Experimental Study on the Suppression of Cavity Noise in a Locking-On State by a Slanting Inner Wall

This paper presents an experimental investigation into the noise characteristics of various slanted wall configurations. The study focuses on the noise suppression effects of cavities with slanted walls on cavity coupling noise. A total of eight configurations, with different slanting angles on the front and rear walls, were analyzed by varying the inclination of the inner wall. Noise and flow field measurements were conducted in an aeroacoustic wind tunnel, utilizing microphones for near-field and far-field noise data acquisition and hot-wire probes for flow field analysis. The results indicate that larger slant angles lead to more effective noise reduction. As the slant angle increases, the acoustic resonance frequency associated with the slanted inner wall rises, which alters the self-excited oscillation modes involved in coupling with the acoustic resonance. This reduces the impact of coupling on the sound pressure levels. The change in acoustic resonance frequency also modifies the phase delay term of the dominant mode, ultimately leading to a shift in the noise frequency.

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Publication Details

Journal
Aerospace
Published
2024-12-04
DOI
https://doi.org/10.3390/aerospace11121005
Citations
2
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
2.60
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article

Experimental Study on the Suppression of Cavity Noise in a Locking-On State by a Slanting Inner Wall

Hao Guo, Yuan Liu, Peiqing Liu
2 citations
Aerospace
Aerodynamics and Acoustics in Jet Flows
2.60
article

Experimental Study on the Suppression of Cavity Noise in a Locking-On State by a Slanting Inner Wall

Hao Guo, Yuan Liu, Peiqing Liu
article en
2 citations

Abstract

This paper presents an experimental investigation into the noise characteristics of various slanted wall configurations. The study focuses on the noise suppression effects of cavities with slanted walls on cavity coupling noise. A total of eight configurations, with different slanting angles on the front and rear walls, were analyzed by varying the inclination of the inner wall. Noise and flow field measurements were conducted in an aeroacoustic wind tunnel, utilizing microphones for near-field and far-field noise data acquisition and hot-wire probes for flow field analysis. The results indicate that larger slant angles lead to more effective noise reduction. As the slant angle increases, the acoustic resonance frequency associated with the slanted inner wall rises, which alters the self-excited oscillation modes involved in coupling with the acoustic resonance. This reduces the impact of coupling on the sound pressure levels. The change in acoustic resonance frequency also modifies the phase delay term of the dominant mode, ultimately leading to a shift in the noise frequency.

AerospaceVol. 11(12)
Beihang University (CN)
Affordable and clean energy
Openalex Percentile: Top 8%
Aerodynamics and Acoustics in Jet Flows
2.60
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