Aircraft Propulsion, 2nd Edition [Book]Description Winner of the Summerfield Book Award! The text presents a complete and realistic aircraft engine design experience. From the request for proposal for a new aircraft to the final engine layout, the book provides the concepts and procedures required for the entire process. It is a significantly expanded and modernized version of the best-selling first edition that emphasizes recent developments impacting engine design such as theta break-throttle ratio, life management, controls, and stealth. The key steps of the process are detailed in 10 chapters that encompass aircraft constraint analysis, aircraft mission analysis, engine parametric design point analysis, engine performance off-design analysis, engine installation drag and sizing, and the design of inlets, fans, compressors, main combustors, turbines, afterburners, and exhaust nozzles. The AEDsys software that accompanies the text provides comprehensive computational support for every design step. The software has been carefully integrated with the text to enhance both the learning process and productivity, and allows effortless transfer between British engineering and SI units.
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Aircraft Engines and Gas Turbines, Second Edition
New edition of the successful textbook updated to include new material on UAVs, design guidelines in aircraft engine component systems and additional end of chapter problems. Aircraft Propulsion, Second Edition follows the successful first edition textbook with comprehensive treatment of the subjects in airbreathing propulsion, from the basic principles to more advanced treatments in engine components and system integration. This new edition has been extensively updated to include a number of new and important topics. Propeller theory is added to the presentation of turboprop engines. New material on drop-in biofuels and design for sustainability is added to refl ect the FAA's Vision. In addition, the design guidelines in aircraft engine components are expanded to make the book user friendly for engine designers.
Aircraft Engines and Gas Turbines is widely used as a text in the United States and abroad, and has also become a standard reference for professionals in the aircraft engine industry. Unique in treating the engine as a complete system at increasing levels of sophistication, it covers all types of modern aircraft engines, including turbojets, turbofans, and turboprops, and also discusses hypersonic propulsion systems of the future. Performance is described in terms of the fluid dynamic and thermodynamic limits on the behavior of the principal components: inlets, compressors, combustors, turbines, and nozzles. Environmental factors such as atmospheric pollution and noise are treated along with performance. This new edition has been substantially revised to include more complete and up-to-date coverage of compressors, turbines, and combustion systems, and to introduce current research directions.
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Flight Physics pp Cite as. Aircraft rely on the reaction principle much more than ground vehicles. They almost exclusively use chemical energy released by combustion of liquid fuels or propellants. Air breathing engines use atmospheric air for generating power by combustion and obtain their thrust by reaction to the backward acceleration of ambient air or exhaust gases. Rocket engines are nonairbreathers carrying their propellant internally; they will only be mentioned superficially in this tbook.
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