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contributor authorJ. A. Demko
contributor authorG. L. Morrison
contributor authorD. L. Rhode
date accessioned2017-05-08T23:29:52Z
date available2017-05-08T23:29:52Z
date copyrightOctober, 1989
date issued1989
identifier issn1528-8919
identifier otherJETPEZ-26672#697_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105347
description abstractPredictions and measurements were obtained for incompressible flow in a labyrinth seal for Taylor numbers of 0, 7,600, and 19,000 at an axial Reynolds number near 50,000. A hot-film anemometer with computer data acquisition was used in obtaining the measurements. The computations were made using a turbulent flow Navier-Stokes finite difference code. The QUICK differencing scheme was utilized in order to diminish false diffusion. Comparison between experiments and predictions are given for the axial and swirl velocity components and turbulent kinetic energy. Also, the substantial effect of the Taylor number on the pressure distribution is presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Prediction and Measurement of Incompressible Flow in a Labyrinth Seal
typeJournal Paper
journal volume111
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3240315
journal fristpage697
journal lastpage702
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsMeasurement
keywordsTurbulence
keywordsKinetic energy
keywordsReynolds number
keywordsComputers
keywordsComputation
keywordsData acquisition
keywordsDiffusion (Physics) AND Pressure
treeJournal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 004
contenttypeFulltext


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