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    Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004::page 41011-1
    Author:
    Ananth, S. M.
    ,
    Nardini, Massimiliano
    ,
    Kozul, Melissa
    ,
    Vadlamani, Nagabhushana Rao
    ,
    Sandberg, Richard D.
    DOI: 10.1115/1.4066815
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent research has demonstrated the effectiveness of riblets (streamwise aligned grooves) in reducing the profile loss of low-pressure turbine (LPT) blades under high-lift (HL) loading. In this research, we pursue the efficacy of riblets in reducing the blade profile loss under various design and off-design conditions. We adopt a strategy in which surface roughness is employed in the transitional regime to minimize the separation bubble-related losses and flush-mounted riblets downstream to further mitigate the skin-friction drag and boundary layer losses due to an increase in the turbulent wetted area. Several high-fidelity scale-resolving simulations are carried out to test the efficacy of this ‘rough-ribbed’ LPT blade for loadings ranging from low-lift (LL), HL, and ultra high-lift (UHL) conditions. Furthermore, two exit Reynolds numbers—83,000 and 166,000—pertaining to engine relevant design and off-design conditions, respectively, are considered. The streamwise evolution of skin-friction coefficient and boundary layer integral parameters are compared and contrasted among different test cases. The instantaneous flow features and second-order statistics such as the Reynolds stress and turbulent kinetic energy are analyzed to determine the design and off-design performance of riblets. It is found that the efficacy of scallop-shaped riblets in reducing the profile loss improves with loading. Specifically, the net skin-friction reduction increases from 3.4% under LL to 8% under UHL loading at cruise Re. There is a corresponding reduction in the trailing edge momentum thickness (θTE) from 10% to 15%. A further reduction in θTE is attained from design to off-design Re under UHL loading. Thus, the effect of riblets in reducing mixing losses improves with increasing Re. It is also found that the riblets reduce flow blockage due to boundary layers. Furthermore, the necessity to optimize riblet ramp to achieve skin-friction reduction under off-design conditions is highlighted.
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      Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions

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    contributor authorAnanth, S. M.
    contributor authorNardini, Massimiliano
    contributor authorKozul, Melissa
    contributor authorVadlamani, Nagabhushana Rao
    contributor authorSandberg, Richard D.
    date accessioned2025-08-20T09:26:39Z
    date available2025-08-20T09:26:39Z
    date copyright10/25/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_147_4_041011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4308288
    description abstractRecent research has demonstrated the effectiveness of riblets (streamwise aligned grooves) in reducing the profile loss of low-pressure turbine (LPT) blades under high-lift (HL) loading. In this research, we pursue the efficacy of riblets in reducing the blade profile loss under various design and off-design conditions. We adopt a strategy in which surface roughness is employed in the transitional regime to minimize the separation bubble-related losses and flush-mounted riblets downstream to further mitigate the skin-friction drag and boundary layer losses due to an increase in the turbulent wetted area. Several high-fidelity scale-resolving simulations are carried out to test the efficacy of this ‘rough-ribbed’ LPT blade for loadings ranging from low-lift (LL), HL, and ultra high-lift (UHL) conditions. Furthermore, two exit Reynolds numbers—83,000 and 166,000—pertaining to engine relevant design and off-design conditions, respectively, are considered. The streamwise evolution of skin-friction coefficient and boundary layer integral parameters are compared and contrasted among different test cases. The instantaneous flow features and second-order statistics such as the Reynolds stress and turbulent kinetic energy are analyzed to determine the design and off-design performance of riblets. It is found that the efficacy of scallop-shaped riblets in reducing the profile loss improves with loading. Specifically, the net skin-friction reduction increases from 3.4% under LL to 8% under UHL loading at cruise Re. There is a corresponding reduction in the trailing edge momentum thickness (θTE) from 10% to 15%. A further reduction in θTE is attained from design to off-design Re under UHL loading. Thus, the effect of riblets in reducing mixing losses improves with increasing Re. It is also found that the riblets reduce flow blockage due to boundary layers. Furthermore, the necessity to optimize riblet ramp to achieve skin-friction reduction under off-design conditions is highlighted.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions
    typeJournal Paper
    journal volume147
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4066815
    journal fristpage41011-1
    journal lastpage41011-14
    page14
    treeJournal of Turbomachinery:;2024:;volume( 147 ):;issue: 004
    contenttypeFulltext
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