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Fan buzz-saw noise under intake flow distortion: a computational study

Fan buzz-saw noise under intake flow distortion: a computational study
Fan buzz-saw noise under intake flow distortion: a computational study

Steady intake flow distortion due to non-axisymmetric intake geometry and angle of attack of the flight stream can affect various fan tone noise, especially fan buzz-saw noise. In this paper, unsteady CFD simulations have been performed on fully coupled fan and intake models to study the effect of intake flow distortion on fan buzz-saw noise. Three cases have been investigated, namely a baseline case, an axisymmetric distorted case, and a drooped distorted case, and comparisons have been made on the intake noise data extracted from the CFD calculations. The distortion fields generated in the last two cases have been compared and characterised by Fourier-Bessel harmonics. The results show that the distortion generated in the drooped case is more significant and has resulted in stronger circumferential mode scattering appearing initially in the fan domain. The main effect of the distortions in both cases is to cause scattering of the rotor-locked modes into adjacent circumferential harmonics, as the shock waves propagate through the intake ducts.

American Institute of Aeronautics and Astronautics
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Wilson, Alexander G.
208d47f4-0a9d-4de3-8e45-07536862d07b
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Wilson, Alexander G.
208d47f4-0a9d-4de3-8e45-07536862d07b

Wu, Long and Wilson, Alexander G. (2024) Fan buzz-saw noise under intake flow distortion: a computational study. In 30th AIAA/CEAS Aeroacoustics Conference, 2024. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2024-3426).

Record type: Conference or Workshop Item (Paper)

Abstract

Steady intake flow distortion due to non-axisymmetric intake geometry and angle of attack of the flight stream can affect various fan tone noise, especially fan buzz-saw noise. In this paper, unsteady CFD simulations have been performed on fully coupled fan and intake models to study the effect of intake flow distortion on fan buzz-saw noise. Three cases have been investigated, namely a baseline case, an axisymmetric distorted case, and a drooped distorted case, and comparisons have been made on the intake noise data extracted from the CFD calculations. The distortion fields generated in the last two cases have been compared and characterised by Fourier-Bessel harmonics. The results show that the distortion generated in the drooped case is more significant and has resulted in stronger circumferential mode scattering appearing initially in the fan domain. The main effect of the distortions in both cases is to cause scattering of the rotor-locked modes into adjacent circumferential harmonics, as the shock waves propagate through the intake ducts.

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More information

Published date: 30 May 2024
Venue - Dates: 30th AIAA/CEAS Aeroacoustics Conference, 2024, , Rome, Italy, 2024-06-04 - 2024-06-07

Identifiers

Local EPrints ID: 497376
URI: http://eprints.soton.ac.uk/id/eprint/497376
PURE UUID: 24a492dc-8e6c-4b18-8a37-d6c275467041
ORCID for Long Wu: ORCID iD orcid.org/0009-0006-8578-7755

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Date deposited: 21 Jan 2025 17:48
Last modified: 22 Jan 2025 03:00

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Author: Long Wu ORCID iD

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