Investigation of the enhanced cavitation model considering turbulence effects of fuel flow in the injector nozzle holes

被引:0
|
作者
Liu, Weilong [1 ]
Zhao, Jianhui [1 ]
Markov, Vladimir [1 ]
Wu, Han [2 ]
Grekhov, Leonid [1 ]
机构
[1] Harbin Engn Univ, Coll Power & Energy Engn, Dongli Bldg,1212 Room,Nantong St 145, Harbin, Peoples R China
[2] Beijing Inst Technol, Sch Mech Engn, Beijing, Peoples R China
基金
国家重点研发计划;
关键词
Turbulent kinetic energy; shear stress; gas/liquid two-phase flow; modification of cavitation model; injector nozzles;
D O I
10.1177/14680874241290630
中图分类号
O414.1 [热力学];
学科分类号
摘要
The cavitation model is essential in simulating cavitation flow characteristics of injector nozzles, with its accuracy directly impacting simulation precision. This paper developed a quantitative relationship between critical cavitation pressure, turbulent kinetic energy, and shear stress, and introduced a modified cavitation model that considers turbulence effects. A simulation study was conducted on the fuel flow characteristics inside the nozzle of a high-pressure common rail diesel injector with seven nozzle holes. The results indicate that compared to the original model, the cavitation development calculated by the modified model is enhanced at different injection pressures. In terms of axial distribution, cavitation inside the nozzle hole increases, but the impact on cavitation of different intensities varies, with the development of moderate to low-intensity cavitation being promoted, while strong cavitation is inhibited. In terms of radial distribution, the intensity of cavitation on the upper wall inside the nozzle hole increases, which is caused by the higher mass transfer rate near the upper wall at the nozzle hole inlet. As the injection pressure increases from 120 to 240 MPa, the change rate of cavitation volume ratio inside the nozzle holes calculated by the original and modified models increases from 5.1% to 9.7%. It is necessary to use the modified model for the calculations of gas/liquid two-phase flow within the nozzle hole, especially at high injection pressure.
引用
收藏
页数:15
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