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Acoustic resonance in aeroengine intake ducts

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UNSPECIFIED. (2004) Acoustic resonance in aeroengine intake ducts. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 126 (3). pp. 432-441. ISSN 0889-504X

Full text not available from this repository.
Official URL: http://dx.doi.org/10.1115/1.1776586

Abstract

A theoretical model is used to investigate the effect of geometry, flow conditions and acoustic lining on the occurrence of acoustic resonance within aeroengine ducts. Semi-analytical methods are used to demonstrate that two types of acoustic resonance can be excited. The first is an intake resonance arising due to axial variation of the intake shape and the presence of swirling flow downstream of the rotor. The second occurs as a result of mode trapping between the rotor and stator. Such resonance phenomena may be relevant to the destabilization of the fan and the onset of flutter and rotating stall.

Item Type: Journal Article
Subjects: T Technology > TJ Mechanical engineering and machinery
Journal or Publication Title: JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Publisher: ASME-AMER SOC MECHANICAL ENG
ISSN: 0889-504X
Date: July 2004
Volume: 126
Number: 3
Number of Pages: 10
Page Range: pp. 432-441
Identification Number: 10.1115/1.1776586
Publication Status: Published
URI: http://wrap.warwick.ac.uk/id/eprint/7958

Data sourced from Thomson Reuters' Web of Knowledge

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