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Aerothermodynamics of aircraft engine components /
Annotation
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
New York, N.Y. :
American Institute of Aeronautics and Astronautics,
©1985.
|
| Colección: | AIAA education series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 037 | |b Knovel Corporation |n http://www.knovel.com | ||
| 042 | |a dlr | ||
| 050 | 4 | |a TL574.A45 |b A37 1985eb | |
| 082 | 0 | 4 | |a 629.134/353 |2 22 |
| 049 | |a UAMI | ||
| 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. | ||
| 588 | 0 | |a Print version record. | |
| 506 | |3 Use copy |f Restrictions unspecified |2 star |5 MiAaHDL | ||
| 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. | |
| 533 | |a Electronic reproduction. |b [Place of publication not identified] : |c HathiTrust Digital Library, |d 2010. |5 MiAaHDL | ||
| 538 | |a 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. |u http://purl.oclc.org/DLF/benchrepro0212 |5 MiAaHDL | ||
| 583 | 1 | |a digitized |c 2010 |h HathiTrust Digital Library |l committed to preserve |2 pda |5 MiAaHDL | |
| 506 | |a Access restricted to Ryerson students, faculty and staff. |5 CaOTR | ||
| 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 System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� 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 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"" | |
| 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 ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aerothermodynamics. | |
| 650 | 0 | |a Aircraft gas-turbines. | |
| 650 | 6 | |a Aérothermodynamique. | |
| 650 | 7 | |a Aerothermodynamics. |2 fast |0 (OCoLC)fst00798683 | |
| 650 | 7 | |a Aircraft gas-turbines. |2 fast |0 (OCoLC)fst00802823 | |
| 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://appknovel.uam.elogim.com/kn/resources/kpAAEC0007/toc |z Texto completo |
| 938 | |a ebrary |b EBRY |n ebr10516677 | ||
| 938 | |a YBP Library Services |b YANK |n 7355834 | ||
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