Computation of spinning modal radiation from an unflanged duct
Computation of spinning modal radiation from an unflanged duct
The radiation of high-order spinning modes from an unflanged duct with or without a mean flow is studied
numerically. The application is to noise radiation from the intake duct of an aircraft engine. The numerical
method is based on solutions of the linearized Euler equations (LEE) for propagation in the duct and near field
and the acoustic analogy for far-field radiation. A formulation of the LEE is used for a single azimuthal mode,
which offers an advantage in terms of computational efficiency: in the case of an axisymmetric mean flow-field,
this model reduces computing costs connected with a three-dimensional model. In the solution process, acoustic
waves are admitted from upstream into the propagation area surrounding the exit of an axisymmetric duct and
the region immediately downstream. The wave admission is realized through an absorbing nonreflecting boundary
treatment, which admits incoming waves and damps spurious waves generated by the numerical solutions. The
wave propagation is calculated using a high-order compact scheme. Far-field directivity is estimated by solving
the Ffowcs Williams–Hawkings equations. The far-field prediction is compared with analytic solutions, and good
agreement is found.
1795-1801
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Chen, X.
1c7ce635-f117-4cb5-8f61-cb6a9b23d8a5
Morfey, C.L.
d5f9a8d0-7d8a-4915-a522-bf49dee111f2
Nelson, P.A.
5c6f5cc9-ea52-4fe2-9edf-05d696b0c1a9
2004
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Chen, X.
1c7ce635-f117-4cb5-8f61-cb6a9b23d8a5
Morfey, C.L.
d5f9a8d0-7d8a-4915-a522-bf49dee111f2
Nelson, P.A.
5c6f5cc9-ea52-4fe2-9edf-05d696b0c1a9
Zhang, Xin, Chen, X., Morfey, C.L. and Nelson, P.A.
(2004)
Computation of spinning modal radiation from an unflanged duct.
AIAA Journal, 42 (9), .
Abstract
The radiation of high-order spinning modes from an unflanged duct with or without a mean flow is studied
numerically. The application is to noise radiation from the intake duct of an aircraft engine. The numerical
method is based on solutions of the linearized Euler equations (LEE) for propagation in the duct and near field
and the acoustic analogy for far-field radiation. A formulation of the LEE is used for a single azimuthal mode,
which offers an advantage in terms of computational efficiency: in the case of an axisymmetric mean flow-field,
this model reduces computing costs connected with a three-dimensional model. In the solution process, acoustic
waves are admitted from upstream into the propagation area surrounding the exit of an axisymmetric duct and
the region immediately downstream. The wave admission is realized through an absorbing nonreflecting boundary
treatment, which admits incoming waves and damps spurious waves generated by the numerical solutions. The
wave propagation is calculated using a high-order compact scheme. Far-field directivity is estimated by solving
the Ffowcs Williams–Hawkings equations. The far-field prediction is compared with analytic solutions, and good
agreement is found.
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Published date: 2004
Identifiers
Local EPrints ID: 22951
URI: http://eprints.soton.ac.uk/id/eprint/22951
ISSN: 0001-1452
PURE UUID: a18cb913-3d5d-4ec7-b90c-8ea661ed22cd
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Date deposited: 23 Mar 2006
Last modified: 18 Mar 2022 02:32
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Author:
Xin Zhang
Author:
C.L. Morfey
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