摘要
基于RANS方法对氢气在氩气和氮气氛围下的高压喷射过程进行仿真,研究了压力、温度和激波对氢气射流喷射和卷吸特性的影响.研究表明:射流贯穿距由于马赫盘的存在而呈现三阶段变化.在不同喷射压力下,射流前期卷吸能力随着喷嘴压力比(NPR)的增加而增大,而后期呈现相反趋势.在相同密度下,激波影响射流前期卷吸效果,但随着射流发展效果逐渐减弱.温度升高,氢气射流的贯穿距明显增大,但射流卷吸能力也显著降低.此外,氢气射流在氮气氛围下的卷吸环境气体物质的量和卷吸能力均强于氩气氛围.
The hydrogen jets under argon and nitrogen atmosphere were simulated by the RANS method.The effects of gas pressure,gas temperature and shock wave on spray and entrainment characteristics of hydrogen jet were studied.It is found that the penetration of the jet presents three stages of changes due to the Mach disk.The entrainment capacity of the jet at different injection pressures increases with the increase of the nozzle pressure ratio(NPR)in the early stage but the opposite trend in the later stage.Under the same density,the shock wave affects the entrainment in the early stage of jet,but the effect gradually decreases with the development of jet.With the increase of temperature,the penetration of hydrogen jet increases obviously,but the jet entrainment capacity decreases significantly.In addition,the entrainment amount of ambient gas and the entrainment capacity of hydrogen jet under a nitrogen atmosphere are both stronger than those under an argon atmosphere.
作者
邓俊
钟慧平
龚学海
龚寅春
李理光
Deng Jun;Zhong Huiping;Gong Xuehai;Gong Yinchun;Li Liguang(School of Automotive Studies,Tongji University,Shanghai 200092,China;CDHK,Tongji University,Shanghai 200092,China)
出处
《内燃机学报》
EI
CAS
CSCD
北大核心
2019年第1期68-75,共8页
Transactions of Csice
基金
国家自然科学基金资助项目(51576141
51006075)
关键词
氢气射流
马赫盘
贯穿距
卷吸
hydrogen jet
Mach disk
penetration
entrainment