Analytical and experimental investigation into the effects of leading-edge radius on gust–aerofoil interaction noise

DOI10.1017/jfm.2017.594zbMath1460.76689OpenAlexW2757844620MaRDI QIDQ4972437

Lorna J. Ayton, Paruchuri Chaitanya

Publication date: 25 November 2019

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

Full work available at URL: https://doi.org/10.1017/jfm.2017.594

zbMATH Keywords

acousticsaeroacoustics

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05)

Related Items (3)

An analytic solution for the noise generated by gust–aerofoil interaction for plates with serrated leading edges ⋮ An analytical and experimental investigation of aerofoil–turbulence interaction noise for plates with spanwise-varying leading edges ⋮ An analytical correction to Amiet’s solution of airfoil leading-edge noise in non-uniform mean flows

Cites Work

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• High-accuracy large-step explicit Runge-Kutta (HALE-RK) schemes for computational aeroacoustics
• Modern Challenges Facing Turbomachinery Aeroacoustics
• Acoustic radiation from an airfoil in a turbulent stream
• Unsteady vortical and entropic distortions of potential flows round arbitrary obstacles
• Influence of camber on sound generation by airfoils interacting with high-frequency gusts
• Influence of incidence angle on sound generation by airfoils interacting with high-frequency gusts

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