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 Here
Book Description
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: Paul G. A. Cizmas
Publisher:
ISBN: 1108575595
Category : Science
Languages : en
Pages : 488
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Book Description
Get 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: Meinhard T. Schobeiri
Publisher: Springer
ISBN: 3319583786
Category : Technology & Engineering
Languages : en
Pages : 522
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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: George P. Sutton
Publisher: John Wiley & Sons
ISBN: 9780471326427
Category : Science
Languages : en
Pages : 772
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Book Description
Aerospace Engineering/Mechanical Engineering The definitive text on rocket propulsion-now completely revised to reflect rapid advancements in the field For more than fifty years, this seminal text has been regarded as the single most authoritative sourcebook on rocket propulsion technology. More comprehensive and coherently organized than any other book on the subject, Rocket Propulsion Elements guides readers evenhandedly through the complex factors that shape propulsion, with both theory and practical design considerations. With more than a third of the text and illustrations either completely new or extensively revised, this latest edition includes current information on engine structures, nozzle theory, gas properties, thrust chambers, launch vehicles, and more. With a detailed table of contents breaking down each chapter into subsections-as well as an expanded index of key words-the Seventh Edition efficiently steers readers quickly to the information they need. Other highlights include: * Separate chapters on liquid, solid, and hybrid propulsion systems and a new chapter on thrust chambers including the new aerospike nozzle * Comprehensive coverage of rocket propulsion technology, with applications to space flight, satellite flight, and guided and unguided missiles * Problem-solving examples and exercises relevant to actual design situations * More than 340 illustrations, including photographs, tables, and graphs * Coherent, up-to-date chapter on electrical propulsion balancing fundamentals with practical aspects and applications For professional engineers in the aerospace and defense industries as well as undergraduate and graduate students in mechanical and aerospace engineering, this time-honored resource is indispensable for its scope of coverage and utility.
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860218
Category : Aircraft gas-turbines
Languages : en
Pages : 544
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Book Description
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: Claire Soares
Publisher: Elsevier
ISBN: 0124104851
Category : Technology & Engineering
Languages : en
Pages : 1021
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Book Description
Covering basic theory, components, installation, maintenance, manufacturing, regulation and industry developments, Gas Turbines: A Handbook of Air, Sea and Land Applications is a broad-based introductory reference designed to give you the knowledge needed to succeed in the gas turbine industry, land, sea and air applications.Providing the big picture view that other detailed, data-focused resources lack, this book has a strong focus on the information needed to effectively decision-make and plan gas turbine system use for particular applications, taking into consideration not only operational requirements but long-term life-cycle costs in upkeep, repair and future use.With concise, easily digestible overviews of all important theoretical bases and a practical focus throughout, Gas Turbines is an ideal handbook for those new to the field or in the early stages of their career, as well as more experienced engineers looking for a reliable, one-stop reference that covers the breadth of the field. - Covers installation, maintenance, manufacturer's specifications, performance criteria and future trends, offering a rounded view of the area that takes in technical detail as well as well as industry economics and outlook - Updated with the latest industry developments, including new emission and efficiency regulations and their impact on gas turbine technology - Over 300 pages of new/revised content, including new sections on microturbines, non-conventional fuel sources for microturbines, emissions, major developments in aircraft engines, use of coal gas and superheated steam, and new case histories throughout highlighting component improvements in all systems and sub-systems
Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364
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Book Description
The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Author: T. W. Lee
Publisher: John Wiley & Sons
ISBN: 1118534875
Category : Technology & Engineering
Languages : en
Pages : 316
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Book Description
Aerospace propulsion devices embody some of the most advanced technologies, ranging from materials, fluid control, and heat transfer and combustion. In order to maximize the performance, sophisticated testing and computer simulation tools are developed and used. Aerospace Propulsion comprehensively covers the mechanics and thermal-fluid aspects of aerospace propulsion, starting from the fundamental principles, and covering applications to gas-turbine and space propulsion (rocket) systems. It presents modern analytical methods using MATLAB and other advanced software and includes essential elements of both gas-turbine and rocket propulsion systems. Gas turbine coverage includes thermodynamic analysis, turbine components, diffusers, compressors, turbines, nozzles, compressor-turbine matching, combustors and afterburners. Rocket coverage includes chemical rockets, electrical rockets, nuclear and solar sail. Key features: Both gas-turbine and rocket propulsion covered in a single volume Presents modern analytical methods and examples Combines fundamentals and applications, including space applications Accompanied by a website containing MATLAB examples, problem sets and solutions Aerospace Propulsion is a comprehensive textbook for senior undergraduate graduate and aerospace propulsion courses, and is also an excellent reference for researchers and practicing engineers working in this area.
