DocumentCode
1046024
Title
Hypersonic flight [scramjet aircraft propulsion]
Author
Guizzo, Erico
Volume
41
Issue
1
fYear
2004
Firstpage
66
Abstract
Current turbojet engines cannot propel an aircraft to hypersonic speeds -their spinning shafts and compressors would simply collapse. To solve this problem, groups in the United States, Japan, Australia, and other countries are working on a propulsion system that burns fuel combined with air flowing at supersonic speeds through the engine, which is essentially a metallic funnel, with no moving parts. These so-called supersonic combustion ramjet (scramjet) engines, outlined in this article, could in theory propel an aircraft to Mach 10 and eventually even more.
Keywords
hypersonic flow; jet engines; supersonic flow; fuel/air burning propulsion system; hypersonic speeds; metallic funnel; no moving parts; scramjet aircraft propulsion; supersonic combustion ramjet; turbojet engines; Aircraft propulsion; Australia; Combustion; Compressors; Engines; Fuels; Shafts; Spinning;
fLanguage
English
Journal_Title
Spectrum, IEEE
Publisher
ieee
ISSN
0018-9235
Type
jour
DOI
10.1109/MSPEC.2004.1317885
Filename
1317885
Link To Document