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Title Aerothermodynamics of aircraft engine components / edited by Gordon C. Oates
Published New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1985

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Description 1 online resource (vii, 551 pages) : illustrations
Series AIAA education series
AIAA education series.
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 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
Summary Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design
Bibliography Includes bibliographical references and index
Notes Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL
Print version record
digitized 2010 HathiTrust Digital Library committed to preserve pda MiAaHDL
Subject Aerothermodynamics.
Aircraft gas-turbines.
Aerothermodynamics
Aircraft gas-turbines
Form Electronic book
Author Oates, Gordon C.
ISBN 9781601192042
1601192045
0915928973
9780915928972
1600860052
9781600860058