跳到主要导航 跳到搜索 跳到主要内容

Physical model for acoustic resonance in annular cavity structure

  • Fengtong ZHAO
  • , Mingsui YANG*
  • , Xiaodong JING
  • , Deyou WANG
  • , Yundong SHA
  • , Yujin LIU
  • *此作品的通讯作者
  • Beihang University
  • Shenyang Aerospace University
  • AECC Shenyang Engine Research Institute

科研成果: 期刊稿件文章同行评审

摘要

A physical model for acoustic resonance in the annular cavity structure is developed to represent the typical characteristic when acoustic resonance occurs. Firstly, the measurement of sound pressure in the casing and rotor blades vibration is operated in a multistage high pressure compressor. The sharp peak frequency and discrete multi-tone occur in the frequency spectrum of sound pressure in the compressor, and the vibration of the first stage of rotor blades synchronously presents the high amplitude. The frequencies associated with rotor blades vibration can be calculated with rotating sound source theory. It is also confirmed that acoustic resonance occurs in the multistage compressor. With acoustic similarity principle, an annular cavity model is established to simulate the typical characteristics of acoustic resonance in the compressor based on Large Eddy Simulation (LES) and Lighthill acoustic analogy. The coupling relationship between cavity acoustic mode and disc vibration mode shape is expounded when acoustic resonance occurs in the model. And acoustic resonance will be locked in the certain flow rate range. All these characteristics match well with those occur in the multistage high pressure compressor.

源语言英语
页(从-至)3228-3237
页数10
期刊Chinese Journal of Aeronautics
33
12
DOI
出版状态已出版 - 12月 2020

学术指纹

探究 'Physical model for acoustic resonance in annular cavity structure' 的科研主题。它们共同构成独一无二的学术指纹。

引用此