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Author : Ronald D. Flack
Publisher : Cambridge University Press
Page : 739 pages
File Size : 47,7 Mb
Release : 2023-07-31
Category : Technology & Engineering
ISBN : 9781316517369
A revised second edition of this introductory text on air-breathing jet propulsion, emphasizing jet engines and gas turbines.
Author : Ronald D. Flack
Publisher : Cambridge University Press
Page : 128 pages
File Size : 45,6 Mb
Release : 2005-04-25
Category : Technology & Engineering
ISBN : 9781107393882
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 : Ronald Flack
Publisher : Unknown
Page : 660 pages
File Size : 45,6 Mb
Release : 2005
Category : Electronic
ISBN : OCLC:1137348589
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 : S. Can Gülen
Publisher : Cambridge University Press
Page : 735 pages
File Size : 40,6 Mb
Release : 2019-02-14
Category : Science
ISBN : 9781108416658
Everything you wanted to know about industrial gas turbines for electric power generation in one source with hard-to-find, hands-on technical information.
Author : Otis E. Lancaster
Publisher : Princeton University Press
Page : 842 pages
File Size : 55,6 Mb
Release : 2015-12-08
Category : Science
ISBN : 9781400877911
Volume XII of the High Speed Aerodynamics and Jet Propulsion series. Partial Contents: Historical development of jet propulsion; basic principles of jet propulsion; analyses of the various types of jet propulsion engines including the turbojet, the turboprop, the ramjet, and intermittent jets, as well as solid and liquid propellant rocket engines and the ramrocket. Another section deals with jet driven rotors. The final sections discuss the use of atomic energy in jet propulsion and the future prospects of jet propulsion. Originally published in 1959. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Paul W. Gill,James H. Smith,Eugene J. Ziurys
Publisher : Unknown
Page : 602 pages
File Size : 45,7 Mb
Release : 1959
Category : Internal combustion engines
ISBN : CORNELL:31924004266288
Author : N. A. Cumpsty
Publisher : Cambridge University Press
Page : 326 pages
File Size : 54,9 Mb
Release : 2003-08-14
Category : Technology & Engineering
ISBN : 0521541441
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.
Author : Paul W. Gill
Publisher : Unknown
Page : 248 pages
File Size : 46,9 Mb
Release : 1952
Category : Gas-turbines
ISBN : CORNELL:31924003951302
Author : Ahmed F. El-Sayed
Publisher : Springer
Page : 1010 pages
File Size : 42,6 Mb
Release : 2016-05-25
Category : Technology & Engineering
ISBN : 9781447167969
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 : Corin Segal
Publisher : Cambridge University Press
Page : 271 pages
File Size : 48,8 Mb
Release : 2009-06-22
Category : Technology & Engineering
ISBN : 9780521838153
Demand for high-speed propulsion has renewed development of the supersonic combustion ramjet engine (Scramjet engine) for hypersonic flight applications.
Author : V. Babu
Publisher : Springer Nature
Page : 164 pages
File Size : 44,9 Mb
Release : 2021-08-25
Category : Technology & Engineering
ISBN : 9783030799458
p="" This highly informative book offers a comprehensive overview of the fundamentals of propulsion. The book focuses on foundational topics in propulsion, namely gas dynamics, turbomachinery, and combustion to more complex subjects such as practical design aspects of aircraft engines and thermodynamic aspects and analysis. It also includes pedagogical aspects such as end-of-chapter problems and worked examples to augment learning and self-testing. This book is a useful reference for students in the area of mechanical and aerospace engineering. Also, scientists and engineers working in the areas of aerospace propulsion and gas dynamics find this book a valuable addition. ^
Author : Walter John Hesse,Nicholas V. S. Mumford
Publisher : Unknown
Page : 648 pages
File Size : 48,6 Mb
Release : 1964
Category : Jet propulsion
ISBN : UOM:39015058304711
Author : Kiruba Haran,Nateri Madavan,Tim C. O'Connell
Publisher : Cambridge University Press
Page : 317 pages
File Size : 52,6 Mb
Release : 2022-05-26
Category : Business & Economics
ISBN : 9781108419345
An ideal introduction to advances and outstanding challenges in large electric aircraft design, combining expertise from leading researchers.
Author : Stephen D. Heister,William E. Anderson,Timothée L. Pourpoint,R. Joseph Cassady
Publisher : Cambridge University Press
Page : 589 pages
File Size : 44,5 Mb
Release : 2019-02-07
Category : Science
ISBN : 9781108422277
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.
Author : Ahmed F. El-Sayed
Publisher : CRC Press
Page : 1184 pages
File Size : 42,6 Mb
Release : 2017-07-06
Category : Science
ISBN : 9781466595187
Aircraft Propulsion and Gas Turbine Engines, Second Edition builds upon the success of the book’s first edition, with the addition of three major topic areas: Piston Engines with integrated propeller coverage; Pump Technologies; and Rocket Propulsion. The rocket propulsion section extends the text’s coverage so that both Aerospace and Aeronautical topics can be studied and compared. Numerous updates have been made to reflect the latest advances in turbine engines, fuels, and combustion. The text is now divided into three parts, the first two devoted to air breathing engines, and the third covering non-air breathing or rocket engines.
