"Sinopsis" puede pertenecer a otra edición de este libro.
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. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained.
Fundamentals of Aircraft and Rocket Propulsion provides information about and analyses of:
Aimed at graduate and final-year 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. 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.
Prof. Ahmed F. El-Sayed was a Senior Engineer for the Egyptian Airline EGYPTAIR, for 10 years, working in in maintenance, technical inspection, and R&D departments as well as the engine overhaul shop. He has worked as a researcher in corporate projects with Westinghouse (USA) and Rolls Royce (UK), and taught propulsion and turbomachinery courses in several universities in Egypt, the USA, and Libya.
"Sobre este título" puede pertenecer a otra edición de este libro.
Gastos de envío:
EUR 23,00
De Alemania a Estados Unidos de America
Descripción Buch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained.Fundamentals of Aircraft and Rocket Propulsionprovides 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 non-chemical rocket engines;conceptual design of modular rocket engines (combustor, nozzle and turbopumps); andconceptual design of different modules of aero-engines in their design and off-design state.Aimed at graduate and final-year 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. 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. 1032 pp. Englisch. Nº de ref. del artículo: 9781447167945
Descripción Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. More than 100 worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration for the student readerMore than 200 illustrations plus 100 photos support and illustrate the text, giving readers. Nº de ref. del artículo: 109507115
Descripción Condición: New. Nº de ref. del artículo: 26304639-n
Descripción Condición: New. Nº de ref. del artículo: 26304639-n
Descripción Condición: New. Book is in NEW condition. Nº de ref. del artículo: 1447167945-2-1
Descripción Condición: New. New! This book is in the same immaculate condition as when it was published. Nº de ref. del artículo: 353-1447167945-new
Descripción Buch. Condición: Neu. Druck auf Anfrage Neuware - Printed after ordering - 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. The text classifies engines powering aircraft and single/multi-stage rockets, and derives performance parameters for both from basic aerodynamics and thermodynamics laws. Each type of engine is analyzed for optimum performance goals, and mission-appropriate engines selection is explained.Fundamentals of Aircraft and Rocket Propulsionprovides 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 non-chemical rocket engines;conceptual design of modular rocket engines (combustor, nozzle and turbopumps); andconceptual design of different modules of aero-engines in their design and off-design state.Aimed at graduate and final-year 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. 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. Nº de ref. del artículo: 9781447167945
Descripción Condición: Brand New. New. US edition. Expediting shipping for all USA and Europe orders excluding PO Box. Excellent Customer Service. Nº de ref. del artículo: ABEOCT23-133910
Descripción Condición: New. Brand New Original US Edition.We Ship to PO BOX Address also. EXPEDITED shipping option also available for faster delivery.This item may ship from the US or other locations in India depending on your location and availability. Nº de ref. del artículo: ABTR-84083
Descripción Hardcover. Condición: new. New Copy. Customer Service Guaranteed. Nº de ref. del artículo: think1447167945