Experimental Study on Spray Characteristics of ADN/Water Based Gel Propellant with Impinging Jet Injectors

被引:11
|
作者
Wang, Feng-Shan [1 ,2 ]
Chen, Jun [1 ,2 ]
Zhang, Tao [1 ,2 ]
Guan, Hao-Sen [3 ,4 ]
Li, Hong-Meng [3 ,4 ]
机构
[1] Beijing Inst Control Engn, Beijing 100190, Peoples R China
[2] Beijing Engn Res Ctr Efficient & Green Aerosp, Prop Technol, Beijing 100190, Peoples R China
[3] Beijing Jiaotong Univ, Sch Mech Elect & Control Engn, Beijing 100044, Peoples R China
[4] Beijing Jiaotong Univ, Key Lab Vehicle Adv Mfg Measuring & Control Techn, Beijing 100044, Peoples R China
关键词
ADN-water based gel propellant; Impinging jet injector; Breakup length; Spray cone angle; ATOMIZATION CHARACTERISTICS; FUELS; ADN;
D O I
10.1002/prep.202000001
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
ADN/water-based gel propellant is a new high-energy, green, non-toxic propellant, so it has good application prospects in the future aerospace industry. In order to study the spray characteristics of ADN/water-based gel propellant, two-strand impinging nozzles were used to carry out experiments. The spray images were observed by high-speed photography, and the effects of different injection pressure, nozzle diameter, and impact angle on spray configuration, spray cone angle and breakup length of liquid film were studied. The results show that the breakup length of liquid film decreased with the increase in injection pressure and impact angle, and increased with the increase in nozzle diameter. The spray cone angle increased with the increase in injection pressure, nozzle diameter, and impact angle. And the effects of spray pressure and nozzle diameter on spray process were obvious. The distribution of propellant spray in space was clarified under these conditions and it would provide reference data for the structural design of the combustion chamber of the engine.
引用
收藏
页码:1357 / 1365
页数:9
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