Scale-Resolving Simulation of Aeroacoustic Sound from Coanda Flaps

Bernicke, Paul; Ananthan, V.B.; Akkermans, R.A.D.; Dierke, Jürgen; Ewert, Roland

doi:10.1007/978-3-030-52429-6_32

Cited by 1 publication

(1 citation statement)

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“…Yet, accuracy challenges arise from the interplay of numerous parameters, underlying assumptions, and the size of resolved eddies [122,123]. Scale-resolving methods, a subset of numerical techniques, strive to encompass a range of turbulence scales, bridging the gap between conventional RANS and DNS methodologies [124]. Empirical or semi-empirical methods, the final category, leverage experimental data and correlations to estimate noise levels.…”

Section: Empirical/semi-empirical Approachesmentioning

confidence: 99%

Recent Advances in Airfoil Self-Noise Passive Reduction

Amirsalari,

Rocha

2023

Aerospace

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Airflow-induced noise prediction and reduction is one of the priorities for both the energy and aviation industries. This review paper provides valuable insights into flow-induced noise computation, prediction, and optimization methods with state-of-the-art efforts in passive noise reduction on airfoils, blades, and wings. This review covers the combination of several approaches in this field, including analytical, numerical, empirical, semi-empirical, artificial intelligence, and optimization methods. Under passive noise reduction techniques, leading and trailing edge treatments, porous materials, controlled diffusion airfoils, morphing wings, surface treatments, and other unique geometries that researchers developed are among the design modification methods discussed here. This work highlights the benefits of incorporating multiple techniques to achieve the best results concerning the desired application and design. In addition, this work provides an overview of the advantages and disadvantages of each tool, with a particular emphasis on the possible challenges when implementing them. The methods and techniques discussed herein will help increase the acoustic efficiency of aerial structures, making them a beneficial resource for researchers, engineers, and other professionals working in aviation noise reduction.

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Section: Empirical/semi-empirical Approachesmentioning

confidence: 99%