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contributor authorY. Nakata
contributor authorJ. Y. Murthy
contributor authorD. E. Metzger
date accessioned2017-05-08T23:39:50Z
date available2017-05-08T23:39:50Z
date copyrightOctober, 1992
date issued1992
identifier issn0889-504X
identifier otherJOTUEI-28625#881_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111053
description abstractConvection heat transfer phenomena on rotating disks are of general interest in relation to turbomachineray design. In gas turbine engines, for example, knowledge of the temperature distribution on turbine disks that are bounded by a fluid cavity is required to predict stresses and durability. Cooling air is generally provided by the compressor section and routed to the turbine disk cavities where it is utilized for cooling both the rotating and stationary components. Since the production and pumping of the compressed cooling air imposes performance penalties on the engine cycle, a goal of the designer is always to minimize cooling air consumption. This requirement produces a need for accurate and detailed knowledge of the convection heat transfer and flow characteristics associated with disk cavity flows for a large variety of possible cooling configurations. In the past, most reliable information on disk cavity flow and heat transfer has been derived from empirical studies, but the large range of possible geometries and flow conditions precludes a complete coverage by experiment alone. In the future, it should be possible to supplement disk cavity flow experiments with numerical computations both to aid in interpretation of and to extend empirical results. The present numerical study of laminar flow cases is intended to complement previous experimental information for disk convection with jet impingment. The computational method is described and applied first to a baseline case of a rotating disk in an enclosure where results are found to compare favorably with the experiments of Daily and Nece. The two-dimensional approach used to model the inclusion of an impinging jet is described, and the computational method is applied to predict both flow and heat transfer characteristics in the vicinity of the interaction between impinging jet and rotating disk. The computed results partition into impingment-dominated and rotational-dominated regimes similar to the findings of prior experimental studies.
publisherThe American Society of Mechanical Engineers (ASME)
titleComputation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement
typeJournal Paper
journal volume114
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2928043
journal fristpage881
journal lastpage890
identifier eissn1528-8900
keywordsHeat transfer
keywordsLaminar flow
keywordsComputation
keywordsRotating Disks
keywordsDisks
keywordsCooling
keywordsCavity flows
keywordsConvection
keywordsFlow (Dynamics)
keywordsTurbines
keywordsCavities
keywordsComputational methods
keywordsTemperature distribution
keywordsCycles
keywordsStress
keywordsInterior walls
keywordsDesign
keywordsDurability
keywordsGas turbines
keywordsFluids
keywordsEngines AND Compressors
treeJournal of Turbomachinery:;1992:;volume( 114 ):;issue: 004
contenttypeFulltext


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