Research on diffusion characteristics of liquid jet effected by shock wave in supersonic high-enthalpy crossflow

被引:13
作者
Feng, Guangjun [1 ,2 ]
Zhang, Junlong [1 ,2 ]
Luan, Guowei [1 ,2 ]
Qiu, Hongchao [1 ,2 ]
Bao, Wen [1 ,2 ]
机构
[1] Harbin Inst Technol, Harbin 150001, Heilongjiang, Peoples R China
[2] Sch Energy Sci & Engn, Harbin, Peoples R China
基金
中国国家自然科学基金;
关键词
Diffusion and mixing characteristics; Liquid-kerosene; Shock wave; Evaporation; Supersonic combustor; MIXING ENHANCEMENT; COMBUSTION; KEROSENE; EVAPORATION; IGNITION; DRAG;
D O I
10.1016/j.ijheatmasstransfer.2024.125181
中图分类号
O414.1 [热力学];
学科分类号
摘要
The diffusion characteristics of liquid jets with phase transition under the action of shock waves in supersonic high-enthalpy crossflow were discussed in this paper. Numerous numerical simulations were carried out in high enthalpy inflow (Tt = 1680 K) under different shock wave intensity and injection parameter conditions. The Euler-Lagrangian method was employed to solve the gas-liquid two-phase flow coupling, and the evaporation, diffusion and mixing processes of kerosene were obtained. By analyzing simulation results, the influence and the mechanism of shock waves on enhanced kerosene mixing were revealed. The results show that increasing the shock wave intensity effectively improves the penetration and mixing of kerosene in general by changing the flow state and evaporation process. The penetration depth can be increased by up to 63.54 % in this paper. To balance the contradiction between total pressure loss and mixing efficiency, it is necessary to select an appropriate shock wave intensity. The enhanced diffusion and mixing process of kerosene by shock waves are related to the injection momentum ratio, evaporation momentum ratio and streamwise vortex intensity. Weakening mainstream momentum while boosting evaporation and vortex intensity effectively strengthens kerosene diffusion and mixing. This research significantly contributes to enhancing the diffusion and mixing of liquid kerosene and improving combustor performance.
引用
收藏
页数:14
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