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    Effect of High Free-Stream Turbulence With Large Length Scale on Blade Heat/Mass Transfer

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002::page 217
    Author:
    H. P. Wang
    ,
    R. J. Goldstein
    ,
    S. J. Olson
    DOI: 10.1115/1.2841304
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The naphthalene sublimation technique is used to investigate the influence of high free-stream turbulence with large length scale on the heat/mass transfer from a turbine blade in a highly accelerated linear cascade. The experiments are conducted at four exit Reynolds numbers, ranging from 2.4 × 105 to 7.8 × 105 , with free-stream turbulence of 3, 8.5, and 8 percent and corresponding integral length scales of 0.9 cm, 2.6 cm, and 8 cm, respectively. On the suction surface, the heat/mass transfer rate is significantly enhanced by high free-stream turbulence due to an early boundary layer transition. By contrast, the transition occurs very late, and may not occur at very low Reynolds numbers with low free-stream turbulence. In the turbulent boundary layer, lower heat/mass transfer rates are found for the highest free-stream turbulence level with large length scale than for the moderate turbulence levels with relatively small scales. Similar phenomena also occur at the leading edge. However, the effect of turbulence is not as pronounced in the laminar boundary layer.
    keyword(s): Heat , Mass transfer , Turbulence , Blades , Reynolds number , Boundary layers , Turbine blades , Cascades (Fluid dynamics) , Boundary layer turbulence AND Suction ,
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      Effect of High Free-Stream Turbulence With Large Length Scale on Blade Heat/Mass Transfer

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/123029
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    contributor authorH. P. Wang
    contributor authorR. J. Goldstein
    contributor authorS. J. Olson
    date accessioned2017-05-09T00:01:17Z
    date available2017-05-09T00:01:17Z
    date copyrightApril, 1999
    date issued1999
    identifier issn0889-504X
    identifier otherJOTUEI-28669#217_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123029
    description abstractThe naphthalene sublimation technique is used to investigate the influence of high free-stream turbulence with large length scale on the heat/mass transfer from a turbine blade in a highly accelerated linear cascade. The experiments are conducted at four exit Reynolds numbers, ranging from 2.4 × 105 to 7.8 × 105 , with free-stream turbulence of 3, 8.5, and 8 percent and corresponding integral length scales of 0.9 cm, 2.6 cm, and 8 cm, respectively. On the suction surface, the heat/mass transfer rate is significantly enhanced by high free-stream turbulence due to an early boundary layer transition. By contrast, the transition occurs very late, and may not occur at very low Reynolds numbers with low free-stream turbulence. In the turbulent boundary layer, lower heat/mass transfer rates are found for the highest free-stream turbulence level with large length scale than for the moderate turbulence levels with relatively small scales. Similar phenomena also occur at the leading edge. However, the effect of turbulence is not as pronounced in the laminar boundary layer.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of High Free-Stream Turbulence With Large Length Scale on Blade Heat/Mass Transfer
    typeJournal Paper
    journal volume121
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841304
    journal fristpage217
    journal lastpage224
    identifier eissn1528-8900
    keywordsHeat
    keywordsMass transfer
    keywordsTurbulence
    keywordsBlades
    keywordsReynolds number
    keywordsBoundary layers
    keywordsTurbine blades
    keywordsCascades (Fluid dynamics)
    keywordsBoundary layer turbulence AND Suction
    treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 002
    contenttypeFulltext
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