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On the balance between the tonal and broadband noise of uninstalled propellers

On the balance between the tonal and broadband noise of uninstalled propellers
On the balance between the tonal and broadband noise of uninstalled propellers
This paper provides a preliminary theoretical investigation of the balance between rotor alone tonal and broadband noise. First, using well-published theory, the different source mechanisms for tonal and broadband noise are discussed and presented. Then, using these theoretical results, an extensive parametric study has been performed in which the propeller thrust, diameter and blade solidity have been maintained constant, but the blade tip speed and blade numbers have been allowed to vary. In order to account for the variations in noise against directivity and, simultaneously, across the audible frequency range, the data are presented as Overall Sound Pressure Levels (OASPLs) and as Overall Acoustic Sound Power Level (OSWLs) integrated over the frequency range. Using these collapsed data metrics, it is found that the tonal noise dominates at low frequency and/or low tip speeds but that broadband noise is the major contributor at high-frequencies and low tip speeds. The results show a clear distinction between the regions dominated by tonal contributions and those dominated by broadband contributions. These results are discussed and related to the different tone and broadband source physical mechanisms. In addition to the primary parametric study, the paper also investigates, separately, the effects of changes in blade chord and propeller thrust. The studies presented in this paper are intended to serve as noise guidelines for propeller preliminary design.
Propeller noise, tonal and broadband noise
American Institute of Aeronautics and Astronautics
Akiwate, Deepak
b6f50d26-e59b-413e-9c66-0ee0a869813c
Parry, A. B.
5fde3fdc-35a1-4788-afd8-4b69863c09fb
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Akiwate, Deepak
b6f50d26-e59b-413e-9c66-0ee0a869813c
Parry, A. B.
5fde3fdc-35a1-4788-afd8-4b69863c09fb
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d

Akiwate, Deepak, Parry, A. B., Joseph, Phillip and Paruchuri, Chaitanya (2021) On the balance between the tonal and broadband noise of uninstalled propellers. In, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021) AIAA AVIATION 2021 FORUM (02/08/21 - 06/08/21) American Institute of Aeronautics and Astronautics. (doi:10.2514/6.2021-2308).

Record type: Book Section

Abstract

This paper provides a preliminary theoretical investigation of the balance between rotor alone tonal and broadband noise. First, using well-published theory, the different source mechanisms for tonal and broadband noise are discussed and presented. Then, using these theoretical results, an extensive parametric study has been performed in which the propeller thrust, diameter and blade solidity have been maintained constant, but the blade tip speed and blade numbers have been allowed to vary. In order to account for the variations in noise against directivity and, simultaneously, across the audible frequency range, the data are presented as Overall Sound Pressure Levels (OASPLs) and as Overall Acoustic Sound Power Level (OSWLs) integrated over the frequency range. Using these collapsed data metrics, it is found that the tonal noise dominates at low frequency and/or low tip speeds but that broadband noise is the major contributor at high-frequencies and low tip speeds. The results show a clear distinction between the regions dominated by tonal contributions and those dominated by broadband contributions. These results are discussed and related to the different tone and broadband source physical mechanisms. In addition to the primary parametric study, the paper also investigates, separately, the effects of changes in blade chord and propeller thrust. The studies presented in this paper are intended to serve as noise guidelines for propeller preliminary design.

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More information

e-pub ahead of print date: 28 July 2021
Venue - Dates: AIAA AVIATION 2021 FORUM, 2021-08-02 - 2021-08-06
Keywords: Propeller noise, tonal and broadband noise

Identifiers

Local EPrints ID: 472223
URI: http://eprints.soton.ac.uk/id/eprint/472223
PURE UUID: 7d8b8d04-51ce-4a05-a533-102207b27d3b
ORCID for Deepak Akiwate: ORCID iD orcid.org/0000-0002-9135-7886

Catalogue record

Date deposited: 29 Nov 2022 17:55
Last modified: 16 Mar 2024 23:03

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Contributors

Author: Deepak Akiwate ORCID iD
Author: A. B. Parry
Author: Phillip Joseph

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