Effect of vortex and entropy sources in sound generation for compressible cavity flow

TL;DR

This study investigates how vortex and entropy sources influence sound generation in compressible cavity flow using hybrid computational aeroacoustics, highlighting the importance of entropy sources for accurate noise prediction.

Contribution

It introduces a hybrid simulation approach that accurately predicts acoustic characteristics and emphasizes the significance of entropy sources in cavity flow noise modeling.

Findings

Hybrid method accurately predicts acoustic pressure.

Entropy sources are crucial for realistic noise simulation.

Vortex sources alone over-predict near-source pressure.

Abstract

The present study reports the effect of different source terms on the near and far-field acoustic characteristics of compressible flow over a rectangular cavity using hybrid computational aeroacoustics methodology. We use a low dispersive and dissipative compressible fluid flow solver in conjunction with an acoustic perturbation equation solver based on the spectral/hp element method. The hybrid approach involves calculating the base fields and the acoustic sources from a fluid simulation in the first step. In the next step, the acoustic solver utilizes the variables to predict the acoustic propagation due to the given sources. The validation of the methodology against benchmark cases provides quite accurate results while compared against the existing literature. The study is then extended to assess the importance of the entropy source term for the flow over a rectangular cavity. The predictions of hybrid simulations with vortex and entropy source terms reproduce the perturbation pressure values very close to the existing direct numerical simulation results. Moreover, the results suggest that the use of just the vortex source terms over-predicts the perturbation pressure near the source region. Finally, we have carried out detailed simulations with all the source terms to investigate the noise sources for compressible flow over the cavity for different Mach number ranges (M = 0.4; 0.5; 0.6; 0.7; 1.5). The obtained acoustic spectra and the sound directivity are in close agreement with the reference experiment.