Aerothermodynamics of aircraft engine components

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Bibliographic Details
Other Authors: Oates, Gordon C.
Format: eBook
Language: English
Published: New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1985.
Series: AIAA education series.
Subjects:
Aerothermodynamics.
Aircraft gas-turbines.
elektronické knihy
electronic books
ISBN: 9781601192042
1601192045
0915928973
9780915928972
1600860052
9781600860058
Physical Description: 1 online resource (vii, 551 pages) : illustrations

Cover

Table of contents

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042 |a dlr 
245 0 0 |a Aerothermodynamics of aircraft engine components /  |c edited by Gordon C. Oates. 
260 |a New York, N.Y. :  |b American Institute of Aeronautics and Astronautics,  |c ©1985. 
300 |a 1 online resource (vii, 551 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a AIAA education series 
504 |a Includes bibliographical references and index. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 8 |a Annotation  |b 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. 
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 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 
505 8 |a FG -- H -- I -- J -- K -- L -- M -- N -- O -- P -- R -- S -- T -- V -- W 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aerothermodynamics. 
650 0 |a Aircraft gas-turbines. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Oates, Gordon C. 
776 0 8 |i Print version:  |t Aerothermodynamics of aircraft engine components.  |d New York, N.Y. : American Institute of Aeronautics and Astronautics, ©1985  |z 0915928973  |w (DLC) 85013355  |w (OCoLC)12132522 
830 0 |a AIAA education series. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpAAEC0007/aerothermodynamics-of-aircraft?kpromoter=marc  |y Full text 

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