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contributor authorD. C. Wisler
contributor authorR. C. Bauer
contributor authorT. H. Okiishi
date accessioned2017-05-08T23:25:58Z
date available2017-05-08T23:25:58Z
date copyrightOctober, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28586#455_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103185
description abstractThe relative importance of convection by secondary flows and diffusion by turbulence as mechanisms responsible for mixing in multistage, axial-flow compressors has been investigated by using the ethylene tracer-gas technique and hot-wire anemometry. The tests were conducted at two loading levels in a large, low-speed, four-stage compressor. The experimental results show that considerable cross-passage and spanwise fluid motion can occur and that both secondary flow and turbulent diffusion can play important roles in the mixing process, depending upon location in the compressor and loading level. In the so-called freestream region, turbulent diffusion appeared to be the dominant mixing mechanism. However, near the endwalls and along airfoil surfaces at both loading levels, the convective effects from secondary flow were of the same order of magnitude as, and in some cases greater than, the diffusive effects from turbulence. Calculations of the secondary flowfield and mixing coefficients support the experimental findings.
publisherThe American Society of Mechanical Engineers (ASME)
titleSecondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors
typeJournal Paper
journal volume109
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262127
journal fristpage455
journal lastpage469
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 004
contenttypeFulltext


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