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contributor authorT. Valkov
contributor authorC. S. Tan
date accessioned2017-05-08T23:48:39Z
date available2017-05-08T23:48:39Z
date copyrightJanuary, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28642#97_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116175
description abstractA computational approach, based on a spectral-element Navier–Stokes solver, has been applied to the study of the unsteady flow arising from wake–stator interaction. Direct, as well as turbulence-model calculations, provide insight into the mechanics of the unsteady flow and demonstrate the potential for controlling its effects. The results show that the interaction between the wakes and the stator blades produces a characteristic pattern of vortical disturbances, which have been correlated to the pressure fluctuations. Within the stator passage, the wakes migrate toward the pressure surface where they evolve into counterrotating vortices. These vortices are the dominant source of disturbances over the pressure surface of the stator blade. Over the suction surface of the stator blade, the disturbances are due to the distortion and detachment of boundary layer fluid. They can be reduced by tailoring the blade loading or by applying nonuniform suction.
publisherThe American Society of Mechanical Engineers (ASME)
titleControl of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes
typeJournal Paper
journal volume117
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2835647
journal fristpage97
journal lastpage105
identifier eissn1528-8900
keywordsWakes
keywordsBlades
keywordsStators
keywordsUnsteady flow
keywordsPressure
keywordsSuction
keywordsVortices
keywordsFluctuations (Physics)
keywordsFluids
keywordsTurbulence AND Boundary layers
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
contenttypeFulltext


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