Acoustic effects of liner damage on zero-splice turbofan intake liners: Computational study
Acoustic effects of liner damage on zero-splice turbofan intake liners: Computational study
Traditional installations of turbofan intake liners include acoustically hard axial splices between liner segments for ease of fabrication and assembly. The splices scatter energy from strong rotor-locked tones into adjacent azimuthal orders for which the liner is less effective, thereby degrading the liner performance. The significance of this splice effect has led to the adoption of zero-splice liners in recent turbofan nacelles. However, damage can occur to such liners in service, and the extent to which local liner repairs reduce the effectiveness of the zero-splice design then becomes an issue. In the current paper, the acoustic effect of damage and repair in a zero-splice liner is simulated numerically. The effects of the extent and the location of a hard patch, representing the liner damage and repair, on the overall performance of the liner are predicted. A close agreement is demonstrated with results from an asymptotic analytical model valid for small patch widths. An approximate method is also described to account for the effect of the nonlinear propagation on linear predictions of the liner performance when repairs are present.
BUZZ-SAW NOISE, AEROENGINE INLET DUCTS, SOUND-PROPAGATION, PREDICTION, ATTENUATION, SCATTERING, flow
703-712
Mustafi, Prateek
c1f218a6-38fc-499a-98a4-c92e36350122
Astley, Richard Jeremy
cb7fed9f-a96a-4b58-8939-6db1010f9893
Sugimoto, Rie
cb8c880d-0be0-4efe-9990-c79faa8804f0
Kempton, Andrew J
08276625-e640-431b-8dd3-1598fe5ec722
March 2015
Mustafi, Prateek
c1f218a6-38fc-499a-98a4-c92e36350122
Astley, Richard Jeremy
cb7fed9f-a96a-4b58-8939-6db1010f9893
Sugimoto, Rie
cb8c880d-0be0-4efe-9990-c79faa8804f0
Kempton, Andrew J
08276625-e640-431b-8dd3-1598fe5ec722
Mustafi, Prateek, Astley, Richard Jeremy, Sugimoto, Rie and Kempton, Andrew J
(2015)
Acoustic effects of liner damage on zero-splice turbofan intake liners: Computational study.
AIAA Journal, 53 (3), .
(doi:10.2514/1.J053219).
Abstract
Traditional installations of turbofan intake liners include acoustically hard axial splices between liner segments for ease of fabrication and assembly. The splices scatter energy from strong rotor-locked tones into adjacent azimuthal orders for which the liner is less effective, thereby degrading the liner performance. The significance of this splice effect has led to the adoption of zero-splice liners in recent turbofan nacelles. However, damage can occur to such liners in service, and the extent to which local liner repairs reduce the effectiveness of the zero-splice design then becomes an issue. In the current paper, the acoustic effect of damage and repair in a zero-splice liner is simulated numerically. The effects of the extent and the location of a hard patch, representing the liner damage and repair, on the overall performance of the liner are predicted. A close agreement is demonstrated with results from an asymptotic analytical model valid for small patch widths. An approximate method is also described to account for the effect of the nonlinear propagation on linear predictions of the liner performance when repairs are present.
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Accepted/In Press date: 2014
e-pub ahead of print date: 12 August 2014
Published date: March 2015
Keywords:
BUZZ-SAW NOISE, AEROENGINE INLET DUCTS, SOUND-PROPAGATION, PREDICTION, ATTENUATION, SCATTERING, flow
Identifiers
Local EPrints ID: 426806
URI: http://eprints.soton.ac.uk/id/eprint/426806
ISSN: 0001-1452
PURE UUID: 7bfccaf9-de4e-4167-91d0-450c5eed9e74
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Date deposited: 12 Dec 2018 17:31
Last modified: 16 Mar 2024 03:36
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Author:
Prateek Mustafi
Author:
Andrew J Kempton
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