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Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
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Book Description
Annotation 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: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
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Book Description
Annotation 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:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
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Book Description
Author: Gordon C. Oates
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 544
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Book Description
Annotation 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: Gordon C. Oates
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 5
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Book Description
Author: F. Whittle
Publisher: Elsevier
ISBN: 1483293211
Category : Technology & Engineering
Languages : en
Pages : 276
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Book Description
For the first time simplified methods of dealing with gas turbine thermal cycles, and further theoretical innovations, have been embodied into a concise textbook. All the major aspects of the subject are covered in a comprehensive and lucid manner. Examples are included for greater clarity
Author: Paul G. A. Cizmas
Publisher: Cambridge University Press
ISBN: 1108480756
Category : Science
Languages : en
Pages : 487
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Book Description
This robust introduction to aerothermodynamics uses example-based teaching to provide students with a solid theoretical foundation linked to real-world engineering scenarios.
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860065
Category : Aerothermodynamics
Languages : en
Pages : 476
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Book Description
Author: Jack D. Mattingly
Publisher: AIAA
ISBN: 9781600860164
Category : Aircraft gas-turbines
Languages : en
Pages : 732
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Book Description
Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).
Author: David R. Greatrix
Publisher: Springer Science & Business Media
ISBN: 1447124847
Category : Technology & Engineering
Languages : en
Pages : 531
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Book Description
Whilst most contemporary books in the aerospace propulsion field are dedicated primarily to gas turbine engines, there is often little or no coverage of other propulsion systems and devices such as propeller and helicopter rotors or detailed attention to rocket engines. By taking a wider viewpoint, Powered Flight - The Engineering of Aerospace Propulsion aims to provide a broader context, allowing observations and comparisons to be made across systems that are overlooked by focusing on a single aspect alone. The physics and history of aerospace propulsion are built on step-by-step, coupled with the development of an appreciation for the mathematics involved in the science and engineering of propulsion. Combining the author’s experience as a researcher, an industry professional and a lecturer in graduate and undergraduate aerospace engineering, Powered Flight - The Engineering of Aerospace Propulsion covers its subject matter both theoretically and with an awareness of the practicalities of the industry. To ensure that the content is clear, representative but also interesting the text is complimented by a range of relevant graphs and photographs including representative engineering, in addition to several propeller performance charts. These items provide excellent reference and support materials for graduate and undergraduate projects and exercises. Students in the field of aerospace engineering will find that Powered Flight - The Engineering of Aerospace Propulsion supports their studies from the introductory stage and throughout more intensive follow-on studies.
Author: Meinhard T. Schobeiri
Publisher: Springer
ISBN: 3319583786
Category : Technology & Engineering
Languages : en
Pages : 510
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Book Description
This 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.