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contributor authorXin Yan
contributor authorJun Li
contributor authorLiming Song
contributor authorZhenping Feng
date accessioned2017-05-09T00:35:45Z
date available2017-05-09T00:35:45Z
date copyrightOctober, 2009
date issued2009
identifier issn0889-504X
identifier otherJOTUEI-28758#041009_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142139
description abstractThe viscous work generated by the rotating components of a seal not only represents a direct loss of power but also causes an increase in the total temperature of fluid (windage effect). In order to study the discharge and total temperature increase characteristics of the stepped labyrinth seals with smooth and honeycomb lands, 3D Reynolds-averaged Navier–Stokes solutions from CFX is used in this work. At first, the influences of the inlet preswirl, leakage flow rate, and rotational speed on the total temperature increase in the convergent and divergent stepped labyrinth seals with smooth and honeycomb lands are conducted. The obtained 3D numerical results are well in agreement with the referenced experimental data. It shows that the utilized numerical approach has sufficient precision to predict the total temperature increase in seals. Then, a range of pressure ratios and four sizes of sealing clearance are performed to investigate the effects of sealing clearances and pressure ratio impact on the discharge and total temperature increase of the stepped labyrinth seals with honeycomb and smooth liners.
publisherThe American Society of Mechanical Engineers (ASME)
titleInvestigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals With Honeycomb and Smooth Lands
typeJournal Paper
journal volume131
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3068320
journal fristpage41009
identifier eissn1528-8900
keywordsPressure
keywordsFlow (Dynamics)
keywordsTemperature
keywordsClearances (Engineering)
keywordsHeating
keywordsSealing (Process)
keywordsLeakage flows AND Leakage
treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 004
contenttypeFulltext


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