In this study, the parameters of a wave-packet model for subsonic jet noise prediction are systematically optimized by leveraging near-and far-field data obtained from the large-eddy simulation (LES) of a free jet at a Mach number of 0.9 across various radial distances. The utilization of near-field information is justified by the observation that the scattering surfaces are typically situated within a few nozzle diameters from the jet axis in the radial direction, both in the current and in innovative aircraft configurations. The far-field information is used to guarantee the correct subdivision between the wave-packet radiating noise and the hydrodynamic components. The results show a notable agreement between the LES data and the wave-packet solutions, consistent with findings documented in the existing literature. This agreement underscores the validity and applicability of the implemented methodology, offering an effective method for obtaining an equivalent jet noise acoustic source, easily implementable in acoustic scattering codes, and accounting for the directional behavior of jet noise.

Subsonic Jet Noise Prediction in Near and Far Field with Optimized Wave-Packet Approach

Palma G.
Primo
;
2024

Abstract

In this study, the parameters of a wave-packet model for subsonic jet noise prediction are systematically optimized by leveraging near-and far-field data obtained from the large-eddy simulation (LES) of a free jet at a Mach number of 0.9 across various radial distances. The utilization of near-field information is justified by the observation that the scattering surfaces are typically situated within a few nozzle diameters from the jet axis in the radial direction, both in the current and in innovative aircraft configurations. The far-field information is used to guarantee the correct subdivision between the wave-packet radiating noise and the hydrodynamic components. The results show a notable agreement between the LES data and the wave-packet solutions, consistent with findings documented in the existing literature. This agreement underscores the validity and applicability of the implemented methodology, offering an effective method for obtaining an equivalent jet noise acoustic source, easily implementable in acoustic scattering codes, and accounting for the directional behavior of jet noise.
2024
Istituto di iNgegneria del Mare - INM (ex INSEAN)
Computational Fluid Dynamics
Aircraft Noise
Aircraft Components and Structure
Jet Noise
Aeroacoustics
Turbulent-Jet Wave Packets
Inverse Problems
Acoustic Scattering
Multi-Objective Evolutionary Algorithms
Reduced Order Model
File in questo prodotto:
File Dimensione Formato  
_AIAAJ_Subsonic_Jet_Noise_Prediction_in_Near_and_Far_Field_with_Optimized_Wave_Packet_Approach (1).pdf

accesso aperto

Descrizione: accepted manuscript
Tipologia: Documento in Post-print
Licenza: Creative commons
Dimensione 2.55 MB
Formato Adobe PDF
2.55 MB Adobe PDF Visualizza/Apri

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/526862
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 0
  • ???jsp.display-item.citation.isi??? 0
social impact