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Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/18614

Title: Large Eddy Simulation of acoustic pulse propagation and turbulent flow interaction in expansion mufflers
Authors: Singh, Nishant K.
Rubini, Philip A.
Keywords: Low Mach number flow
Noise attenuation
Synthetic turbulence
Compressible Navier–Stokes
URANS
LES
Issue Date: 2015
Publisher: © Elsevier
Citation: SINGH, N.K. and RUBINI, P.A., 2015. Large Eddy Simulation of acoustic pulse propagation and turbulent flow interaction in expansion mufflers. Applied Acoustics, 98 pp.6-19
Abstract: A novel hybrid pressure-based compressible solver is developed and validated for low Mach number acoustic flow simulation. The solver is applied to the propagation of an acoustic pulse in a simple expansion muffler, a configuration frequently employed in HVAC and automotive exhaust systems. A set of benchmark results for experimental analysis of the simple expansion muffler both with and without flow are obtained to compare attenuation in forced pulsation for various mean-flow velocities. The experimental results are then used for validation of the proposed pressure-based compressible solver. Compressible, Unsteady Reynolds Averaged Navier–Stokes (URANS) simulation of a muffler with a mean through flow is conducted and results are presented to demonstrate inherent limitations associated with this approach. Consequently, a mixed synthetic inflow boundary condition is developed and validated for compressible Large Eddy Simulation (LES) of channel flow. The mixed synthetic boundary is then employed for LES of a simple expansion muffler to analyse the flow-acoustic and acoustic-pulse interactions inside the expansion muffler. The improvement in the prediction of vortex shedding inside the chamber is highlighted in comparison to the URANS method. Further, the effect of forced pulsation on flow-acoustic is observed in regard to the shift in Strouhal number inside the simple expansion muffler.
Version: Accepted for publication
DOI: 10.1016/j.apacoust.2015.04.015
URI: https://dspace.lboro.ac.uk/2134/18614
Publisher Link: http://dx.doi.org/10.1016/j.apacoust.2015.04.015
ISSN: 1872-910X
Appears in Collections:Published Articles (Aeronautical and Automotive Engineering)

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