44 PWX46 R RA/C S SFC SR Intercooler effectiveness in [-] Intercooler cold to hot mass flow ratio in [-] Lift to Drag ratio in [-] Lower Heating Value of fuel in [J/kg] Number of noise sources in [-] Mach number in [-] Flight Mach number in [-] Cruise flight Mach number in [-] Rotational speed in [rpm] Overall Pressure Ratio in [-] Total pressure in [kPa] Fan inlet total pressure in [kPa] Bypass duct inlet total pressure in [kPa] Intermediate pressure compressor inlet total pressure in [kPa] High pressure compressor inlet total pressure in [kPa] High pressure compressor delivery total pressure in [kPa] Combustor inlet totalpressure in [kPa] High pressure turbine rotor inlet total pressure in [kPa] Intermediate pressure turbine rotor inlet total pressure in [kPa] Low pressure turbine rotor inlet total pressure in [kPa] Compressor inlet total pressure in [kPa] Fan tip pressure ratio in [-] Fan root pressure ratio in [-] Intermediate pressure compressor pressure ratio in [-] High pressure compressor pressure ratio in [-] Component pressure ratio in [-]] Compressor pressure ratio in [-]] Required work in [MW] High pressure shaft power off-take in [kW] Intermediate pressure shaft power off-take in [kW] Low pressure shaft power off-take in [kW] Specific gas constant in [J/(kg·K)] Aircraft range in [km] Turbine blade pitch in [mm] Specific Fuel Consumption in [g fuel/(kN·s)] Specific Range in [m/kg fuel] xxxi

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