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Aircraft propulsion /
"Aircraft Propulsion, Second Edition is a comprehensive textbook covering aircraft gas turbine engine and rocket propulsion from the basic principles to more advanced treatments in engine components"--
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Chichester, West Sussex, United Kingdom :
Wiley,
2014.
|
| Edición: | Second edition. |
| Temas: | |
| Acceso en línea: | Texto completo (Requiere registro previo con correo institucional) |
Tabla de Contenidos:
- Aircraft Propulsion; Table of Contents; Preface to the Second Edition; Acknowledgments; Preface; Intended Audience; Motivation; Mathematical Level; Chapter Organization and Topical Coverage; Instructor Resources; Acknowledgments; Nomenclature; 1 Introduction; 1.1 History of the Airbreathing Jet Engine, a Twentieth-Century Invention-The Beginning; 1.2 Innovations in Aircraft Gas Turbine Engines; 1.2.1 Multispool Configuration; 1.2.2 Variable Stator; 1.2.3 Transonic Compressor; 1.2.4 Low-Emission Combustor; 1.2.5 Turbine Cooling; 1.2.6 Exhaust Nozzles.
- 1.2.7 Modern Materials and Manufacturing Techniques1.3 New Engine Concepts; 1.3.1 Advanced Turboprop (ATP) and Geared Turbofan (GTF); 1.3.2 Advanced Airbreathing Rocket Technology; 1.3.3 Wave Rotor Topping Cycle; 1.3.4 Pulse Detonation Engine (PDE); 1.3.5 Millimeter-Scale Gas Turbine Engines: Triumph of MEMS and Digital Fabrication; 1.3.6 Combined Cycle Propulsion: Engines from Takeoff to Space; 1.4 New Vehicles; 1.5 Summary; 1.6 Roadmap for the Second Edition; References; Problems; 2 Compressible Flow with Friction and Heat: A Review; 2.1 Introduction; 2.2 A Brief Review of Thermodynamics.
- 2.3 Isentropic Process and Isentropic Flow2.4 Conservation Principles for Systems and Control Volumes; 2.5 Speed of Sound & Mach Number; 2.6 Stagnation State; 2.7 Quasi-One-Dimensional Flow; 2.8 Area-Mach Number Relationship; 2.9 Sonic Throat; 2.10 Waves in Supersonic Flow; 2.11 Normal Shocks; 2.12 Oblique Shocks; 2.13 Conical Shocks; 2.14 Expansion Waves; 2.15 Frictionless, Constant-Area Duct Flow with Heat Transfer; 2.16 Adiabatic Flow of a Calorically Perfect Gas in a Constant-Area Duct with Friction; 2.17 Friction (Drag) Coefficient Cf and D'Arcy Friction Factor fD.
- 2.18 Dimensionless Parameters2.19 Fluid Impulse; 2.20 Summary of Fluid Impulse; References; Problems; 3 Engine Thrust and Performance Parameters; 3.1 Introduction; 3.1.1 Takeoff Thrust; 3.2 Installed Thrust-Some Bookkeeping Issues on Thrust and Drag; 3.3 Engine Thrust Based on the Sum of Component Impulse; 3.4 Rocket Thrust; 3.5 Airbreathing Engine Performance Parameters; 3.5.1 Specific Thrust; 3.5.2 Specific Fuel Consumption and Specific Impulse; 3.5.3 Thermal Efficiency; 3.5.4 Propulsive Efficiency; 3.5.5 Engine Overall Efficiency and Its Impact on Aircraft Range and Endurance.
- 3.6 Modern Engines, Their Architecture and Some Performance Characteristics3.7 Summary; References; Problems; 4 Gas Turbine Engine Cycle Analysis; 4.1 Introduction; 4.2 The Gas Generator; 4.3 Aircraft Gas Turbine Engines; 4.3.1 The Turbojet Engine; 4.3.2 The Turbojet Engine with an Afterburner; 4.3.3 The Turbofan Engine; 4.3.4 Ultra-High Bypass (UHB) Turbofan Engines; 4.4 Analysis of a Mixed-Exhaust Turbofan Engine with an Afterburner; 4.4.1 Mixer; 4.4.2 Cycle Analysis; 4.5 The Turboprop Engine; 4.5.1 Introduction; 4.5.2 Propeller Theory; 4.5.3 Turboprop Cycle Analysis; 4.6 Summary.