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Aerothermodynamics of Aircraft Engine Components.

By: Material type: TextTextSeries: AIAA Education SeriesPublisher: Reston : American Institute of Aeronautics and Astronautics, 1985Copyright date: ©1985Edition: 1st edDescription: 1 online resource (559 pages)Content type:
  • text
Media type:
  • computer
Carrier type:
  • online resource
ISBN:
  • 9781600860058
Subject(s): Genre/Form: Additional physical formats: Print version:: Aerothermodynamics of Aircraft Engine ComponentsDDC classification:
  • 629.134/353
LOC classification:
  • TL574.A45 -- A37 1985eb
Online resources:
Contents:
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 System-Technical Requirements -- 3.6 Content of Current and Developing Design Systems- 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 Back-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 Layers -- 6.1 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 -- F -- G -- H -- I -- J -- K -- L -- M -- N -- O -- P -- R -- S -- T -- V -- W.
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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 System-Technical Requirements -- 3.6 Content of Current and Developing Design Systems- 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 Back-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 Layers -- 6.1 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 -- F -- G -- H -- I -- J -- K -- L -- M -- N -- O -- P -- R -- S -- T -- V -- W.

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Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.

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