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contributor authorA. J. Cooper
contributor authorA. B. Parry
contributor authorN. Peake
date accessioned2017-05-09T00:14:40Z
date available2017-05-09T00:14:40Z
date copyrightJuly, 2004
date issued2004
identifier issn0889-504X
identifier otherJOTUEI-28711#432_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130981
description abstractA 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleAcoustic Resonance in Aeroengine Intake Ducts
typeJournal Paper
journal volume126
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1776586
journal fristpage432
journal lastpage441
identifier eissn1528-8900
keywordsResonance
keywordsFlow (Dynamics)
keywordsAcoustics
keywordsRotors
keywordsDucts
keywordsStators
keywordsShapes
keywordsWaves AND Swirling flow
treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 003
contenttypeFulltext


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