Flowfield studies of a diamond-shaped fuel injector in a supersonic flow

被引:15
|
作者
Kobayashi, Kan [1 ]
Bowersox, Rodney D. W.
Srinivasan, Ravichandra
Carter, Campbell D.
Hsu, Kuan-Yu
机构
[1] Japan Aerosp Explorat Agcy, Combined Propuls Res Grp, Combust & Control Sect, Kakuda, Miyagi 9811525, Japan
[2] Texas A&M Univ, College Stn, TX 77843 USA
[3] USAF, Res Lab, Aerosp Propuls Div, Wright Patterson AFB, OH 45433 USA
[4] Innovat Sci Soult Inc, Dayton, OH 45440 USA
关键词
D O I
10.2514/1.30000
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Studies were performed to characterize the flow structure and the mixing characteristics of a diamond-port flush-wall fuel injector at Mach 2.0 airflow. The goals were to examine the flow structure in the near-field region of the diamond- and circular-port injectors and to quantify the effects of igniter torch flow on the near-field How structure with and without torch gas. Planar laser-induced fluorescence was used to document the flow trajectories and the injector-barrel shock shape for the injectors. For the inert mixing studies, the flow was seeded with a nitric-oxide-trace probe molecule, whereas for the reacting experiments, naturally occurring hydroxyl was used. The present experiments confirmed recent computation results that implied that under certain conditions, a diamond-shaped injector port could be tailored to improve mixing and produce an additional secondary flow structure with gasdynamic flame-holding potential. It was also shown that an igniter torch system could be incorporated without adversely affecting the tailored flow structure.
引用
收藏
页码:1168 / 1176
页数:9
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