首页|内壁结构对气体中心式同轴离心喷嘴喷雾特性影响

内壁结构对气体中心式同轴离心喷嘴喷雾特性影响

扫码查看
通过改变气体中心式同轴离心喷嘴的气喷嘴内壁结构,分别对平滑内壁(A)、内壁加凹腔(B)和内壁加凸起(C)的3种喷嘴的喷雾特性进行了实验观测,同时为分析气喷嘴内壁结构改变引起的流场变化,在不考虑液相的情况下对纯气相流场进行了三维模拟研究.结果表明:3种喷嘴的雾化锥角均随气体质量流率的增加而减小,随液体质量流率的增加而增大.气喷嘴内壁加凹腔,对喷嘴的雾化锥角、破碎长度以及自激振荡频率几乎没有影响;而气喷嘴内壁加凸起则对喷雾特性有显著影响.相同工况下,内壁加凸起会使气喷嘴出口的引射作用增强,雾化锥角减小,同时气液间更强的相互作用使喷雾破碎长度随之减小.喷雾自激振荡发生时,内壁凸起亦会导致喷雾自激振荡频率随之增大.3种喷嘴的自激振荡频率均随气体质量流率的增加而增大,并对3种喷嘴的喷雾自激振荡诱发及维持机理进行了分析.通过实验探究了不同凹腔、凸起大小对喷雾特性的影响,对于B喷嘴,其喷雾的雾化锥角、破碎长度几乎一致,自激振荡频率亦差别不大;C喷嘴的雾化锥角、破碎长度均小于B喷嘴,且随凸起的增大而减小,而自激振荡频率均大于B喷嘴,且随凸起的增大而增大.
Gas-centered swirl coaxial injectors spray with variable inner wall structures
The spray characteristics of gas-centered swirl coaxial injectors in three structures of the gas injector,namely,the smooth inner wall(A),inner wall with concave cavities(B),and inner wall with projections(C),were examined by experiments.At the same time,in order to analyze the change of flow field caused by the change of the inner wall structures of the gas injectors,the pure gas flow field was simulated without considering the liquid phase.The results demonstrated that the spray angles of the three injectors increased with the gas mass flow rate,but decreased with the liquid mass flow rate.Adding a concave cavity to the inner wall of gas injector had little effect on spray angle,breakup length and self-pulsation frequency of the injector.But inner wall with projections of gas injector had a significant effect on spray characteristics.Under the same working conditions,the inner wall with projections could enhance the ejection effect of the gas injector outlet,decrease the spray angle,and the stronger gas-liquid interaction could reduce the breakup length.When the self-pulsation occurred,the inner wall with projections also increased the frequency of self-pulsation.The self-pulsation frequency of the three injectors increased with gas mass flow rate,and the induction and maintenance mechanisms of the self-pulsation of the three injectors were analyzed.The effects of different concave cavity sizes and projection sizes on spray characteristics were investigated through experiments.For injector B,the spray angle,breakup length and self-pulsation of the spray were almost the same.The spray angle and breakup length of injector C were smaller than those of injector B,and decreased with the size of projection,while the self-pulsation frequency was larger than that of injector B,and increased with the size of projection.

gas-centered swirl coaxial injectorconcave cavitiesprojectionsspray anglebreakup lengthself-pulsation

高玉超、楚威、苏凌宇、姜传金、谢远、仝毅恒

展开 >

航天工程大学宇航科学与技术系,北京 101416

气体中心式同轴离心喷嘴 凹腔 凸起 雾化锥角 破碎长度 自激振荡

国家自然科学基金

12002386

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(5)
  • 30