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Fundamentals of Aircraft and Rocket Propulsion,Used
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This book provides a comprehensive basicstoadvanced course in an aerothermal science vital to the design of engines for either type of craft. The text classifies engines powering aircraft and single/multistage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and missionappropriate 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 nonchemical rocket engines; conceptual design of modular rocket engines (combustor, nozzle and turbopumps); and conceptual design of different modules of aeroengines in their design and offdesign state.Aimed at graduate and finalyear 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.Endofchapter exercises are provided, increasing the books value to students.
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This product may contain chemicals known to the State of California to cause cancer, birth defects, or other reproductive harm.
For more information, please visit www.P65Warnings.ca.gov.