王李璨

电子邮箱:

所在单位:航空航天技术研究院

学历:研究生(博士后)

办公地点:中国湖南省长沙市岳麓区 岳麓街道麓山南路932号(邮编: 410083) 中南大学 校本部岳麓山校区 升华楼后楼 714室

论文成果

当前位置: 中文主页 >> 论文成果

Investigation of acoustic propagation and source localization in a hot jet flow

发布时间:2025-03-20 点击次数:

DOI码:10.1016/j.jsv.2020.115801
发表刊物:Journal of Sound and Vibration
摘要:A jet flow typically occurs in open-jet wind tunnels and turbofan engines, where there are velocity and temperature gradients between the source region and the outside environment. These gradients form a thermal shear layer that determines acoustic propagation and source localization. Moreover, they induce Kelvin–Helmholtz instabilities in numerical simulations. To stabilize simulations, a gradient-term suppression and filtering method is proposed and validated using time-domain linearized Euler equations. For sound propagation, the influences of the steep gradients of the velocity and temperature together with the spreading angle and source frequency are investigated through a self-similar shear layer with superposition of compressibility and heat. Those refraction influences strongly change the beamforming-related phase rather than the directivity-related amplitude. Next, the computed database is processed by delay-and-sum beamforming to localize the source position. In the beamforming part, refraction and amplitude corrections based on Amiet’s theory with an extension for temperature differences are numerically evaluated and later applied when analyzing the localization error. This localization error is basically proportional to the jet Mach number, temperature ratio, and source frequency and is inversely proportional to the spreading rate. Finally, the localization error is fitted as a linear function of the product of the jet Mach number and the Strouhal number.
合写作者:Yancheng You, Ruofan Qiu
第一作者:Lican Wang
论文类型:期刊论文
通讯作者:Rongqian Chen
学科门类:工学
一级学科:航空宇航科学与技术
文献类型:J
卷号:492
期号:115801
页面范围:1-21
是否译文:
发表时间:2020-10-01
收录刊物:SCI