Experimental study on supersonic combustion phenomena with a cavity-base fuel injection

E. Jeong; S. O'Byrne; I. S. Jeung; A. F.P. Houwing

Experimental study on supersonic combustion phenomena with a cavity-base fuel injection

E. Jeong^*, S. O'Byrne, I. S. Jeung, A. F.P. Houwing

^*Corresponding author for this work

The Australian National University

Research output: Contribution to conference › Paper › peer-review

Abstract

The model cavity scramjet experiments are carried out using T3 free-piston shock tunnel. Upstream hydrogen fuel is injected before the cavity with different injection pressure. OH Planar laser-induced fluorescence is used to investigate the combustion zone. Main combustion region is a mixing layer which is between air and fuel. Also high OH fluorescence signal is appeared in the shear layer above the cavity in high equivalence ratio. From the OH signal in the cavity, this fuel injection system can be a role as a flame-holder.

Original language	English
Publication status	Published - 2007
Event	6th Asia-Pacific Conference on Combustion, ASPACC 2007 - Nagoya, Japan Duration: 20 May 2007 → 23 May 2007

Conference

Conference	6th Asia-Pacific Conference on Combustion, ASPACC 2007
Country/Territory	Japan
City	Nagoya
Period	20/05/07 → 23/05/07

Cite this

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title = "Experimental study on supersonic combustion phenomena with a cavity-base fuel injection",

abstract = "The model cavity scramjet experiments are carried out using T3 free-piston shock tunnel. Upstream hydrogen fuel is injected before the cavity with different injection pressure. OH Planar laser-induced fluorescence is used to investigate the combustion zone. Main combustion region is a mixing layer which is between air and fuel. Also high OH fluorescence signal is appeared in the shear layer above the cavity in high equivalence ratio. From the OH signal in the cavity, this fuel injection system can be a role as a flame-holder.",

author = "E. Jeong and S. O'Byrne and Jeung, {I. S.} and Houwing, {A. F.P.}",

year = "2007",

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TY - CONF

T1 - Experimental study on supersonic combustion phenomena with a cavity-base fuel injection

AU - Jeong, E.

AU - O'Byrne, S.

AU - Jeung, I. S.

AU - Houwing, A. F.P.

PY - 2007

Y1 - 2007

N2 - The model cavity scramjet experiments are carried out using T3 free-piston shock tunnel. Upstream hydrogen fuel is injected before the cavity with different injection pressure. OH Planar laser-induced fluorescence is used to investigate the combustion zone. Main combustion region is a mixing layer which is between air and fuel. Also high OH fluorescence signal is appeared in the shear layer above the cavity in high equivalence ratio. From the OH signal in the cavity, this fuel injection system can be a role as a flame-holder.

AB - The model cavity scramjet experiments are carried out using T3 free-piston shock tunnel. Upstream hydrogen fuel is injected before the cavity with different injection pressure. OH Planar laser-induced fluorescence is used to investigate the combustion zone. Main combustion region is a mixing layer which is between air and fuel. Also high OH fluorescence signal is appeared in the shear layer above the cavity in high equivalence ratio. From the OH signal in the cavity, this fuel injection system can be a role as a flame-holder.

UR - http://www.scopus.com/inward/record.url?scp=85126497518&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:85126497518

T2 - 6th Asia-Pacific Conference on Combustion, ASPACC 2007

Y2 - 20 May 2007 through 23 May 2007

ER -

Experimental study on supersonic combustion phenomena with a cavity-base fuel injection

Abstract

Conference

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