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Product Description: Outstanding amongst the cars that raced at the Motor Course at Brooklands, principally in the 1920s, were the giant aero-engined "specials". The sight and sound of these fiery monsters roaring dangerously round the steeply banked outer circuit near Weybridge in Surrey, thrilled a generation...read more

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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.

Product Description: This is an example product description.

638 pages, with some illustrations.

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Briefly traces the history of the Cessna company, describes the performance and specifications of each model, and offers advice on buying a used plane

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Product Description: This is the history, development and application of piston aero engines, from those used in the Wright Brother's pioneering aircraft at the beginning of the century to the small machines which power microlights today. In addition to listing the various engines it also discusses the principles involved in the working and evolution of these power plants...read more

Product Description: There have been impressive achievements in the last few years in the technologies associated with turboramjets and other combined cycle engines. These technologies, including their thermal management and integration with the vehicle, are the principal concerns of this volume...read more

Looks at technological developments which will shape the future of air and space travel, including ultralight aircraft, antimatter, and high-energy laser propulsion systems

This revised edition provides an understanding of the basic physical, chemical, and aerodynamic processes associated with gas turbine combustion and their relevance and application to combustor performance and design. Also introduced are many new concepts for ultra-low emissions combustors, and new advances in fuel preparation and liner wall-cooling techniques for their success. It details advanced and practical approaches to combustor design for the clean burning of alternative liquid fuels derived form oil shades, tar sands, and coal. (view table of contents)

Recruited by General Claire Chennault to service the engines of the 'Flying Tigers,' the German-born aeronautical engineer recounts his service in the OSS and his thirty-one years at G.E., where he engineered the design and production of jet engines

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