Theoretical investigation of the turbulent inflow noise produced by a shrouded propeller

Sung Tyaek Go, Michael J. Kingan, Ryan S. McKay, Rajnish N. Sharma

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

3 Citations (Scopus)

Abstract

A theoretical model is presented for predicting the noise produced by the interaction of turbulence with a propeller operating inside an acoustically lined shroud in an axisymmetric mean-flow. The theory is developed in the frequency domain and incorporates rapid distortion theory to obtain the distorted turbulent field at the propeller face, accounting for the potential mean-flow effect of the propeller and the shroud. The unsteady loading on the rotating blades is calculated using isolated blade response functions. The noise radiated to the far-field is then evaluated using a tailored Green’s function approach which accounts for the scattering effect of the shroud and is solved using a boundary integral approach. Results are presented for a propeller inside an acoustically rigid and lined shroud operating in flows with a range of different free-stream velocities. It is shown that lining the shroud can significantly reduce the turbulent inflow noise.
Original languageEnglish
Title of host publication28th AIAA/CEAS Aeroacoustics Conference, 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Electronic)9781624106644
DOIs
Publication statusPublished - 13 Jun 2022
Event28th AIAA/CEAS Aeroacoustics Conference, 2022 - Southampton, United Kingdom
Duration: 14 Jun 202217 Jun 2022

Publication series

NameAIAA/CEAS Aeroacoustics Conference
PublisherAIAA
ISSN (Print)1946-7826

Conference

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

Bibliographical note

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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