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Author: Klaus Hünecke
Publisher: Zenith Press
ISBN: 9780760304594
Category : Transportation
Languages : en
Pages : 241
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Book Description
Broaden your knowledge of jet engine technology and its associated subjects. This is a technically comprehensive study of the components that constitute a gas turbine aero-engine and examines each part's design and function in practice. Concentrates on turbojet, turboprop and turbofan designs, and is applicable to civilian and military usage. Contains an overview of the main design types and fundamentals, and looks at air intakes, compressors, turbines and exhaust systems in great detail.
Author: Klaus Hünecke
Publisher: Zenith Press
ISBN: 9780760304594
Category : Transportation
Languages : en
Pages : 241
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Book Description
Broaden your knowledge of jet engine technology and its associated subjects. This is a technically comprehensive study of the components that constitute a gas turbine aero-engine and examines each part's design and function in practice. Concentrates on turbojet, turboprop and turbofan designs, and is applicable to civilian and military usage. Contains an overview of the main design types and fundamentals, and looks at air intakes, compressors, turbines and exhaust systems in great detail.
Author: Norman E. Borden
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 200
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Book Description
Author: Ronald D. Flack
Publisher: Cambridge University Press
ISBN: 1107393884
Category : Technology & Engineering
Languages : en
Pages : 696
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Book Description
This 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: United Aircraft Corporation
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 128
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Book Description
Author: William W. Bathie
Publisher: John Wiley & Sons
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 494
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Book Description
Presents the fundamentals of the gas turbine engine, including cycles, components, component matching, and environmental considerations.
Author: Nicholas Cumpsty
Publisher: Cambridge University Press
ISBN: 1107511224
Category : Science
Languages : en
Pages : 369
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Book Description
This book is an introduction to the design of modern civil and military jet engines using engine design projects.
Author: Pratt & Whitney Canada
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 112
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Book Description
Author: Ahmed F. El-Sayed
Publisher: Springer
ISBN: 1447167961
Category : Technology & Engineering
Languages : en
Pages : 1025
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Book Description
This book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained. Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of: thermodynamic cycles of shaft engines (piston, turboprop, turboshaft and propfan); jet engines (pulsejet, pulse detonation engine, ramjet, scramjet, turbojet and turbofan); chemical and non-chemical rocket engines; conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and conceptual design of different modules of aero-engines in their design and off-design state. Aimed at graduate and final-year undergraduate students, this textbook provides a thorough grounding in the history and classification of both aircraft and rocket engines, important design features of all the engines detailed, and particular consideration of special aircraft such as unmanned aerial and short/vertical takeoff and landing aircraft. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors.
Author:
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 64
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Book Description
Author: N. A. Cumpsty
Publisher: Cambridge University Press
ISBN: 9780521541442
Category : Technology & Engineering
Languages : en
Pages : 326
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Book Description
This is the second edition of Cumpsty's excellent self-contained introduction to the aerodynamic and thermodynamic design of modern civil and military jet engines. Through two engine design projects, first for a new large passenger aircraft, and second for a new fighter aircraft, the text introduces, illustrates and explains the important facets of modern engine design. Individual sections cover aircraft requirements and aerodynamics, principles of gas turbines and jet engines, elementary compressible fluid mechanics, bypass ratio selection, scaling and dimensional analysis, turbine and compressor design and characteristics, design optimization, and off-design performance. The book emphasises principles and ideas, with simplification and approximation used where this helps understanding. This edition has been thoroughly updated and revised, and includes a new appendix on noise control and an expanded treatment of combustion emissions. Suitable for student courses in aircraft propulsion, but also an invaluable reference for engineers in the engine and airframe industry.
