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contributor authorRoque Corral
contributor authorFernando Gisbert
date accessioned2017-05-09T00:11:38Z
date available2017-05-09T00:11:38Z
date copyrightJuly, 2003
date issued2003
identifier issn0889-504X
identifier otherJOTUEI-28704#433_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129237
description abstractThe effect of the finite extent of linear cascades on the unsteady pressure distribution of vibrating blades is assessed by means of a numerical study. The span of a reference cascade made up of flat plates has been changed to investigate its influence on the computed influence coefficients. It is concluded that the number of passages required to match a solution obtained with a traveling-wave mode strongly depends on the interblade phase angle under consideration and that existing linear vibrating cascade facilities have a marginal resolution to accurately match CFD analysis that assume that the blade is vibrating in a traveling-wave mode.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Numerical Investigation on the Influence of Lateral Boundaries in Linear Vibrating Cascades
typeJournal Paper
journal volume125
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1575255
journal fristpage433
journal lastpage441
identifier eissn1528-8900
keywordsCascades (Fluid dynamics)
keywordsWaves
keywordsBlades
keywordsPressure
keywordsTravel
keywordsFlow (Dynamics)
keywordsFlat plates AND Boundary-value problems
treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 003
contenttypeFulltext


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