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Author : Gordon C. Oates
Publisher : AIAA
Page : 476 pages
File Size : 40,6 Mb
Release : 1997
Category : Aerothermodynamics
ISBN : 1600860060
Author : Gordon C. Oates
Publisher : Unknown
Page : 830 pages
File Size : 53,9 Mb
Release : 1978
Category : Aerothermodynamics
ISBN : CORNELL:31924004744201
Author : F. Whittle
Publisher : Elsevier
Page : 276 pages
File Size : 41,7 Mb
Release : 2013-10-22
Category : Technology & Engineering
ISBN : 9781483293219
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
Page : 544 pages
File Size : 46,9 Mb
Release : 1989
Category : Aircraft gas-turbines
ISBN : 1600860214
Author : Jack D. Mattingly,Keith M. Boyer,Hans von Ohain
Publisher : American Institute of Aeronautics and Astronautics Incorporated
Page : 0 pages
File Size : 55,6 Mb
Release : 2016
Category : Aircraft gas-turbines
ISBN : 1624103715
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 : Paul G. A. Cizmas
Publisher : Unknown
Page : 488 pages
File Size : 52,8 Mb
Release : 2021-11-24
Category : Science
ISBN : 9781108575591
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 : Gordon C. Oates
Publisher : AIAA
Page : 568 pages
File Size : 49,6 Mb
Release : 1985
Category : Aerothermodynamics
ISBN : 1600860052
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 : Unknown
Page : 128 pages
File Size : 54,7 Mb
Release : 1982
Category : Electronic
ISBN : OCLC:861385685
Author : Frank Whittle
Publisher : Pergamon
Page : 261 pages
File Size : 43,8 Mb
Release : 1981-01-01
Category : Aircraft gas-turbines
ISBN : 0080267181
Author : George P. Sutton,Oscar Biblarz
Publisher : John Wiley & Sons
Page : 772 pages
File Size : 52,8 Mb
Release : 2001
Category : Science
ISBN : 0471326429
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 : United States. National Bureau of Standards
Publisher : Unknown
Page : 62 pages
File Size : 52,9 Mb
Release : 1947
Category : Gas-turbines
ISBN : UOM:39015021092617
Author : DP Mishra
Publisher : CRC Press
Page : 462 pages
File Size : 44,9 Mb
Release : 2017-07-20
Category : Technology & Engineering
ISBN : 9781498785365
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 : G.W. Meetham
Publisher : Springer Science & Business Media
Page : 311 pages
File Size : 46,7 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9789400981119
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 : Jack D. Mattingly
Publisher : McGraw-Hill Science, Engineering & Mathematics
Page : 1032 pages
File Size : 54,8 Mb
Release : 1996
Category : Aircraft gas-turbines
ISBN : UOM:39076002648405
Designed to provide an introduction to the fundamentals of gas turbine engines and jet propulsion for aerospace or mechanical engineers. The book contains sufficient material for two sequential courses in propulsion, a course in jet propulsion and a gas turbine engine components course.
Author : Ahmed F. El-Sayed
Publisher : CRC Press
Page : 1448 pages
File Size : 41,8 Mb
Release : 2017-07-06
Category : Science
ISBN : 9781466595170
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.