TY - CONF
T1 - A generalized sound extrapolation method for turbulent flows
T2 - Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences
AU - Zhong, S.
AU - Zhang, X.
N1 - Export Date: 12 January 2023; Cited By: 16; Correspondence Address: S. Zhong; Department of Mechanical and Aerospace Engineering, Hong Kong University of Science and Technology, Kowloon, Clear Water Bay, Hong Kong; email: [email protected]
PY - 2018
Y1 - 2018
N2 - Sound extrapolation methods are often used to compute acoustic far-field directivities using nearfield flow data in aeroacoustics applications. The results may be erroneous if the volume integrals are neglected (to save computational cost), while non-acoustic fluctuations are collected on the integration surfaces. In this work, we develop a new sound extrapolation method based on an acoustic analogy using Taylor’s hypothesis (Taylor 1938 Proc. R. Soc. Lon. A 164, 476–490. (doi:10.1098/rspa.1938.0032)). Typically, a convection operator is used to filter out the acoustically inefficient components in the turbulent flows, and an acoustics dominant indirect variable Dcp is solved. The sound pressure p at the far field is computed from Dcp based on the asymptotic properties of the Green’s function. Validations results for benchmark problems with well-defined sources match well with the exact solutions. For aeroacoustics applications: the sound predictions by the aerofoil–gust interaction are close to those by an earlier method specially developed to remove the effect of vortical fluctuations (Zhong & Zhang 2017 J. Fluid Mech. 820, 424–450. (doi:10.1017/jfm.2017.219)); for the case of vortex shedding noise from a cylinder, the off-body predictions by the proposed method match well with the on-body Ffowcs-Williams and Hawkings result; different integration surfaces yield close predictions (of both spectra and far-field directivities) for a co-flowing jet case using an established direct numerical simulation database. The results suggest that the method may be a potential candidate for sound projection in aeroacoustics applications. ©2018 The Author(s) Published by the Royal Society. All rights reserved.
AB - Sound extrapolation methods are often used to compute acoustic far-field directivities using nearfield flow data in aeroacoustics applications. The results may be erroneous if the volume integrals are neglected (to save computational cost), while non-acoustic fluctuations are collected on the integration surfaces. In this work, we develop a new sound extrapolation method based on an acoustic analogy using Taylor’s hypothesis (Taylor 1938 Proc. R. Soc. Lon. A 164, 476–490. (doi:10.1098/rspa.1938.0032)). Typically, a convection operator is used to filter out the acoustically inefficient components in the turbulent flows, and an acoustics dominant indirect variable Dcp is solved. The sound pressure p at the far field is computed from Dcp based on the asymptotic properties of the Green’s function. Validations results for benchmark problems with well-defined sources match well with the exact solutions. For aeroacoustics applications: the sound predictions by the aerofoil–gust interaction are close to those by an earlier method specially developed to remove the effect of vortical fluctuations (Zhong & Zhang 2017 J. Fluid Mech. 820, 424–450. (doi:10.1017/jfm.2017.219)); for the case of vortex shedding noise from a cylinder, the off-body predictions by the proposed method match well with the on-body Ffowcs-Williams and Hawkings result; different integration surfaces yield close predictions (of both spectra and far-field directivities) for a co-flowing jet case using an established direct numerical simulation database. The results suggest that the method may be a potential candidate for sound projection in aeroacoustics applications. ©2018 The Author(s) Published by the Royal Society. All rights reserved.
KW - Acoustic emissions
KW - Acoustic properties
KW - Acoustic waves
KW - Acoustics
KW - Aeroacoustics
KW - Computational aeroacoustics
KW - Extrapolation
KW - Fighter aircraft
KW - Forecasting
KW - Numerical methods
KW - Turbulent flow
KW - Vortex flow
KW - Vortex shedding
KW - Acoustic analogy
KW - Acoustic fluctuations
KW - Aeroacoustics applications
KW - Asymptotic properties
KW - Extrapolation methods
KW - Integration surfaces
KW - Jet noise
KW - Vortex shedding noise
KW - Acoustic noise
KW - Aerofoil noise
KW - Wave extrapolation
U2 - 10.1098/rspa.2017.0614
DO - 10.1098/rspa.2017.0614
M3 - Conference presentation (not published in journal/proceeding/book)
ER -