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 Drag1.3.3 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 Afterburner1.8.1 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 Analysis1.10.2.3 Optimum Power Split between the Propeller and the Jet; 1.10.2.4 Advanced Propeller: Prop-Fan; 1.11 High-Speed Air-Breathing Engines; 1.11.1 Supersonic Combustion Ramjet; 1.11.1.1 Inlet Analysis; 1.11.1.2 Scramjet Combustor; 1.11.1.3 Scramjet Nozzle; 1.12 Rocket-Based Airbreathing Propulsion; 1.13 Summary; References; Chapter 2 Aircraft Aerodynamics
A Review; 2.1 Introduction; 2.2 Similarity Parameters in Compressible Flow: Flight vs. Wind Tunnel; 2.3 Physical Boundary Conditions on a Solid Wall (in Continuum Mechanics); 2.4 Profile and Parasite Drag

2.4.1 Boundary Layers2.4.1.1 Case 1: Incompressible Laminar Flow; 2.4.1.2 Case 2: Laminar Compressible Boundary Layers; 2.4.1.3 Case 3: Turbulent Boundary Layers; 2.4.1.4 Case 4: Transition; 2.4.2 Profile Drag of an Airfoil; 2.5 Drag Due to Lift; 2.5.1 Classical Theory; 2.5.2 Optimal Spanloading: The Case of Bell Spanload; 2.6 Waves in Supersonic Flow; 2.6.1 Speed of Sound; 2.6.2 Normal Shock Wave; 2.6.3 Oblique Shock Waves; 2.6.4 Expansion Waves; 2.7 Compressibility Effects and Critical Mach Number; 2.8 Drag Divergence Phenomenon and Supercritical Airfoil; 2.9 Wing Sweep