Aerothermodynamics of Gas Turbine and Rocket Propulsion PDF Download
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Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860065
Category : Aerothermodynamics
Languages : en
Pages : 476
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Book Description
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860065
Category : Aerothermodynamics
Languages : en
Pages : 476
Get Book
Book Description
Author: Gordon C. Oates
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 480
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Book Description
This seminal book on gas turbine technology has been a bestseller since it was first published. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are atmosphere programs, quasi-one-dimensional flow programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and PC given, He and PC given, isentropic expansion).
Author: Gordon C. Oates
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
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Book Description
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: Jack D. Mattingly
Publisher: American Institute of Aeronautics and Astronautics Incorporated
ISBN: 9781624103711
Category : Aircraft gas-turbines
Languages : en
Pages : 0
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Book Description
Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Textbook coverage has been revised and expanded, including a new chapter on compressible flow. Design concepts are introduced early and integrated throughout. Written with extensive student input, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles.
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: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860218
Category : Aircraft gas-turbines
Languages : en
Pages : 544
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Book Description
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.
Author: G.W. Meetham
Publisher: Springer Science & Business Media
ISBN: 9400981112
Category : Technology & Engineering
Languages : en
Pages : 311
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Book Description
The turbine has many advantages over other prime movers for producing power. The first turbine used water as the working fluid and this principle is still used in hydro-electric power generation. The steam turbine was developed late in the nineteenth century and was first applied to marine propulsion by Parsons in 1897. Since that time it has become the most widely used prime mover in electricity generation and marine propulsion. The equipment required to generate steam is bulky however and it was realised that much more compact power plant could be designed if the hot gases used for steam generation could drive the turbine directly. Early attempts to produce gas turbines were unsuccessful for several reasons, one major problem being that materials with the capability of operating at sufficiently high stresses and temperatures were not available. Following the first experimental Whittle engine in 1937, the emphasis on the development of the gas turbine engine for aircraft propulsion during World War II changed this situation dramatically. Gas turbine powered civil aircraft entered airline service in the early 1950s and gas turbines also began to compete successfully in other fields. Apart from the aircraft market, they have been used widely in pumping sets for oil and gas transmission pipelines and peak load electricity generation. Use in warship propulsion is increasing and there is currently major activity, in the USA in particular, in developments for vehicular propulsion.
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.
