Format:
Online-Ressource (1 online resource (270 p.))
,
digital, PDF file(s).
Edition:
Online-Ausg.
ISBN:
9780511627019
Series Statement:
Cambridge Aerospace Series no. 25
Content:
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.
Note:
Title from publishers bibliographic system (viewed on 18 Feb 2013)
Additional Edition:
ISBN 9780521838153
Additional Edition:
Druckausg. Segal, Corin, 1952 - The scramjet engine Cambridge [u.a.] : Cambridge Univ. Press, 2009 ISBN 9780521838153
Additional Edition:
ISBN 0521838150
Language:
English
Subjects:
Engineering
Keywords:
Überschallstaustrahltriebwerk
DOI:
10.1017/CBO9780511627019
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