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 language | English |
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| Title of host publication | 28th AIAA/CEAS Aeroacoustics Conference, 2022 |
| Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
| ISBN (Electronic) | 9781624106644 |
| DOIs | |
| Publication status | Published - 13 Jun 2022 |
| Event | 28th AIAA/CEAS Aeroacoustics Conference, 2022 - Southampton, United Kingdom Duration: 14 Jun 2022 → 17 Jun 2022 |
Publication series
| Name | AIAA/CEAS Aeroacoustics Conference |
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| Publisher | AIAA |
| ISSN (Print) | 1946-7826 |
Conference
| Conference | 28th AIAA/CEAS Aeroacoustics Conference, 2022 |
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| Country/Territory | United Kingdom |
| City | Southampton |
| Period | 14/06/22 → 17/06/22 |
Bibliographical note
Publisher Copyright:© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.