Aeroacoustic analysis using natural Helmholtz–Hodge decomposition
The analysis of aeroacoustic phenomena is crucial for a deeper understanding of the damping mechanisms of a sound-absorbing bias flow liner (BFL). For this purpose, simultaneous measurements of the sound field and the flow field in a BFL are required. The fluid velocity can serve as the measurand...
Main Authors: | , , , , , |
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Format: | Article |
Language: | English |
Published: |
Copernicus Publications
2018-03-01
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Series: | Journal of Sensors and Sensor Systems |
Online Access: | https://www.j-sens-sens-syst.net/7/113/2018/jsss-7-113-2018.pdf |
Summary: | The analysis of aeroacoustic phenomena is crucial for a deeper understanding
of the damping mechanisms of a sound-absorbing bias flow liner (BFL). For
this purpose, simultaneous measurements of the sound field and the flow field
in a BFL are required. The fluid velocity can serve as the measurand, where both
the acoustic particle velocity and the aerodynamic flow velocity contribute and, thus, can be acquired simultaneously. However, there is
a need to separate these two quantities to distinguish between them. This is
challenging because they generally coincide with each other in the time
domain. Due to the interaction of sound and flow in a BFL, both velocities
also overlap in the temporal frequency domain, having a coherent oscillation
at the acoustic frequency. For this reason, the recently developed natural
Helmholtz–Hodge decomposition (NHHD) is applied to separate both quantities
from the measured oscillation velocity field in the spatial domain. The
evaluation of synthetic vector field data shows that the quality of the
decomposition is enhanced when a smaller grid size is chosen. The velocity
field in a generic BFL, necessarily recorded within a three-dimensional
region of interest at more than 4000 measurement locations, is evaluated
using NHHD. As a result, the measured oscillation velocity in the BFL is
dominated by the flow that is related to vortices and also by irrotational
aerodynamic flow. Moreover, indications for an aeroacoustic source near the
facing sheet of the liner are revealed. |
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ISSN: | 2194-8771 2194-878X |