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Aerothermodynamics of Aircraft Engine Components by Gordon C. Oates Pdf
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.
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
Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).
Whilst most contemporary books in the aerospace propulsion field are dedicated primarily to gas turbine engines, there is often little or no coverage of other propulsion systems and devices such as propeller and helicopter rotors or detailed attention to rocket engines. By taking a wider viewpoint, Powered Flight - The Engineering of Aerospace Propulsion aims to provide a broader context, allowing observations and comparisons to be made across systems that are overlooked by focusing on a single aspect alone. The physics and history of aerospace propulsion are built on step-by-step, coupled with the development of an appreciation for the mathematics involved in the science and engineering of propulsion. Combining the author’s experience as a researcher, an industry professional and a lecturer in graduate and undergraduate aerospace engineering, Powered Flight - The Engineering of Aerospace Propulsion covers its subject matter both theoretically and with an awareness of the practicalities of the industry. To ensure that the content is clear, representative but also interesting the text is complimented by a range of relevant graphs and photographs including representative engineering, in addition to several propeller performance charts. These items provide excellent reference and support materials for graduate and undergraduate projects and exercises. Students in the field of aerospace engineering will find that Powered Flight - The Engineering of Aerospace Propulsion supports their studies from the introductory stage and throughout more intensive follow-on studies.
Building on the success of its predecessor, Handbook of Turbomachinery, Second Edition presents new material on advances in fluid mechanics of turbomachinery, high-speed, rotating, and transient experiments, cooling challenges for constantly increasing gas temperatures, advanced experimental heat transfer and cooling effectiveness techniques, and propagation of wake and pressure disturbances. Completely revised and updated, it offers updated chapters on compressor design, rotor dynamics, and hydraulic turbines and features six new chapters on topics such as aerodynamic instability, flutter prediction, blade modeling in steam turbines, multidisciplinary design optimization.
Aircraft Landing Gear Design by Norman S. Currey Pdf
This is the only book available today that covers military and commercial aircraft landing gear design. It is a comprehensive text that will lead students and engineers from the initial concepts of landing gear design through final detail design. The book provides a vital link in landing gear design technology from historical practices to modern design trends, and it considers the necessary airfield interface with landing gear design. The text is backed up by calculations, specifications, references, working examples.
Future Propulsion Systems and Energy Sources in Sustainable Aviation by Saeed Farokhi Pdf
A comprehensive review of the science and engineering behind future propulsion systems and energy sources in sustainable aviation Future Propulsion Systems and Energy Sources in Sustainable Aviation is a comprehensive reference that offers a review of the science and engineering principles that underpin the concepts of propulsion systems and energy sources in sustainable air transportation. The author, a noted expert in the field, examines the impact of air transportation on the environment and reviews alternative jet fuels, hybrid-electric and nuclear propulsion and power. He also explores modern propulsion for transonic and supersonic-hypersonic aircraft and the impact of propulsion on aircraft design. Climate change is the main driver for the new technology development in sustainable air transportation. The book contains critical review of gas turbine propulsion and aircraft aerodynamics; followed by an insightful presentation of the aviation impact on environment. Future fuels and energy sources are introduced in a separate chapter. Promising technologies in propulsion and energy sources are identified leading to pathways to sustainable aviation. To facilitate the utility of the subject, the book is accompanied by a website that contains illustrations, and equation files. This important book: Contains a comprehensive reference to the science and engineering behind propulsion and power in sustainable air transportation Examines the impact of air transportation on the environment Covers alternative jet fuels and hybrid-electric propulsion and power Discusses modern propulsion for transonic, supersonic and hypersonic aircraft Examines the impact of propulsion system integration on aircraft design Written for engineers, graduate and senior undergraduate students in mechanical and aerospace engineering, Future Propulsion Systems and Energy Sources in Sustainable Aviation explores the future of aviation with a guide to sustainable air transportation that includes alternative jet fuels, hybrid-electric propulsion, all-electric and nuclear propulsion.
Aircraft Engines and Gas Turbines by Jack L. Kerrebrock Pdf
This text on aircraft engines and turbines presents the engine as a complete system, with emphasis on the performance of the engine and its dependence on the major design parameters and physical limitations. The system is described at three levels, first by ideal cycle and analysis, then by more refined cycle analysis, and finally as an assembly of components. At this last level the behavior of each component is described in terms of the fluid mechanical processes, chemistry, and mechanical stresses which limit its performance. The factors which control the engine's noise production and chemical pollutant emission are also addressed. Special emphasis is placed on the past, present and likely future evolution of the aircraft engine in response to the requirements for better performance, lower noise and reduced pollution. A clear appreciation of all these factors requires basic preparation in fluid mechanics, solid mechanics, chemistry and thermodynamics. Clearly, no single text can review all these: an undergraduate preparation is assumes. The application of these several disciplines to a complex system should help the students to appreciate their interrelationship as well as to understand the engine itself. With the rapid advances that have occurred since the large-scale introduction of gas turbine power plants into military aircraft in the 1950s and into commercial aircraft in the 1960s, it has become necessary to make a clear understanding of the characteristics of these devices accessible at the undergraduate level. Such understanding is essential both for entrance to professional work in industry and as preparation for graduate study. The book will also prove valuable as a reference for engineers already working in the field. Although the main focus is on aircraft propulsion, the text will also be useful to those interested in automotive and stationary applications of gas turbines. These applications are treated at the level of cycle analysis, and much of the discussion of components is directly applicable. The eleven chapters of the text take up basic definitions and concepts, trends in ideal cycle analysis, quantitative cycle analysis, nonrotating components, compressors, turbines, the structure of turbomachinery, component matching and engine performance, aircraft engine noise, hypersonic engines, and propulsion systems analysis. Each chapter includes problems and references.
