Future propulsion systems and energy sources in sustainable aviation

Cover -- Title Page -- Copyright Page -- Contents -- Preface -- Acknowledgments -- Abbreviations and Acronyms -- About the Companion Website -- Chapter 1 Aircraft Engines - A Review -- 1.1 Introduction -- 1.2 Aerothermodynamics of Working Fluid -- 1.2.1 Isentropic Process and Isentropic Flow -- 1.2.2 Conservation of Mass -- 1.2.3 Conservation of Linear Momentum -- 1.2.4 Conservation of Angular Momentum -- 1.2.5 Conservation of Energy -- 1.2.6 Speed of Sound and Mach Number -- 1.2.7 Stagnation State -- 1.3 Thrust and Specific Fuel Consumption -- 1.3.1 Takeoff Thrust -- 1.3.2 Installed Thrust - Some Bookkeeping Issues on Thrust and Drag -- 1.3.3 Air-Breathing Engine Performance Parameters -- 1.3.3.1 Specific Thrust -- 1.3.3.2 Specific Fuel Consumption and Specific Impulse -- 1.4 Thermal and Propulsive Efficiency -- 1.4.1 Thermal Efficiency -- 1.4.2 Propulsive Efficiency -- 1.4.3 Engine Overall Efficiency and Its Impact on Aircraft Range and Endurance -- 1.5 Gas Generator -- 1.6 Engine Components -- 1.6.1 The Inlet -- 1.6.2 The Nozzle -- 1.6.3 The Compressor -- 1.6.4 The Combustor -- 1.6.5 The Turbine -- 1.7 Performance Evaluation of a Turbojet Engine -- 1.8 Turbojet Engine with an Afterburner -- 1.8.1 Introduction -- 1.8.2 Analysis -- 1.9 Turbofan Engine -- 1.9.1 Introduction -- 1.9.2 Analysis of a Separate-Exhaust Turbofan Engine -- 1.9.3 Thermal Efficiency of a Turbofan Engine -- 1.9.4 Propulsive Efficiency of a Turbofan Engine -- 1.9.5 Ultra-High Bypass (UHB) Geared Turbofan Engines -- 1.9.6 Analysis of Mixed-Exhaust Turbofan Engines with Afterburners -- 1.9.6.1 Mixer -- 1.9.6.2 Mixed-Turbofan Cycle Analysis -- 1.9.6.3 Solution Procedure -- 1.10 Turboprop Engine -- 1.10.1 Introduction -- 1.10.2 Turboprop Cycle Analysis -- 1.10.2.1 The New Parameters -- 1.10.2.2 Design-Point Analysis.