Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/26138
Title: LES–RANS Study of Serrated Nozzle Jet Aeroacoustics for an Installed Ultra-High-Bypass-Ratio Aeroengine
Authors: Wang, ZN
Tyacke, JC
Tucker, PG
Issue Date: 28-Jun-2021
Publisher: American Institute of Aeronautics and Astronautics (AIAA)
Citation: Wang, Z.N. Tyacke, J.C. and Tucker, P.G.. (2021) 'LES–RANS Study of Serrated Nozzle Jet Aeroacoustics for an Installed Ultra-High-Bypass-Ratio Aeroengine', AIAA Journal, 59 (10), pp. 4155 - 4165. doi: 10.2514/1.J060447.
Abstract: Jet noise is amplified at low frequencies when the jet is installed under a wing. Serrations are designed at the nozzle exit to mitigate installation noise generation. In this paper, hybrid large-eddy simulation (LES) and Reynoldsaveraged Navier–Stokes (RANS) is performed to investigate the serration effects on installed jet flows and acoustics in an industrially relevant configuration: an ultra-high-bypass-ratio aeroengine mounted under a three-dimensional wing. The results show that the serrations are able to weaken jet and wing interactions, and consequently reduce farfield installation noise. The noise reduction mechanisms have been sought through the quadrupole sources in the jet plume and evanescent pressure wave scattering at the wing trailing edge.
URI: https://bura.brunel.ac.uk/handle/2438/26138
DOI: https://doi.org/10.2514/1.J060447
ISSN: 0001-1452
Other Identifiers: ORCID iD: James C. Tyacke https://orcid.org/0000-0001-7220-7711
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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