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contributor authorJ. Nordquist
contributor authorS. Abrahamson
contributor authorJ. Wechkin
contributor authorJ. Eaton
date accessioned2017-05-08T23:34:09Z
date available2017-05-08T23:34:09Z
date copyrightApril, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28601#308_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107772
description abstractAn experimental study was performed in a simplified turbine disk cavity consisting of a single disk rotating near a stationary flat plate, bounded radially by an axial seal fixed to the plate. The disk Reynolds number was 6.2 × 105 . Cooling flow was supplied axially at a dimensionless radius of 0.33. Flow visualization showed boundary layers on both the rotating and stationary disks with the core between the layers rotating in solid body motion. At intermediate cooling flow rates, large vortical structures aligned with the disk spin axis and spanning the core were observed.
publisherThe American Society of Mechanical Engineers (ASME)
titleVisualization Studies in Rotating Disk Cavity Flows
typeJournal Paper
journal volume112
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927656
journal fristpage308
journal lastpage310
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsCooling
keywordsMotion
keywordsReynolds number
keywordsFlow visualization
keywordsParticle spin
keywordsBoundary layers
keywordsCavity flows
keywordsTurbines
keywordsVisualization
keywordsDisks
keywordsCavities
keywordsFlat plates AND Rotating Disks
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 002
contenttypeFulltext


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