基于CLSVOF(coupled level-set and volume of fluid)方法对两股互击式喷嘴雾化过程进行了数值模拟,仿真结果与实验结果进行对比,并详细考察了动量比对液膜特性的影响.结果表明:①CLSVOF方法能对射流撞击形成的液膜形态进行有效捕捉,计算获得的液膜形态与实验结果一致.②两股不同孔径的射流在撞击点撞击过程中,由于大孔径一侧的部分射流未参与撞击,而中心位置的液体在撞击之后速度迅速下降,周围的液体则保持撞击前的速度,使得射流撞击之后形成弧形状液膜.③在不同动量比条件下,射流撞击后轴线位置的合成角主要取决于参与撞击射流的动量比,数值计算结果与理论计算结果吻合较好,误差均小于10%.
Abstract
Numerical simulation was carried out on the atomization process of unlike-doublet impinging jets injector based on the CLSVOF (coupled level-set and volume of fluid) method. The simulation results were compared with the experiment results
and the effect of momentum ratios on liquid sheet characteristics was investigated in detail. The results show that:(1) The CLSVOF method can efficiently capture the liquid sheet characteristics formed by jet impact. The calculated liquid sheet agrees well with the experiment result. (2) In the impinging process of jets
part of the jet flow of large diameter nozzle is not involved in the impact
while the velocity of liquid in the central position drops rapidly after impact
and at the same time
the surrounding liquid maintains the velocity before impact
which results in the formation of cured liquid sheet. (3) Under the conditions of different momentum ratios
the resultant angle in the axis position after impact mainly depends on the momentum ratio of impinging jets. The simulation results are in good agreement with the theoretical calculation results
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Related Author
Jun TIAN
Yufan XIE
Fei LONG
Qin LIU
Yidan CHEN
Hongyu CHEN
Yazhou LIU
Shijie LIU
Related Institution
China Special Vehicle Research Institute,Aviation Industry Corporation of China,Limited
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Nanjing Puguo Technology Company,Limeted
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation