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Aerothermodynamics of Aircraft Engine Components.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Oates, Gordon C.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston : American Institute of Aeronautics and Astronautics, 2000.
Temas:
Acceso en línea:Texto completo

MARC

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100 1 |a Oates, Gordon C. 
245 1 0 |a Aerothermodynamics of Aircraft Engine Components. 
260 |a Reston :  |b American Institute of Aeronautics and Astronautics,  |c 2000. 
300 |a 1 online resource (559 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
588 0 |a Print version record. 
505 0 |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"" 
505 8 |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 Systemâ€?Technical Requirements""; ""3.6 Content of Current and Developing Design Systemsâ€? The Technology Base""; ""3.7 Component and Configuration Experimental Development"" 
505 8 |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 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"" 
505 8 |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"" 
505 8 |a ""F""""g""; ""h""; ""i""; ""j""; ""k""; ""l""; ""m""; ""n""; ""o""; ""p""; ""r""; ""s""; ""t""; ""v""; ""w"" 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Aerothermodynamics. 
650 0 |a Aircraft gas-turbines. 
650 6 |a Aérothermodynamique. 
650 7 |a Aerothermodynamics  |2 fast 
650 7 |a Aircraft gas-turbines  |2 fast 
758 |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 
776 0 8 |i Print version:  |a Oates, Gordon C.  |t Aerothermodynamics of Aircraft Engine Components.  |d Reston : American Institute of Aeronautics and Astronautics, ©2000  |z 9780915928972 
856 4 0 |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111573  |z Texto completo 
938 |a ProQuest Ebook Central  |b EBLB  |n EBL3111573 
994 |a 92  |b IZTAP