Upstream porthole injection in a 2-D scramjet model

Gardner, A. D., Paull, A. and McIntyre, T. J. (2002) Upstream porthole injection in a 2-D scramjet model. Shock Waves, 11 5: 369-375. doi:10.1007/s001930200120


Author Gardner, A. D.
Paull, A.
McIntyre, T. J.
Title Upstream porthole injection in a 2-D scramjet model
Journal name Shock Waves   Check publisher's open access policy
ISSN 0938-1287
1432-2153
Publication date 2002-04-01
Sub-type Article (original research)
DOI 10.1007/s001930200120
Volume 11
Issue 5
Start page 369
End page 375
Total pages 7
Editor H. Groenig
Place of publication Berlin, Germany
Publisher Springer Verlag
Language eng
Subject C1
290299 Aerospace Engineering not elsewhere classified
780102 Physical sciences
Abstract Injection from portholes upstream of the combustion chamber was investigated as a method of delivering fuel into a scramjet. This method reduces the viscous drag on a model by allowing a reduction in the length of the combustion chamber. At experimental enthalpies of 3.0 MJ/kg in the T4 shock tunnel, there was no evidence of combustion in the intake, either by shadowgraph or pressure measurements. Combustion was observed in the combustion chamber. A theoretical extension of these results is made to a hot wall scenario.
Keyword Mechanics
Scramjet
Upstream Injection
Porthole Injection
Shock Tunnel
Combustion
Q-Index Code C1

Document type: Journal Article
Sub-type: Article (original research)
Collections: Excellence in Research Australia (ERA) - Collection
School of Mechanical & Mining Engineering Publications
 
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Citation counts: TR Web of Science Citation Count  Cited 13 times in Thomson Reuters Web of Science Article | Citations
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Created: Wed, 15 Aug 2007, 03:54:46 EST