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    Investigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 010::page 0101010-1
    Author:
    Liu, Qiang
    ,
    Zhong, Shan
    ,
    Li, Lin
    DOI: 10.1115/1.4046960
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the effects of an array of herringbone riblets with different riblet geometry (height and spacing) and start locations on the pressure losses in a cascade of diffuser blades are investigated over a range of low Reynolds numbers (0.50 × 105–1.00 × 105). The herringbone riblets with a given geometry are found to produce a profound modification to the wake structure above certain critical Reynolds numbers. It is also found that within the range of parameters tested an increase in riblet height and riblet spacing results in an onset of significant control effect at a lower Reynolds number, which is accompanied by a slight reduction in zone-averaged loss coefficient and flow turning angle. An upstream shift of the start position of the riblet array along the blades enables the riblets to become effective at a lower Reynolds number at the expense of a reduced loss reduction and flow turning angle. A semi-empirical relationship between the ratio of riblet height to local baseline boundary layer displacement thickness and the critical Reynolds number is established using the present experimental data. A preliminary methodology for designing the herringbone riblets to ensure an effective control of 2D flow separations around the mid-span of diffuser blades over a specified range of Reynolds numbers is also proposed.
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      Investigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4275401
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    contributor authorLiu, Qiang
    contributor authorZhong, Shan
    contributor authorLi, Lin
    date accessioned2022-02-04T22:21:20Z
    date available2022-02-04T22:21:20Z
    date copyright9/16/2020 12:00:00 AM
    date issued2020
    identifier issn0889-504X
    identifier otherturbo_142_10_101010.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4275401
    description abstractIn this paper, the effects of an array of herringbone riblets with different riblet geometry (height and spacing) and start locations on the pressure losses in a cascade of diffuser blades are investigated over a range of low Reynolds numbers (0.50 × 105–1.00 × 105). The herringbone riblets with a given geometry are found to produce a profound modification to the wake structure above certain critical Reynolds numbers. It is also found that within the range of parameters tested an increase in riblet height and riblet spacing results in an onset of significant control effect at a lower Reynolds number, which is accompanied by a slight reduction in zone-averaged loss coefficient and flow turning angle. An upstream shift of the start position of the riblet array along the blades enables the riblets to become effective at a lower Reynolds number at the expense of a reduced loss reduction and flow turning angle. A semi-empirical relationship between the ratio of riblet height to local baseline boundary layer displacement thickness and the critical Reynolds number is established using the present experimental data. A preliminary methodology for designing the herringbone riblets to ensure an effective control of 2D flow separations around the mid-span of diffuser blades over a specified range of Reynolds numbers is also proposed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers
    typeJournal Paper
    journal volume142
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4046960
    journal fristpage0101010-1
    journal lastpage0101010-14
    page14
    treeJournal of Turbomachinery:;2020:;volume( 142 ):;issue: 010
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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