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    Passage Flow Structure and Its Influence on Endwall Heat Transfer in a 90 deg Turning Duct: Mean Flow and High Resolution Endwall Heat Transfer Experiments

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001::page 39
    Author:
    B. G. Wiedner
    ,
    C. Camci
    DOI: 10.1115/1.2841009
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Three-dimensional measurements of the mean velocity field have been made in a square-cross-sectional, strongly curved, 90 deg turbulent duct flow. The mean radius to duct width ratio was 2.3. The study was performed as part of an overall investigation of the physics of endwall convective heat transfer. All three components of the velocity vector and the static and total pressure fields were measured using a five-hole probe at four duct cross sections: inlet, 0, 45, and 90 deg. Preliminary turbulence measurements using a single sensor hot wire at the inlet cross section were also obtained to provide streamwise fluctuation levels through the boundary layer. The endwall heat transfer coefficient distribution was determined using a steady-state measurement technique and liquid crystal thermography. A high-resolution heat transfer map of the endwall surface from far upstream of the curve through the 90 deg cross section is presented. The three-dimensional velocity field measurements indicate that a highly symmetric, strong secondary flow develops in the duct with a significant transfer of streamwise momentum to the transverse directions. The cross-stream vorticity components within the measurement plane were estimated using the five-hole probe data and an inviscid from of the incompressible momentum equation. The development of the total and static pressure fields, the three-dimensional mean velocity field, and all three components of the vorticity field are discussed. The endwall heat transfer distribution is interpreted with respect to the measured mean flow quantities.
    keyword(s): Flow (Dynamics) , Heat transfer , Resolution (Optics) , Turning , Ducts , Measurement , Vorticity , Pressure , Momentum , Turbulence , Probes , Steady state , Heat transfer coefficients , Physics , Thermography , Wire , Cross section (Physics) , Liquid crystals , Boundary layers , Convection , Sensors AND Equations ,
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      Passage Flow Structure and Its Influence on Endwall Heat Transfer in a 90 deg Turning Duct: Mean Flow and High Resolution Endwall Heat Transfer Experiments

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119657
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    • Journal of Turbomachinery

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    contributor authorB. G. Wiedner
    contributor authorC. Camci
    date accessioned2017-05-08T23:55:13Z
    date available2017-05-08T23:55:13Z
    date copyrightJanuary, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28657#39_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119657
    description abstractThree-dimensional measurements of the mean velocity field have been made in a square-cross-sectional, strongly curved, 90 deg turbulent duct flow. The mean radius to duct width ratio was 2.3. The study was performed as part of an overall investigation of the physics of endwall convective heat transfer. All three components of the velocity vector and the static and total pressure fields were measured using a five-hole probe at four duct cross sections: inlet, 0, 45, and 90 deg. Preliminary turbulence measurements using a single sensor hot wire at the inlet cross section were also obtained to provide streamwise fluctuation levels through the boundary layer. The endwall heat transfer coefficient distribution was determined using a steady-state measurement technique and liquid crystal thermography. A high-resolution heat transfer map of the endwall surface from far upstream of the curve through the 90 deg cross section is presented. The three-dimensional velocity field measurements indicate that a highly symmetric, strong secondary flow develops in the duct with a significant transfer of streamwise momentum to the transverse directions. The cross-stream vorticity components within the measurement plane were estimated using the five-hole probe data and an inviscid from of the incompressible momentum equation. The development of the total and static pressure fields, the three-dimensional mean velocity field, and all three components of the vorticity field are discussed. The endwall heat transfer distribution is interpreted with respect to the measured mean flow quantities.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePassage Flow Structure and Its Influence on Endwall Heat Transfer in a 90 deg Turning Duct: Mean Flow and High Resolution Endwall Heat Transfer Experiments
    typeJournal Paper
    journal volume119
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841009
    journal fristpage39
    journal lastpage50
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsResolution (Optics)
    keywordsTurning
    keywordsDucts
    keywordsMeasurement
    keywordsVorticity
    keywordsPressure
    keywordsMomentum
    keywordsTurbulence
    keywordsProbes
    keywordsSteady state
    keywordsHeat transfer coefficients
    keywordsPhysics
    keywordsThermography
    keywordsWire
    keywordsCross section (Physics)
    keywordsLiquid crystals
    keywordsBoundary layers
    keywordsConvection
    keywordsSensors AND Equations
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 001
    contenttypeFulltext
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