Time-domain impedance boundary conditions for computational acoustics and aeroacoustics
KY Fung, H Ju - International Journal of Computational Fluid …, 2004 - Taylor & Francis
This paper reviews the short history, motivation, numerical and theoretical issues, and
development of methods for treating a boundary as a reflective/absorptive surface for the …
development of methods for treating a boundary as a reflective/absorptive surface for the …
[HTML][HTML] A systematic literature review on Lattice Boltzmann Method applied to acoustics
Abstract The Lattice Boltzmann Method (LBM) can be applied to several fluid dynamic
problems in the time domain. This numerical method indirectly solves the Navier–Stokes …
problems in the time domain. This numerical method indirectly solves the Navier–Stokes …
Impedance models in time domain, including the extended Helmholtz resonator model
S Rienstra - 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA …, 2006 - arc.aiaa.org
An explicit solution is given of a pulse reflecting in time domain at a Helmholtz resonator
impedance wall that provides some insight into the reflection problem in time domain and at …
impedance wall that provides some insight into the reflection problem in time domain and at …
Fundamental problems with the model of uniform flow over acoustic linings
EJ Brambley - Journal of Sound and Vibration, 2009 - Elsevier
The walls of ducts containing flow are often acoustically lined in order to reduce sound.
Many simple models of acoustic linings assume the lining to be linear and locally reacting; …
Many simple models of acoustic linings assume the lining to be linear and locally reacting; …
Compressible turbulent channel flow with impedance boundary conditions
We have performed large-eddy simulations of isothermal-wall compressible turbulent
channel flow with linear acoustic impedance boundary conditions (IBCs) for the wall-normal …
channel flow with linear acoustic impedance boundary conditions (IBCs) for the wall-normal …
Broadband time-domain impedance models
KY Fung, H Ju - AIAA journal, 2001 - arc.aiaa.org
The modeling of a set of impedance values given either experimentally or heuristically for
implementation as a time-domain impedance-equivalent boundary condition (TDIBC) is …
implementation as a time-domain impedance-equivalent boundary condition (TDIBC) is …
Design of broadband time-domain impedance boundary conditions using the oscillatory-diffusive representation of acoustical models
F Monteghetti, D Matignon, E Piot… - The Journal of the …, 2016 - pubs.aip.org
A methodology to design broadband time-domain impedance boundary conditions (TDIBCs)
from the analysis of acoustical models is presented. The derived TDIBCs are recast …
from the analysis of acoustical models is presented. The derived TDIBCs are recast …
Time-domain characterization of the acoustic damping of a perforated liner with bias flow
Z Zhong, D Zhao - The Journal of the Acoustical Society of America, 2012 - pubs.aip.org
Combustion instabilities are caused by the interaction of unsteady heat releases and
acoustic waves. To mitigate combustion instabilities, perforated liners, typically subjected to …
acoustic waves. To mitigate combustion instabilities, perforated liners, typically subjected to …
Trapped waves in supersonic and hypersonic turbulent channel flow over porous walls
Y Chen, C Scalo - Journal of Fluid Mechanics, 2021 - cambridge.org
Trapped waves in supersonic and hypersonic turbulent channel flow over porous walls Page 1
J. Fluid Mech. (2021), vol. 920, A24, doi:10.1017/jfm.2021.428 Trapped waves in supersonic …
J. Fluid Mech. (2021), vol. 920, A24, doi:10.1017/jfm.2021.428 Trapped waves in supersonic …
Comparison of time-domain impedance boundary conditions for lined duct flows
C Richter, FH Thiele, XD Li, M Zhuang - AIAA journal, 2007 - arc.aiaa.org
AEROENGINE noise reduction is, in today's turbine design, achieved principally by using
passive-acoustic treatments. Reductions of noise in the forward arc of aeroengines are …
passive-acoustic treatments. Reductions of noise in the forward arc of aeroengines are …