摘要
本文研究了后掠叶栅的发声机理,并给出了相应的声压、声功率的计算公式。文中还讨论了转子尾流与后掠静子相互作用的干涉噪声随后掠角的变化规律,结果表明合理地选择后掠角将对干涉噪声的大小产生重要的影响。
A theoretical model for analysing the aeroacoustic nature of swej t cascade is described.Some closed form expressions for the acoustic pressure and acoustic power in far field are obtained.These expressions are used in parametric,calculations of rotor viscous wake-stator vane interaction in order to study the effectiveness of sweep as a noise reduc-tion mechanism.It is concluded that the swept angle play an important role in the generation of noise of cascade,in some cases,however,the swept angle does not result in the reduction of noise generated by the interaction of rotor viscous wake-stator vane.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1989年第1期39-49,共11页
Journal of Beijing University of Aeronautics and Astronautics
关键词
叶轮机
噪声
叶栅
气动
声学
unsteady flow of turbomachnery,noise of turbomachinery,aeroacousties,cascade