Acoustic modeling of perforated plates with bias flow for large eddy simulations

DOI10.1016/j.jcp.2009.03.026zbMath1166.76050OpenAlexW1970158002MaRDI QIDQ2390426

Jeff. D. Eldredge, Simon Mendez

Publication date: 22 July 2009

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jcp.2009.03.026

zbMATH Keywords

combustion chambersthermo-acoustic instabilitiesacoustic damping

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05) Combustion (80A25) Reaction effects in flows (76V05)

Related Items (4)

Numerical study of acoustic multiperforated plates ⋮ Large eddy simulation of a motored single-cylinder piston engine: numerical strategies and validation ⋮ The acoustic impedance of a laminar viscous jet through a thin circular aperture ⋮ Effective conditions for the reflection of an acoustic wave by low-porosity perforated plates

Uses Software

• AVBP

Cites Work

• Numerical methods for unsteady compressible multi-component reacting flows on fixed and moving grids
• Boundary conditions for direct simulations of compressible viscous flows
• Development of high-order Taylor-Galerkin schemes for LES
• Subgrid-scale stress modelling based on the square of the velocity gradient tensor
• The influence of tangential mean flow on the Rayleigh conductivity of an aperture
• On the theory of unsteady high Reynolds number flow through a circular aperture
• High amplitude acoustic transmission through duct terminations: Theory
• Large-eddy simulation and experimental study of heat transfer, nitric oxide emissions and combustion instability in a swirled turbulent high-pressure burner
• Large-eddy simulation of a bi-periodic turbulent flow with effusion
• A thickened flame model for large eddy simulations of turbulent premixed combustion
• Acoustics of Fluid-Structure Interactions
• Time-domain impedance boundary conditions for computational aeroacoustics
• The absorption of axial acoustic waves by a perforated liner with bias flow
• Progress-variable approach for large-eddy simulation of non-premixed turbulent combustion

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