Experimental study on the flow field distribution characteristics of an open-end swirl injector under ambient pressure

被引:16
作者
He, Xiujie [1 ,2 ]
Chen, Chen [2 ,3 ]
Yang, Yang [2 ]
Yan, Zhihui [2 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, 1 Dongxiang Rd, Xian, Shaanxi, Peoples R China
[2] China Aerodynam Res & Dev Ctr, 6 South Sect,Second Ring Rd, Mianyang, Sichuan, Peoples R China
[3] Jiangsu Univ Sci & Technol, Sch Mech Engn, 2 Mengxi Rd, Zhenjiang, Jiangsu, Peoples R China
关键词
Swirl injector; Ambient pressure; Spray morphology; SMD; Velocity; SPRAY CONE ANGLE; AIR-CORE; FUEL SPRAY; BREAKUP; COEFFICIENT; PERFORMANCE; PREDICTION; DISCHARGE; DIAMETER; CHAMBER;
D O I
10.1016/j.ast.2020.105691
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
To investigate the influence of ambient pressure on the atomization characteristics of an open-end swirl injector, the spray morphology, droplet diameter distribution and velocity distribution were measured under ambient pressures of 0.1 MPa, 0.5 MPa, 1.0 MPa, 1.5 MPa and 2.0 MPa using a high-speed camera and Phase Doppler Interferometer (PDI). As the ambient pressure increased, the spray region and intact liquid film area decreased, and the spray angle, spray width and breakup length shortened. Increased ambient pressure made droplet SMD larger and the SMD curves flatter. The droplet Sauter Mean Diameter (SMD) at each measuring point along the radial direction increased gradually and then decreased slightly, but there was no significant difference between different measuring sections. Ambient pressure had a more significant influence on axial velocity than the tangential velocity. As the ambient pressure increased, the axial velocity decreased, and the region where droplets had negative axial velocity was compressed backward to the injector outlet. Additionally, the tangential velocity near the outlet fluctuated greatly along the radial distribution. As the axial distance increased, the velocity curves became much flatter. (C) 2020 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:8
相关论文
共 45 条
[1]   Liquid flow in a simplex swirl nozzle [J].
Amini, Ghobad .
INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 2016, 79 :225-235
[2]  
[Anonymous], [No title captured]
[3]  
[Anonymous], [No title captured]
[4]  
[Anonymous], [No title captured]
[5]   Performance comparison of oxidizer injectors in a 1-kN paraffin-fueled hybrid rocket motor [J].
Bouziane, M. ;
Bertoldi, A. E. M. ;
Milova, P. ;
Hendrick, P. ;
Lefebvre, M. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 89 :392-406
[6]   The spray characteristics of an open-end swirl injector at ambient pressure [J].
Chen, Chen ;
Yang, Yang ;
Yang, Shun-hua ;
Gao, Hong-li .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 67 :78-87
[7]   Effect of ambient pressure on liquid swirl injector flow dynamics [J].
Chen, Xiaodong ;
Yang, Vigor .
PHYSICS OF FLUIDS, 2014, 26 (10)
[8]  
[陈晓东 Chen Xiaodong], 2010, [推进技术, Journal of Propulsion Technology], V31, P539
[9]   AN APPRAISAL OF SWIRL ATOMIZER INVISCID FLOW ANALYSIS, PART 2: INVISCID SPRAY CONE ANGLE ANALYSIS AND COMPARISON OF INVISCID METHODS WITH EXPERIMENTAL RESULTS FOR DISCHARGE COEFFICIENT, AIR CORE RADIUS, AND SPRAY CONE ANGLE [J].
Chinn, John Joss .
ATOMIZATION AND SPRAYS, 2009, 19 (03) :283-308
[10]   Experimental Evaluation of Low Pressure-Swirl Atomizer Applied Engineering Design Procedure [J].
Couto, Heraldo da Silva ;
Lacava, Pedro Teixeira ;
Bastos-Netto, Demetrio ;
Pimenta, Amilcar Porto .
JOURNAL OF PROPULSION AND POWER, 2009, 25 (02) :358-364