An acoustically-tuned spectral proper orthogonal decomposition

A new method to construct efficient reduced-order models for far-field radiation from a turbulent round jet over a wide band of frequencies and directivity angles is proposed here. It leverages the property of the free-space Green’s function, often employed in the solution to the Lighthill's equation, in extracting the acoustic component from the Lighthill's equivalent near-field sources. The methodology is referred to here as the “Lighthill Spectral Proper Orthogonal Decomposition” or LSPOD. The process yields sharply low-rank LSPOD modes that recovers up to 95% of the acoustic fluctuations energy with just five modes for St ≲ 1. The LSPOD mode shapes resemble acoustic waves emanating from the jet’s breakdown location, very different to the wavepacket shapes of typical near-field fluctuations-based SPOD modes. Remarkably, the leading LSPOD mode alone reconstructs the far-field spectra at the peak radiation angle of ϕ = 30° to within 1 dB accuracy across all frequencies considered here. In fact, the OASPL results show that eight LSPOD modes are able to consistently recover the radiated sound pressure at all observer angles, even at sideline and upstream angles, within a single decibel error.

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Publication Details

Journal
International Journal of Aeroacoustics
Published
2025-10-08
DOI
https://doi.org/10.1177/1475472x251382213
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
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article

An acoustically-tuned spectral proper orthogonal decomposition

Nishanth Muthichur, Arnab Samanta, Santosh Hemchandra, Chandan Vempati
International Journal of Aeroacoustics
Aerodynamics and Acoustics in Jet Flows
article

An acoustically-tuned spectral proper orthogonal decomposition

Nishanth Muthichur, Arnab Samanta, Santosh Hemchandra, Chandan Vempati
article en

Abstract

A new method to construct efficient reduced-order models for far-field radiation from a turbulent round jet over a wide band of frequencies and directivity angles is proposed here. It leverages the property of the free-space Green’s function, often employed in the solution to the Lighthill's equation, in extracting the acoustic component from the Lighthill's equivalent near-field sources. The methodology is referred to here as the “Lighthill Spectral Proper Orthogonal Decomposition” or LSPOD. The process yields sharply low-rank LSPOD modes that recovers up to 95% of the acoustic fluctuations energy with just five modes for St ≲ 1. The LSPOD mode shapes resemble acoustic waves emanating from the jet’s breakdown location, very different to the wavepacket shapes of typical near-field fluctuations-based SPOD modes. Remarkably, the leading LSPOD mode alone reconstructs the far-field spectra at the peak radiation angle of ϕ = 30° to within 1 dB accuracy across all frequencies considered here. In fact, the OASPL results show that eight LSPOD modes are able to consistently recover the radiated sound pressure at all observer angles, even at sideline and upstream angles, within a single decibel error.

International Journal of AeroacousticsVol. 24(7-8)
Indian Institute of Science Bangalore (IN), Indian Institute of Technology Kanpur (IN)
Openalex Percentile: Top 63%
Aerodynamics and Acoustics in Jet Flows
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