The supersonic combustion ramjet engine, 'Scramjet', is a potential means of powering both hypersonic aircraft and for satellite boosting. It is theoretically superior to the present rocket engine, however further 'Scramjet' research is required. The tailored interface hypersonic shock tunnel provides a means by which the conditions in the scramjet combustion chamber can be simulated for short periods of time. For maximum testing times tailored operation of the tunnel is essential. (Author)
The Shock Tunnel as a Supersonic Combustion Test Facility
1966
14 pages
Report
No indication
English
Shock tunnel as supersonic combustion test facility
Engineering Index Backfile | 1966
|Investigations on supersonic combustion in a combustion-driven shock tunnel
Online Contents | 2012
|Investigations on supersonic combustion in a combustion-driven shock tunnel
SAGE Publications | 2012
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