Aerothermodynamics of aircraft engine components /

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Otros Autores: Oates, Gordon C.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1985.
Colección:AIAA education series.
Temas:
Aerothermodynamics.
Aircraft gas-turbines.
Aérothermodynamique.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Title
  • Copyright
  • Foreword
  • Table of Contents
  • Preface
  • Chapter 1. Fundamentals of Combustion
  • 1.1 Introduction
  • 1.2 Chemistry
  • 1.3 Thermodynamics
  • 1.4 Gasdynamics and Diffusion Processes
  • 1.5 Combustion Parameters
  • 1.6 Jet Fuels
  • 1.7 Summary
  • Chapter 2. Afterburners
  • 2.1 Introduction
  • 2.2 Diffuser
  • 2.3 Fuel Injection, Atomization, and Vaporization
  • 2.4 Ignition
  • 2.5 Stabilization Process
  • 2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures
  • 2.7 Nozzle and Fuel Control Systems
  • ""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design Systemâ€?Technical Requirements""; ""3.6 Content of Current and Developing Design Systemsâ€? The Technology Base""; ""3.7 Component and Configuration Experimental Development""
  • ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Backâ€?Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances""
  • Chapter 6. Computation of Turbomachinery Boundary Layers6.1 Introduction
  • 6.2 Two-Dimensional or Axisymmetric Boundary Layers
  • 6.3 Three-Dimensional Boundary Layers
  • 6.4 Boundary-Layer Separation
  • 6.5 Turbulence Models
  • 6.6 Conclusion
  • Chapter 7. Engine Noise
  • 7.1 Introduction
  • 7.2 Scales and Ratings for Noise
  • 7.3 Introduction to Acoustics of Ducts
  • 7.4 Compressor and Fan Noise
  • 7.5 Turbine Noise
  • 7.6 Core Noise
  • 7.7 Acoustic Treatment
  • 7.8 Conclusions and Future Prospects
  • Subject Index
  • A
  • B
  • C
  • D
  • E
  • FG
  • H
  • I
  • J
  • K
  • L
  • M
  • N
  • O
  • P
  • R
  • S
  • T
  • V
  • W

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