Aircraft Propulsion

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Detalles Bibliográficos
Autor principal: Farokhi, Saeed
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Newark : John Wiley & Sons, Incorporated, 2014.
Colección:New York Academy of Sciences Ser.
Temas:
Electronic books.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Intro
  • 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 Techniques
  • 1.3 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 Flow
  • 2.4 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 Parameters
  • 2.19 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 Characteristics
  • 3.7 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

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