Effect of serrated trailing edges on aerofoil tonal noise

DOI10.1017/jfm.2020.724zbMath1460.76696OpenAlexW3096644006MaRDI QIDQ5131324

Matthieu B. R. Gelot, Jae Wook Kim

Publication date: 5 November 2020

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://eprints.soton.ac.uk/443649/1/ste_tonal_noise_reduction.pdf

zbMATH Keywords

aeroacousticsflow-structure interactionsturbulence simulation

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05)

Cites Work

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• On the universal trends in the noise reduction due to wavy leading edges in aerofoil–vortex interaction
• Numerical investigation of the tone noise mechanism over laminar airfoils

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