Sound generated by the interaction between shock and instability waves in supersonic round jets
Binhong Li, Benshuai Lyu

TL;DR
This paper develops an analytical model for sound generated by shock-instability interactions in supersonic round jets, revealing key directivity features and the inadequacy of the monopole assumption, with results aligning well with experimental data.
Contribution
The study extends previous planar models to circular jets, providing a closed-form solution for the acoustic field and insights into shock-related noise mechanisms.
Findings
Sound directivity matches experimental screech patterns.
Noise intensity decays near 180-degree observer angle.
Mach wave radiation is the primary noise generation mechanism.
Abstract
In this paper, we develop an analytical model to investigate the sound generated by the shock-instability interactions (SII) in supersonic round jets, extending our previous two-dimensional planar study to circular configurations. The jet is represented by a vortex sheet, with its motion modeled by the Euler equations. Shock and instability waves are modeled using Pack's approach and the linear stability theory, respectively, while their interaction is calculated by solving an inhomogeneous wave equation. Using the Fourier transform and steepest descent method, we obtain a closed-form solution for the resulting acoustic field. Results due to the interaction between the instability waves and one interaction cell capture the key directivity features of screech reported in experiments and numerical simulations, indicating that the classic monopole assumption may be inadequate. In…
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Taxonomy
TopicsAerodynamics and Acoustics in Jet Flows · Computational Fluid Dynamics and Aerodynamics · Plasma and Flow Control in Aerodynamics
