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    Secondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004::page 455
    Author:
    D. C. Wisler
    ,
    R. C. Bauer
    ,
    T. H. Okiishi
    DOI: 10.1115/1.3262127
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
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      Secondary Flow, Turbulent Diffusion, and Mixing in Axial-Flow Compressors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103185
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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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