LES study of noise and its sources of closely installed jets

Zhong-Nan Wang, Anderson Proenca, Jack Lawrence, Paul G. Tucker

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

When a jet is closely installed under a solid surface, turbulent jet plume is modified. Two levels of jet-plate interactions are present. In addition to linear evanescent instability wave scattered by the plate trailing edge, nonlinear jet turbulence strongly interacts with the plate underneath surface. Both of the interactions could lead to far-field noise change but with different mechanisms. Large-Eddy Simulation (LES) has been performed on two installed jets and one baseline isolated jet to investigate the noise generation mechanisms for this closely installed jet. The distance between jet and plate surface is adjusted for the two installed jets so that strong hydrodynamic interaction is only present in one of the configurations. Far-field noise, computed using Ffowcs Williams-Hawkings (FW-H) equations, is compared for the two installed jets to show the effect of close installation. The near-field sound sources are examined by analysing quadrupole sources of turbulent mixing and dipole sources of unsteady plate surface loading.
Original languageEnglish
Title of host publication28th AIAA/CEAS Aeroacoustics 2022 Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages12
ISBN (Electronic)9781624106644
DOIs
Publication statusPublished - 13 Jun 2022
Event28th AIAA/CEAS Aeroacoustics 2022 Conference - Southampton, United Kingdom
Duration: 14 Jun 202217 Jun 2022

Conference

Conference28th AIAA/CEAS Aeroacoustics 2022 Conference
Country/TerritoryUnited Kingdom
CitySouthampton
Period14/06/2217/06/22

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