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|a 9781600860058
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|a 1600860052
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|b BV044094880
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|a (OCoLC)922978789
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|a TL574.A45 ǂb A37 1985eb
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|a 629.134/353
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|a UAMI
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|a Oates, Gordon C.
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|a Aerothermodynamics of Aircraft Engine Components.
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|a Reston :
|b American Institute of Aeronautics and Astronautics,
|c 2000.
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|a 1 online resource (559 pages)
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
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|a Print version record.
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|a ""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""
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|a ""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""
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|a ""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""
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|a ""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""
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|a ""F""""g""; ""h""; ""i""; ""j""; ""k""; ""l""; ""m""; ""n""; ""o""; ""p""; ""r""; ""s""; ""t""; ""v""; ""w""
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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650 |
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|a Aerothermodynamics.
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|a Aircraft gas-turbines.
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|a Aérothermodynamique.
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|a Aerothermodynamics
|2 fast
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|a Aircraft gas-turbines
|2 fast
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|i has work:
|a Aerothermodynamics of aircraft engine components (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGPm4WfR7Tht3TRpDkXVBX
|4 https://id.oclc.org/worldcat/ontology/hasWork
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0 |
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|i Print version:
|a Oates, Gordon C.
|t Aerothermodynamics of Aircraft Engine Components.
|d Reston : American Institute of Aeronautics and Astronautics, ©2000
|z 9780915928972
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856 |
4 |
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|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111573
|z Texto completo
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938 |
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|a ProQuest Ebook Central
|b EBLB
|n EBL3111573
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994 |
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|a 92
|b IZTAP
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