The renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both theoretical and experimental research. The focus is on the phenomena that dictate the thermo-aerodynamic processes encountered in the scramjet engine, including component analyses and flowpath considerations; fundamental theoretical topics related to internal flow with chemical reactions and non-equilibrium effects, high-temperature gas dynamics, and hypersonic effects are included. Cycle and component analyses are further described, followed by flowpath examination. Finally, the book reviews experimental and theoretical capabilities and describes ground testing facilities and computational fluid dynamics facilities developed for the study of time-accurate, high-temperature aerodynamics.
"synopsis" may belong to another edition of this title.
Corin Segal has been a member of the faculty at the University of Florida in the Mechanical and Aerospace Department since completing his Ph.D. at the University of Virginia. He leads research in the Combustion and Propulsion Laboratory. Prior to his graduate studies Dr Segal spent over eleven years in the aerospace industry as a senior aerodynamicist, project manager, and as a leader of the technical bureau. His current research covers a range of topics including mixing and combustion in high speed flows, supercritical mixing, high pressure combustion and cavitation. Results of his group's research have appeared in national and international publications. He is an associate editor of the AIAA Journal of Propulsion and Power and an Associate Fellow in the AIAA.
"About this title" may belong to another edition of this title.
FREE shipping within United Kingdom
Destination, rates & speeds£ 27.34 shipping from Spain to United Kingdom
Destination, rates & speedsSeller: WYEMART LIMITED, HEREFORD, United Kingdom
Hardcover. Condition: Very Good. Seller Inventory # mon0000195543
Quantity: 3 available
Seller: Llibreria Hispano Americana, Barcelona, B, Spain
Encuadernación de tapa dura. Condition: Nuevo. Dust Jacket Condition: Nuevo. 1ª Edición. Seller Inventory # ABE-1734446989705
Quantity: 1 available
Seller: Toscana Books, AUSTIN, TX, U.S.A.
Hardcover. Condition: new. Excellent Condition.Excels in customer satisfaction, prompt replies, and quality checks. Seller Inventory # Scanned0521838150
Quantity: 1 available
Seller: Feldman's Books, Menlo Park, CA, U.S.A.
Hardcover. Condition: Very Fine. 1st Edition. No Markings. Seller Inventory # 045474
Quantity: 1 available
Seller: Ria Christie Collections, Uxbridge, United Kingdom
Condition: New. In. Seller Inventory # ria9780521838153_new
Quantity: Over 20 available
Seller: THE SAINT BOOKSTORE, Southport, United Kingdom
Hardback. Condition: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days 720. Seller Inventory # C9780521838153
Quantity: Over 20 available
Seller: CitiRetail, Stevenage, United Kingdom
Hardcover. Condition: new. Hardcover. The renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both theoretical and experimental research. The focus is on the phenomena that dictate the thermo-aerodynamic processes encountered in the scramjet engine, including component analyses and flowpath considerations; fundamental theoretical topics related to internal flow with chemical reactions and non-equilibrium effects, high-temperature gas dynamics, and hypersonic effects are included. Cycle and component analyses are further described, followed by flowpath examination. Finally, the book reviews experimental and theoretical capabilities and describes ground testing facilities and computational fluid dynamics facilities developed for the study of time-accurate, high-temperature aerodynamics. The renewed interest in high-speed propulsion has lead to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. Corin Segal, a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both the theoretical and experimental research. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Seller Inventory # 9780521838153
Quantity: 1 available
Seller: Revaluation Books, Exeter, United Kingdom
Hardcover. Condition: Brand New. 1st edition. 253 pages. 10.00x7.00x1.00 inches. In Stock. This item is printed on demand. Seller Inventory # __0521838150
Quantity: 1 available
Seller: California Books, Miami, FL, U.S.A.
Condition: New. Seller Inventory # I-9780521838153
Quantity: Over 20 available
Seller: moluna, Greven, Germany
Gebunden. Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. The renewed interest in high-speed propulsion has lead to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. Corin Segal, a leading researcher, describes the processes and characteristics of . Seller Inventory # 446949765
Quantity: Over 20 available