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Author: Gordon C. Oates
Publisher: AIAA
Published: 1985
Total Pages: 568
ISBN-13: 9781600860058
DOWNLOAD EBOOKAnnotation 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.
Author: Gordon C. Oates
Publisher:
Published: 1978
Total Pages: 830
ISBN-13:
DOWNLOAD EBOOKAuthor: Gordon C. Oates
Publisher: AIAA
Published: 1997
Total Pages: 476
ISBN-13: 9781600860065
DOWNLOAD EBOOKAuthor: Paul G. A. Cizmas
Publisher:
Published: 2021-11-24
Total Pages: 488
ISBN-13: 1108575595
DOWNLOAD EBOOKGet up to speed with this robust introduction to the aerothermodynamics principles underpinning jet propulsion, and learn how to apply these principles to jet engine components. Suitable for undergraduate students in aerospace and mechanical engineering, and for professional engineers working in jet propulsion, this textbook includes consistent emphasis on fundamental phenomena and key governing equations, providing students with a solid theoretical grounding on which to build practical understanding; clear derivations from first principles, enabling students to follow the reasoning behind key assumptions and decisions, and successfully apply these approaches to new problems; practical examples grounded in real-world jet propulsion scenarios illustrate new concepts throughout the book, giving students an early introduction to jet and rocket engine considerations; and online materials for course instructors, including solutions, figures, and software resources, to enhance student teaching.
Author: Gordon C. Oates
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 1989
Total Pages: 544
ISBN-13:
DOWNLOAD EBOOKAnnotation The last of three texts on aircraft propulsion technology planned by Gordon C. Oates. Other titles: Aerodynamics of gas turbine and rocket propulsion (1988); Aerothermodynamics of aircraft engine components (1985). Chapters treat combustion technology, engine/airplane performance matching, inlets and inlet/engine integration, variable convergent/divergent nozzle aerodynamics, engine instability, aeroelasticity, and unsteady aerodynamics. Annotation(c) 2003 Book News, Inc., Portland, OR (booknews.com)
Author: Ronald D. Flack
Publisher: Cambridge University Press
Published: 2005-04-25
Total Pages: 696
ISBN-13: 1107393884
DOWNLOAD EBOOKThis introductory 2005 text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. Previous coursework in fluid mechanics and thermodynamics is elucidated and applied to help the student understand and predict the characteristics of engine components and various types of engines and power gas turbines. Numerous examples help the reader appreciate the methods and differing, representative physical parameters. A capstone chapter integrates the text material into a portion of the book devoted to system matching and analysis so that engine performance can be predicted for both on- and off-design conditions. The book is designed for advanced undergraduate and first-year graduate students in aerospace and mechanical engineering. A basic understanding of fluid dynamics and thermodynamics is presumed. Although aircraft propulsion is the focus, the material can also be used to study ground- and marine-based gas turbines and turbomachinery and some advanced topics in compressors and turbines.
Author: Meinhard T. Schobeiri
Publisher: Springer
Published: 2017-06-06
Total Pages: 522
ISBN-13: 3319583786
DOWNLOAD EBOOKThis book written by a world-renowned expert with more than forty years of active gas turbine R&D experience comprehensively treats the design of gas turbine components and their integration into a complete system. Unlike many currently available gas turbine handbooks that provide the reader with an overview without in-depth treatment of the subject, the current book is concentrated on a detailed aero-thermodynamics, design and off-deign performance aspects of individual components as well as the system integration and its dynamic operation.This new book provides practicing gas turbine designers and young engineers working in the industry with design material that the manufacturers would keep proprietary. The book is also intended to provide instructors of turbomachinery courses around the world with a powerful tool to assign gas turbine components as project and individual modules that are integrated into a complete system. Quoting many statements by the gas turbine industry professionals, the young engineers graduated from the turbomachinery courses offered by the author, had the competency of engineers equivalent to three to four years of industrial experience.
Author: Erian A. Baskharone
Publisher: Cambridge University Press
Published: 2006-07-31
Total Pages: 599
ISBN-13: 0521858100
DOWNLOAD EBOOKThis book is intended for advanced undergraduate and graduate students in mechanical and aerospace engineering taking a course commonly called Principles of Turbomachinery or Aerospace Propulsion. The book begins with a review of basic thermodynamics and fluid mechanics principles to motive their application to aerothermodynamics and real-life design issues. This approach is ideal for the reader who will face practical situations and design decisions in the gas turbine industry. The text is fully supported by over 200 figures, numerous examples, and homework problems.
Author: Meredith Colket
Publisher:
Published: 2021
Total Pages: 0
ISBN-13: 9781624106033
DOWNLOAD EBOOKIn summarizing the results obtained in the first five years of the National Jet Fuel Combustion Program (NJFCP), this book demonstrates that there is still much to be learned about the combustion of alternative jet fuels.
Author: S. Can Gülen
Publisher: Cambridge University Press
Published: 2019-02-14
Total Pages: 735
ISBN-13: 1108416659
DOWNLOAD EBOOKEverything you wanted to know about industrial gas turbines for electric power generation in one source with hard-to-find, hands-on technical information.
