Effects of boundary-layer tripping on the acoustic tones of impinging jets

The influence of boundary-layer tripping on the acoustic tones generated by a jet at a Mach number of 0.9 impinging on a flat plate is investigated for two nozzle-to-plate distances. Tripping the jet boundary-layer is found not to appreciably alter the frequencies but to significantly affect the levels of the tones. These effects strongly depend on the tone number and on the nozzle-to plate distance. For a given tone, in particular, the levels can decrease or increase depending on the distance. Therefore, tripping the boundary layers of impinging jets can result to less or more noise, and cannot be considered as a reliable method to reduce noise for these jets.

Publication Details

Journal
Springer Link (Chiba Institute of Technology)
Published
2025-11-14
DOI
https://doi.org/10.1051/aacus/2025059/pdf
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
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article

Effects of boundary-layer tripping on the acoustic tones of impinging jets

Springer Link (Chiba Institute of Technology)
Aerodynamics and Acoustics in Jet Flows
article

Effects of boundary-layer tripping on the acoustic tones of impinging jets

article en

Abstract

The influence of boundary-layer tripping on the acoustic tones generated by a jet at a Mach number of 0.9 impinging on a flat plate is investigated for two nozzle-to-plate distances. Tripping the jet boundary-layer is found not to appreciably alter the frequencies but to significantly affect the levels of the tones. These effects strongly depend on the tone number and on the nozzle-to plate distance. For a given tone, in particular, the levels can decrease or increase depending on the distance. Therefore, tripping the boundary layers of impinging jets can result to less or more noise, and cannot be considered as a reliable method to reduce noise for these jets.

Springer Link (Chiba Institute of Technology)
Openalex Percentile: Top 28%
Aerodynamics and Acoustics in Jet Flows
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