Nonlinear evolution and low-frequency acoustic radiation of ring-mode coherent structures on subsonic turbulent circular jets
File(s)ring CS - final.pdf (2.35 MB)
Accepted version
Author(s)
Zhang, Zhongyu
Wu, Xuesong
Type
Journal Article
Abstract
By adapting the triple decomposition of an instantaneous turbulent flow into a
time-averaged mean field, large-scale coherent motion and fine-scale random fluctuations,
and treating the coherent motion as instability modes on the mean flow, a mathematical
theory is developed to describe the nonlinear spatial–temporal modulation and acoustic
radiation of a coherent structure (CS) on a circular jet in the form of a wavepacket
consisting of an axisymmetric (ring) mode and its sideband components. The effect of
fine-scale turbulence on the CS is characterised via a gradient closure model, and the
non-parallelism due to the axial variation and radial velocity of the mean flow is taken
into account. By employing the matched asymptotic expansion and multi-scale techniques,
a strongly nonlinear system is derived, which governs the envelope of the CS and its
vorticity and temperature in the critical layer. Numerical solutions to the evolution system
show that the theory captures the nonlinear amplitude attenuation and vorticity roll-up
as observed in experiments. The large-distance asymptotic properties of the CS allow us
to describe and predict its acoustic radiation on the basis of first principles. The CS is
trapped within the jet, but its self-interaction generates a temporally and axially modulated
mean-flow distortion, which acts as the emitter to radiate low-frequency sound waves, with
the Reynolds stresses driving this mean-flow distortion being identified unambiguously
to be the physical source in the present context. An equivalent source in the Lighthill
type of acoustic analogy is also identified. For the present ring-mode CS in the fully
developed region of a circular jet, the equivalent source can be determined before the
acoustic field is, and the intensity of the radiated sound waves is found to be O(3), where
measures the magnitude of the CS. The directivity and spectrum of the acoustic far field are calculated for representative parameters, and the predicted features resemble experimental
measurements.
time-averaged mean field, large-scale coherent motion and fine-scale random fluctuations,
and treating the coherent motion as instability modes on the mean flow, a mathematical
theory is developed to describe the nonlinear spatial–temporal modulation and acoustic
radiation of a coherent structure (CS) on a circular jet in the form of a wavepacket
consisting of an axisymmetric (ring) mode and its sideband components. The effect of
fine-scale turbulence on the CS is characterised via a gradient closure model, and the
non-parallelism due to the axial variation and radial velocity of the mean flow is taken
into account. By employing the matched asymptotic expansion and multi-scale techniques,
a strongly nonlinear system is derived, which governs the envelope of the CS and its
vorticity and temperature in the critical layer. Numerical solutions to the evolution system
show that the theory captures the nonlinear amplitude attenuation and vorticity roll-up
as observed in experiments. The large-distance asymptotic properties of the CS allow us
to describe and predict its acoustic radiation on the basis of first principles. The CS is
trapped within the jet, but its self-interaction generates a temporally and axially modulated
mean-flow distortion, which acts as the emitter to radiate low-frequency sound waves, with
the Reynolds stresses driving this mean-flow distortion being identified unambiguously
to be the physical source in the present context. An equivalent source in the Lighthill
type of acoustic analogy is also identified. For the present ring-mode CS in the fully
developed region of a circular jet, the equivalent source can be determined before the
acoustic field is, and the intensity of the radiated sound waves is found to be O(3), where
measures the magnitude of the CS. The directivity and spectrum of the acoustic far field are calculated for representative parameters, and the predicted features resemble experimental
measurements.
Date Issued
2022-06-10
Date Acceptance
2022-03-16
Citation
Journal of Fluid Mechanics, 2022, 940
ISSN
0022-1120
Publisher
Cambridge University Press
Journal / Book Title
Journal of Fluid Mechanics
Volume
940
Copyright Statement
Copyright © 2022 Cambridge University Press. This article has been published in a revised form in Journal of Fluid Mechanics http://dx.doi.org/10.1017/jfm.2022.252 This version is free to view and download for private research and study only. Not for re-distribution, re-sale or use in derivative works.
Copyright URL
Identifier
https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000781112600001&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=a2bf6146997ec60c407a63945d4e92bb
Subjects
aeroacoustics
CONTROLLED EXCITATION
FIELD
FLOW
HIGH-SPEED
jet noise
LARGE-SCALE STRUCTURES
Mechanics
NOISE SOURCES
Physical Sciences
Physics
Physics, Fluids & Plasmas
Science & Technology
shear-flow instability
SHEAR-LAYER INSTABILITY
SOUND RADIATION
SOURCE MECHANISMS
Technology
WAVES
Publication Status
Published
Article Number
A39
Date Publish Online
2022-04-12