Hybrid-electric propulsion systems are tacitly dealt with, unless expressly provided otherwise. End-of-chapter exercises make this a valuable student resource, and the provision of a downloadable solutions manual will be of further benefit for course instructors. Manual control of aircraft propulsion solution This specification addresses airworthiness requirements for the design and installation of aircraft electrical propulsion systems.
Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained.įundamentals of Aircraft and Rocket Propulsion provides information about and analyses of: Unlike static PDF Aircraft Propulsion and Gas Turbine Engines solution manuals or printed answer keys, our experts show you how to solve each problem step-by. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. This book provides a comprehensive basics-to-advanced course in an aero-thermal science vital to the design of engines for either type of craft.