Numerical study on dynamic characteristics for sharp opening procedure of boundary-layer suction slot

被引:4
|
作者
He, Yubao [1 ]
Yin, Hang [1 ]
Huang, Hongyan [1 ]
Yu, Daren [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China
基金
中国国家自然科学基金;
关键词
Shock train; Boundary layer; Inlet unstart; Suction slot; Hypersonic inlet; INLET; SIMULATIONS; COMBUSTION; MODEL;
D O I
10.1016/j.actaastro.2017.04.019
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Based on the sharp forward of shock train and taking the forthcoming unstart for a background, the dynamic characteristics for sharp opening procedure of boundary-layer suction slot are investigated numerically using the dynamic mesh technique. Results indicate that the climbing path of shock train with the complex background waves exhibits a sharp and slow forward state at different time. The compression waves in the primary shock sweep the trailing edge of the separation bubble, and the recirculation within the shock train is communicated with the separation bubble, which reveals that the flow is in a critical state and is about to be unstart at the subsequent time. Furthermore, the dynamic pattern for sharp opening procedure of boundary layer suction slot can be classified into four distinct stages, namely, the formation of the jet plume without suction mass loss, the formation of the barrier shock with suction mass loss characterized by gradient increase and subsequent two oscillations, the evolution of the barrier shock and jet plume with suction mass loss that ramps up via a series of discrete step increases, and the formation of the stable structure accompanied by the linear suction mass loss.
引用
收藏
页码:145 / 156
页数:12
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