Identification of structures driving trailing-edge noise. Part II -- Numerical investigation
Zhenyang Yuan, Simon Demange, Kilian Oberleithner, Andr\'e V., G. Cavalieri, Ardeshir Hanifi

TL;DR
This study uses high-fidelity simulations and spectral analysis to identify the turbulent structures responsible for broadband trailing-edge noise on an airfoil, confirming experimental observations and proposing a reduced-order acoustic model.
Contribution
It introduces a detailed numerical investigation linking spanwise-coherent structures to trailing-edge noise, and develops a reduced-order model for acoustic prediction.
Findings
Streamwise-travelling wavepackets are identified as noise sources.
Good agreement between simulations and experiments in flow and acoustic spectra.
A low-rank acoustic model is proposed for far-field noise reconstruction.
Abstract
The aim of the present work is to investigate the mechanisms of broadband trailing-edge noise generation to improve prediction tools and control strategies. We focus on a NACA 0012 airfoil at 3 degrees angle of attack and chord Reynolds number Re = 200,000. A high-fidelity wall-resolved compressible implicit large eddy simulation (LES) is performed to collect data for our analysis. The simulation is designed in close alignment with the experiment described in detail in the companion paper (Demange et al. 2024b). Zig-zag geometrical tripping elements, added to generate a turbulent boundary layer, are meshed to closely follow the experimental setup. A large spanwise domain is used in the simulation to include propagative acoustic waves with low wavenumbers. An in-depth comparison with experiments is conducted showing good agreement in terms of mean flow statistics, acoustic and…
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Taxonomy
TopicsAcoustic Wave Phenomena Research · Vehicle Noise and Vibration Control · Structural Health Monitoring Techniques
