Theory Of Aerospace Propulsion (Hb) Hardcover

Theory of Aerospace Propulsion offers comprehensive coverage of aerospace propulsion systems, including propellers, nuclear rockets, and space propulsion. The book provides an in-depth, quantitative analysis of jet propulsion engine components, equipping readers with the tools needed to evaluate and match components for optimal system performance. It includes worked examples and chapter-end exercises to help readers practice analysis, preliminary design, and systems integration. The book teaches how to apply fluid mechanics and thermodynamics principles to analyze aircraft engines, understand common gas turbine propulsion systems, and determine the suitability of each system. It also covers conducting system studies for specific flight conditions, performing preliminary aerothermal design of turbomachinery components, and optimizing designs for both conventional and unconventional missions. Organized into 15 chapters, the book addresses topics such as idealized flow machines, quasi-one-dimensional flow equations, jet engine cycle analysis, combustion chambers for airbreathing engines, nozzles and inlets, turbomachinery, blade element analysis, turbine engine performance and integration, propellers, liquid and solid propellant rockets, nuclear rockets, space propulsion, and propulsion for high-speed flight. This resource is ideal for aerospace and mechanical engineers specializing in gas turbines, turbomachinery, aircraft propulsion, and rocket propulsion. It is also a valuable text for undergraduate and graduate students studying aerospace propulsion or turbomachinery. Early chapters on cycle analysis provide a systems perspective, offering context for later sections on turbomachinery and components. The book’s broader scope, including topics like propellers and nuclear rockets, allows for the analysis and design of a wide range of propulsion systems.