Aircraft Propulsion Systems Technology and Design. (Record no. 68237)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04258nam a22004573i 4500 |
| 001 - CONTROL NUMBER | |
| control field | EBC3111570 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MiAaPQ |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20240729124522.0 |
| 006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS | |
| fixed length control field | m o d | |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION | |
| fixed length control field | cr cnu|||||||| |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240724s1989 xx o ||||0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781600860218 |
| Qualifying information | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Canceled/invalid ISBN | 9780930403249 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (MiAaPQ)EBC3111570 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (Au-PeEL)EBL3111570 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (CaPaEBR)ebr10516674 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC)922978802 |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | MiAaPQ |
| Language of cataloging | eng |
| Description conventions | rda |
| -- | pn |
| Transcribing agency | MiAaPQ |
| Modifying agency | MiAaPQ |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER | |
| Classification number | TL709 -- .A44 1989eb |
| 082 0# - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.134/353 |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Oates, Gordon C. |
| 245 10 - TITLE STATEMENT | |
| Title | Aircraft Propulsion Systems Technology and Design. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. |
| 264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Reston : |
| Name of producer, publisher, distributor, manufacturer | American Institute of Aeronautics and Astronautics, |
| Date of production, publication, distribution, manufacture, or copyright notice | 1989. |
| 264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | ©1989. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 1 online resource (535 pages) |
| 336 ## - CONTENT TYPE | |
| Content type term | text |
| Content type code | txt |
| Source | rdacontent |
| 337 ## - MEDIA TYPE | |
| Media type term | computer |
| Media type code | c |
| Source | rdamedia |
| 338 ## - CARRIER TYPE | |
| Carrier type term | online resource |
| Carrier type code | cr |
| Source | rdacarrier |
| 490 1# - SERIES STATEMENT | |
| Series statement | AIAA Education Series |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Cover -- Title -- Copyright -- Foreword -- Table of Contents -- Chapter 1. Design and Development of Aircraft Propulsion Systems -- 1.1 Introduction -- 1.2 Engine Design Objectives -- 1.3 Effect of Thermodynamic Variables on Engine Performance -- 1.4 Development of Thrust -- 1.5 Off-Design Performance of Gas Turbine Propulsion Engines -- 1.6 Losses in Available Energy -- 1.7 Interrelations Among Aerodynamic Components -- 1.8 Interaction with Other Specialties -- 1.9 Advanced Flow Calculations -- 1.10 Biography of a Typical Engine -- Chapter 2. Turbopropulsion Combustion Technology -- 2.1 Introduction -- 2.2 Combustion System Description/Definitions -- 2.3 Component Considerations -- 2.4 Design Tools -- 2.5 Future Requirements -- 2.6 Conclusions -- Chapter 3. Engine/Airframe Performance Matching -- 3.1 Introduction -- 3.2 Mission Analysis -- 3.3 Optimization of Engine/Airplane Match -- 3.4 Sensitivity and Influence Coefficients -- 3.5 Computer Simulation of Gas Turbine Engines -- Chapter 4. Inlets and Inlet/Engine Integration -- 4.1 Introduction -- 4.2 Elements of a Successful Inlet/Engine Integration Program -- 4.3 Definition of Subsonic Inlet/Engine Operational Requirements -- 4.4 Definition of Supersonic Inlet/Engine Operational Requirements -- 4.5 Engine Impact on Inlet Design -- 4.6 Inlet Impact on Engine Design -- 4.7 Validation of Inlet/Engine System -- Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics -- 5.1 Introduction -- 5.2 Nozzle Concept -- 5.3 Performance Predictions -- 5.4 Aerodynamic Load Predictions -- Chapter 6. Engine Operability -- 6.1 Introduction -- 6.2 Definitions -- 6.3 Stability Assessment -- 6.4 Aerodynamic Interface Plane -- 6.5 Total Pressure Distortion -- 6.6 Total Temperature Distortion -- 6.7 Planar Waves -- 6.8 Recoverability -- 6.9 Analytical Techniques -- 6.10 Summary. |
| 505 8# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Chapter 7. Aeroelasticity and Unsteady Aerodynamics -- 7.1 Introduction -- 7.2 Overview of Turbomachinery Flutter -- 7.3 Brief Survey of Turbomachinery Flutter Regimes -- 7.4 Elementary Considerations of Aircraft Wing Flutter -- 7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter -- 7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils -- 7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils -- 7.8 Dynamic Stall-Empiricism and Experiment -- 7.9 Coupled Blade-Disk-Shroud Stability Theory -- Subject Index -- A -- B -- C -- D -- E -- F -- G -- H -- I -- K -- L -- M -- N -- O -- P -- R -- S -- T -- U -- V -- W. |
| 588 ## - SOURCE OF DESCRIPTION NOTE | |
| Source of description note | Description based on publisher supplied metadata and other sources. |
| 590 ## - LOCAL NOTE (RLIN) | |
| Local note | Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Aircraft gas-turbines. |
| 655 #4 - INDEX TERM--GENRE/FORM | |
| Genre/form data or focus term | Electronic books. |
| 776 08 - ADDITIONAL PHYSICAL FORM ENTRY | |
| Relationship information | Print version: |
| Main entry heading | Oates, Gordon C. |
| Title | Aircraft Propulsion Systems Technology and Design |
| Place, publisher, and date of publication | Reston : American Institute of Aeronautics and Astronautics,c1989 |
| International Standard Book Number | 9780930403249 |
| 797 2# - LOCAL ADDED ENTRY--CORPORATE NAME (RLIN) | |
| Corporate name or jurisdiction name as entry element | ProQuest (Firm) |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| Uniform title | AIAA Education Series |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111570">https://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111570</a> |
| Public note | Click to View |
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