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    The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation

    Source: Journal of Turbomachinery:;2021:;volume( 144 ):;issue: 004::page 41001-1
    Author:
    Gramespacher, Christoph
    ,
    Stripf, Matthias
    ,
    Bauer, Hans-Jörg
    DOI: 10.1115/1.4052458
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer measurements in transitional flat plate boundary layers subjected to surface roughness, strong pressure gradients, and freestream turbulence are presented. The surfaces considered consist of a smooth reference and 26 deterministic surface topographies that vary in roughness element aspect ratio, height, and density. They are designed to cover the full range of roughness regimes from smooth over transitionally rough to fully rough. For each surface, two pressure distributions, characteristic for a suction and a pressure side turbine vane, are investigated. Inlet Reynolds numbers range from 3.0 × 105 to 6.0 × 105 and inlet turbulence intensity is varied between 1% and 8%. Furthermore, different turbulence Reynolds numbers, i.e., turbulence length scales, are realized while the incident turbulence intensity is kept constant. Additionally, the turbulence intensity and Reynolds stress distributions in the freestream along the flat plate are measured using x-wire probes. Results show a strong influence of roughness and turbulence intensity on the onset of transition. The new data set is used to develop an improved correlation considering the roughness height, density, and shape as well as the turbulence intensity and turbulent length scales.
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      The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4284494
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    contributor authorGramespacher, Christoph
    contributor authorStripf, Matthias
    contributor authorBauer, Hans-Jörg
    date accessioned2022-05-08T08:54:28Z
    date available2022-05-08T08:54:28Z
    date copyright11/2/2021 12:00:00 AM
    date issued2021
    identifier issn0889-504X
    identifier otherturbo_144_4_041001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284494
    description abstractHeat transfer measurements in transitional flat plate boundary layers subjected to surface roughness, strong pressure gradients, and freestream turbulence are presented. The surfaces considered consist of a smooth reference and 26 deterministic surface topographies that vary in roughness element aspect ratio, height, and density. They are designed to cover the full range of roughness regimes from smooth over transitionally rough to fully rough. For each surface, two pressure distributions, characteristic for a suction and a pressure side turbine vane, are investigated. Inlet Reynolds numbers range from 3.0 × 105 to 6.0 × 105 and inlet turbulence intensity is varied between 1% and 8%. Furthermore, different turbulence Reynolds numbers, i.e., turbulence length scales, are realized while the incident turbulence intensity is kept constant. Additionally, the turbulence intensity and Reynolds stress distributions in the freestream along the flat plate are measured using x-wire probes. Results show a strong influence of roughness and turbulence intensity on the onset of transition. The new data set is used to develop an improved correlation considering the roughness height, density, and shape as well as the turbulence intensity and turbulent length scales.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation
    typeJournal Paper
    journal volume144
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4052458
    journal fristpage41001-1
    journal lastpage41001-10
    page10
    treeJournal of Turbomachinery:;2021:;volume( 144 ):;issue: 004
    contenttypeFulltext
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