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    Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layers on Convex-Curved Surfaces

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003::page 443
    Author:
    T. Wang
    ,
    T. W. Simon
    DOI: 10.1115/1.3262125
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of the effects of convex curvature and free-stream turbulence on momentum and heat transfer in a boundary layer undergoing natural transition was performed. The test section was designed for providing a two-dimensional boundary layer flow on a uniformly heated curved surface. The unique feature of the test wall was its flexibility to be bent to various radii of curvature R . Three cases of R = ∞, 180 cm, and 90 cm, are presented, each with two free-stream turbulence intensity levels, 0.68 and 2 percent. Mean velocity and temperature profiles and local Stanton number data were taken in a heated flow and streamwise Reynolds normal stress profiles were taken in an isothermal flow. Mild convex curvature (R = 180 cm) is shown to delay transition. Bending the test wall to a smaller radius of curvature, 90 cm, results in no significant further delay of transition. Cases with both curvature and higher free-stream disturbance effects show a pronounced dominance of the latter. Heat transfer rates and mean temperature profiles are shown to change more slowly after transition than wall shear stress values and velocity profiles. This can be observed as higher values of turbulent Prandtl number and lower values of the Reynolds-analogy factor, 2St/C f , in the transitional and early-turbulent flows than values known to apply for mature turbulent flows. The results of this study increase the data base for development of transition prediction models which can be used in gas turbine blade design.
    keyword(s): Heat transfer , Measurement , Boundary layers , Fluid mechanics , Turbulence , Flow (Dynamics) , Delays , Temperature profiles , Stress , Shear (Mechanics) , Design , Gas turbines , Blades , Databases , Momentum , Prandtl number AND Plasticity ,
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      Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layers on Convex-Curved Surfaces

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103225
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    contributor authorT. Wang
    contributor authorT. W. Simon
    date accessioned2017-05-08T23:26:02Z
    date available2017-05-08T23:26:02Z
    date copyrightJuly, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28585#443_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103225
    description abstractAn experimental investigation of the effects of convex curvature and free-stream turbulence on momentum and heat transfer in a boundary layer undergoing natural transition was performed. The test section was designed for providing a two-dimensional boundary layer flow on a uniformly heated curved surface. The unique feature of the test wall was its flexibility to be bent to various radii of curvature R . Three cases of R = ∞, 180 cm, and 90 cm, are presented, each with two free-stream turbulence intensity levels, 0.68 and 2 percent. Mean velocity and temperature profiles and local Stanton number data were taken in a heated flow and streamwise Reynolds normal stress profiles were taken in an isothermal flow. Mild convex curvature (R = 180 cm) is shown to delay transition. Bending the test wall to a smaller radius of curvature, 90 cm, results in no significant further delay of transition. Cases with both curvature and higher free-stream disturbance effects show a pronounced dominance of the latter. Heat transfer rates and mean temperature profiles are shown to change more slowly after transition than wall shear stress values and velocity profiles. This can be observed as higher values of turbulent Prandtl number and lower values of the Reynolds-analogy factor, 2St/C f , in the transitional and early-turbulent flows than values known to apply for mature turbulent flows. The results of this study increase the data base for development of transition prediction models which can be used in gas turbine blade design.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layers on Convex-Curved Surfaces
    typeJournal Paper
    journal volume109
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262125
    journal fristpage443
    journal lastpage452
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsMeasurement
    keywordsBoundary layers
    keywordsFluid mechanics
    keywordsTurbulence
    keywordsFlow (Dynamics)
    keywordsDelays
    keywordsTemperature profiles
    keywordsStress
    keywordsShear (Mechanics)
    keywordsDesign
    keywordsGas turbines
    keywordsBlades
    keywordsDatabases
    keywordsMomentum
    keywordsPrandtl number AND Plasticity
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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