Experimental Investigation on the Circular Cylindrical Cavity Noise at the Locked-on State

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Abstract

In the locked-on state, the ratio of resonant frequency to the fundamental frequency of self-sustained oscillation is suggested to play a key role in predicting the dominant tonal noise for the square cavity. In this paper, we similarly investigate the mechanism of coupled self-excited oscillation and acoustic resonance aerodynamic noise in cylindrical cavities with different depths at low speeds. The experimental noise field results are described for a circular cavity with a diameter of 78 mm and a depth ranging from 70 mm to 120 mm at an incoming flow velocity of 5 to 35 m/s. A strong self-excited oscillatory discrete noise is generated in this cylindrical cavity flow at the locked-on state and the parameter Rd is also well proofed to evaluate and predict the dominant mode order and the total sound pressure level peak.

Original languageEnglish
Title of host publication2023 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2023, Proceedings - Volume I
EditorsSong Fu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1577-1590
Number of pages14
ISBN (Print)9789819739974
DOIs
StatePublished - 2024
EventAsia-Pacific International Symposium on Aerospace Technology, APISAT 2023 - Lingshui, China
Duration: 16 Oct 202318 Oct 2023

Publication series

NameLecture Notes in Electrical Engineering
Volume1050 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceAsia-Pacific International Symposium on Aerospace Technology, APISAT 2023
Country/TerritoryChina
CityLingshui
Period16/10/2318/10/23

Keywords

  • Aeroacoustics
  • Cavity noise
  • Dominant mode frequency
  • Locked-on state
  • Overall sound pressure level

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