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    On the Response of a Strongly Diffusing Flow to Propagating Wakes

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002::page 21006
    Author:
    J. P. Gostelow
    ,
    R. L. Thomas
    ,
    D. S. Adebayo
    DOI: 10.1115/1.2950054
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Further evidence on the similarities between transition and separation phenomena occurring in turbomachinery and wind tunnel flows is provided by measurements on a large scale flat plate under a strong adverse pressure gradient. The flat plate has a long laminar separation bubble and is subjected to a range of disturbances with triggering caused by injection of a transverse jet and subsequently by wakes generated by rods moving transversely upstream of the leading edge. Wakes were originally presented individually. Each individual wake provoked a vigorous turbulent patch, resulting in the instantaneous collapse of the separation bubble. This was followed by a very strong, and stable, calmed region. Following the lead given by the experiments of and (1987, “ On the Structure of Turbulent Spot in a Heated Laminar Boundary Layer,” Exp. Fluids, 5, pp. 207–229.) on triggered turbulent spots, wakes were then presented in pairs at different wake spacing intervals. In this way wake interaction effects could be investigated in more detail. As in the work on triggered turbulent spots the spacing between impinging wakes was systematically varied; it was found that for close wake spacings the calmed region acted to suppress the turbulence in the following turbulent patch. To investigate whether this phenomenon was a recurring one or whether the flow then reverted back to its unperturbed state, the experiments were repeated with three and four rods instead of two. This has the potential for making available a wide range of variables including direction and speed of rod rotation. It was found that the subsequent wakes were also suppressed by the calming effect. It may be anticipated that this repeating situation is present in a turbomachine, resulting in hidden benefits for blade count and efficiency. There may also conceivably be blade loading advantages while retaining favorable heat transfer conditions in high pressure turbines or stall margin in axial compressors. The inherent and prospective benefits of the calming effect therefore need to be understood thoroughly and new opportunities exploited where this is feasible.a
    keyword(s): Turbulence , Wakes AND Flow (Dynamics) ,
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      On the Response of a Strongly Diffusing Flow to Propagating Wakes

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    contributor authorJ. P. Gostelow
    contributor authorR. L. Thomas
    contributor authorD. S. Adebayo
    date accessioned2017-05-09T00:35:50Z
    date available2017-05-09T00:35:50Z
    date copyrightApril, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28754#021006_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142182
    description abstractFurther evidence on the similarities between transition and separation phenomena occurring in turbomachinery and wind tunnel flows is provided by measurements on a large scale flat plate under a strong adverse pressure gradient. The flat plate has a long laminar separation bubble and is subjected to a range of disturbances with triggering caused by injection of a transverse jet and subsequently by wakes generated by rods moving transversely upstream of the leading edge. Wakes were originally presented individually. Each individual wake provoked a vigorous turbulent patch, resulting in the instantaneous collapse of the separation bubble. This was followed by a very strong, and stable, calmed region. Following the lead given by the experiments of and (1987, “ On the Structure of Turbulent Spot in a Heated Laminar Boundary Layer,” Exp. Fluids, 5, pp. 207–229.) on triggered turbulent spots, wakes were then presented in pairs at different wake spacing intervals. In this way wake interaction effects could be investigated in more detail. As in the work on triggered turbulent spots the spacing between impinging wakes was systematically varied; it was found that for close wake spacings the calmed region acted to suppress the turbulence in the following turbulent patch. To investigate whether this phenomenon was a recurring one or whether the flow then reverted back to its unperturbed state, the experiments were repeated with three and four rods instead of two. This has the potential for making available a wide range of variables including direction and speed of rod rotation. It was found that the subsequent wakes were also suppressed by the calming effect. It may be anticipated that this repeating situation is present in a turbomachine, resulting in hidden benefits for blade count and efficiency. There may also conceivably be blade loading advantages while retaining favorable heat transfer conditions in high pressure turbines or stall margin in axial compressors. The inherent and prospective benefits of the calming effect therefore need to be understood thoroughly and new opportunities exploited where this is feasible.a
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Response of a Strongly Diffusing Flow to Propagating Wakes
    typeJournal Paper
    journal volume131
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2950054
    journal fristpage21006
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsWakes AND Flow (Dynamics)
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 002
    contenttypeFulltext
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