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Journal ArticleDOI

The radiation of sound by the instability waves of a compressible plane turbulent shear layer

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TLDR
In this article, the problem of acoustic radiation generated by instability waves of a compressible plane turbulent shear layer is solved, and the solution provided is valid up to the acoustic far-field region.
Abstract
The problem of acoustic radiation generated by instability waves of a compressible plane turbulent shear layer is solved. The solution provided is valid up to the acoustic far-field region. It represents a significant improvement over the solution obtained by classical hydrodynamic-stability theory which is essentially a local solution with the acoustic radiation suppressed. The basic instability-wave solution which is valid in the shear layer and the near-field region is constructed in terms of an asymptotic expansion using the method of multiple scales. This solution accounts for the effects of the slightly divergent mean flow. It is shown that the multiple-scales asymptotic expansion is not uniformly valid far from the shear layer. Continuation of this solution into the entire upper half-plane is described. The extended solution enables the near- and far-field pressure fluctuations associated with the instability wave to be determined. Numerical results show that the directivity pattern of acoustic radiation into the stationary medium peaks at 20 degrees to the axis of the shear layer in the downstream direction for supersonic flows. This agrees qualitatively with the observed noise-directivity patterns of supersonic jets.

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Citations
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Journal ArticleDOI

A stability study of the developing mixing layer formed by two supersonic laminar streams

TL;DR: In this paper, an inviscid, parallel, spatial linear stability analysis is performed on both bounded and semibounded developing mixing layers formed between a laminar Mach 8 stream and another at Mach 3.
Journal ArticleDOI

Instability waves in high-speed jets: near- and far-field DNS/LES data analysis

TL;DR: In this article, the authors extracted coherent components of the turbulent jet flow fields using a filter based on proper orthogonal decomposition (POD) to examine the effects of nonlinear interactions and test the decomposition method, forced laminar jets were also considered; the flow data were obtained from a direct numerical simulation (DNS) database for an unheated Mj = 0.90 and ReD = 4,100 jet.
Journal ArticleDOI

Acoustic near field of a transonic instability wave packet

TL;DR: In this paper, the authors considered the problem of acoustic radiation generated by a spatial instability wave on a weakly developing shear flow and computed the acoustic pressure field by using a Fourier transform along the streamwise direction.
Journal ArticleDOI

Two-point radiation statistics from large-scale turbulent structures within supersonic jets:

TL;DR: The noise from large-scale coherent turbulent structures within jets remains the dominant source of noise in jets as discussed by the authors, and for the purpose of developing future control systems for the large scale noise source, the authors investigate the use of large scale coherent turbulent structure within jets.
Dissertation

Résolution des équations de stabilité globale en régimes incompressible et compressible avec une méthode aux différences finies de haute précision

Xavier Merle
TL;DR: In this paper, the authors propose a code de stabilite globale adapte aux ecoulements en regime compressible and en geometrie curviligne, in order to study l'interaction entre l'onde de choc et la couche limite turbulente.
References
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The fast Fourier Transform

TL;DR: A computer algorithm that computes the discrete Fourier transform much faster than other algorithms, is explained and examples and detailed procedures are provided to assist the reader in learning how to use the algorithm.
Journal ArticleDOI

The role of shear-layer instability waves in jet exhaust noise

TL;DR: In this article, large-scale structures in the form of instability waves are shown to be present in an acoustically and aerodynamically well behaved jet even at high Mach numbers.
Journal ArticleDOI

Stability of slowly diverging jet flow

TL;DR: In this paper, coherent axisymmetric structures in a turbulent jet are modelled as linear instability modes of the mean velocity profile, regarded as the profile of a fictitious laminar inviscid flow.
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