Modeling of a Feedback Mechanism in Supersonic Deep-Cavity Flows

被引:16
作者
Handa, Taro [1 ]
Miyachi, Hiroaki [2 ]
Kakuno, Hatsuki [3 ]
Ozaki, Takaya [3 ]
Maruyama, Shinji [1 ]
机构
[1] Kyushu Univ, Dept Energy & Environm Engn, Kasuga, Fukuoka 8168580, Japan
[2] Mitsubishi Heavy Ind Co Ltd, Power Syst Plant Engn Dept, Takasago, Hyogo 6768686, Japan
[3] Nippon Steel & Sumikin Engn, Plant & Machinery Div, Kitakyushu, Fukuoka 8048505, Japan
关键词
PRESSURE OSCILLATIONS; RECTANGULAR CAVITIES;
D O I
10.2514/1.J053184
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, a feedback mechanism for supersonic deep-cavity flows is modeled. The model is developed on the basis of previous flow visualization results. In this model, two pressure waves play an important role in the feedback mechanism; one wave is generated at the trailing edge of the cavity owing to the motion of the shear layer, and the other wave is generated as a result of the third reflection of the former wave at the cavity bottom. The constants in the model are determined using the flow visualization results. The frequencies calculated in the model agree well with the dominant frequencies observed in experiments; in particular, the feedback mechanism responsible for deep-cavity-induced pressure oscillation is successfully clarified.
引用
收藏
页码:420 / 425
页数:6
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