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    Measurement of Flow Phenomena in a Lower Plenum Model of a Prismatic Gas-Cooled Reactor

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 002::page 22901
    Author:
    Hugh M. McIlroy
    ,
    Donald M. McEligot
    ,
    Robert J. Pink
    DOI: 10.1115/1.3078784
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Mean-velocity-field and turbulence data are presented that measure turbulent flow phenomena in an approximately 1:7 scale model of a region of the lower plenum of a typical prismatic gas-cooled reactor similar to a General Atomics gas-turbine-modular helium reactor design. The data were obtained in the Matched-Index-of-Refraction (MIR) Facility at Idaho National Laboratory (INL) and are offered for assessing computational fluid dynamics software. This experiment has been selected as the first standard problem endorsed by the Generation IV International Forum. Results concentrate on the region of the lower plenum near its far reflector wall (away from the outlet duct). The flow in the lower plenum consists of multiple jets injected into a confined cross flow—with obstructions. The model consists of a row of full circular posts along its centerline with half-posts on the two parallel walls to approximate geometry scaled to that expected from the staggered parallel rows of posts in the reactor design. The model is fabricated from clear, fused quartz to match the refractive-index of the working fluid so that optical techniques may be employed for the measurements. The benefit of the MIR technique is that it permits optical measurements to determine flow characteristics in complex passages in and around objects to be obtained without locating intrusive transducers that will disturb the flow field and without distortion of the optical paths. An advantage of the INL system is its large size, leading to improved spatial and temporal resolutions compared with similar facilities at smaller scales. A three-dimensional particle image velocimetry system was used to collect the data. Inlet-jet Reynolds numbers (based on the jet diameter and the time-mean bulk velocity) are approximately 4300 and 12,400. Uncertainty analyses and a discussion of the standard problem are included. The measurements reveal developing, nonuniform, turbulent flow in the inlet jets and complicated flow patterns in the model lower plenum. Data include three-dimensional vector plots, data displays along the coordinate planes (slices), and presentations that describe the component flows at specific regions in the model. Information on inlet conditions is also presented.
    keyword(s): Flow (Dynamics) , Gas cooled reactors , Jets , Computational fluid dynamics , Uncertainty , Turbulence , Design , Fluids , Refractive index , Very high temperature reactors AND Computer software ,
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      Measurement of Flow Phenomena in a Lower Plenum Model of a Prismatic Gas-Cooled Reactor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/143286
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorHugh M. McIlroy
    contributor authorDonald M. McEligot
    contributor authorRobert J. Pink
    date accessioned2017-05-09T00:37:53Z
    date available2017-05-09T00:37:53Z
    date copyrightFebruary, 2010
    date issued2010
    identifier issn1528-8919
    identifier otherJETPEZ-27094#022901_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143286
    description abstractMean-velocity-field and turbulence data are presented that measure turbulent flow phenomena in an approximately 1:7 scale model of a region of the lower plenum of a typical prismatic gas-cooled reactor similar to a General Atomics gas-turbine-modular helium reactor design. The data were obtained in the Matched-Index-of-Refraction (MIR) Facility at Idaho National Laboratory (INL) and are offered for assessing computational fluid dynamics software. This experiment has been selected as the first standard problem endorsed by the Generation IV International Forum. Results concentrate on the region of the lower plenum near its far reflector wall (away from the outlet duct). The flow in the lower plenum consists of multiple jets injected into a confined cross flow—with obstructions. The model consists of a row of full circular posts along its centerline with half-posts on the two parallel walls to approximate geometry scaled to that expected from the staggered parallel rows of posts in the reactor design. The model is fabricated from clear, fused quartz to match the refractive-index of the working fluid so that optical techniques may be employed for the measurements. The benefit of the MIR technique is that it permits optical measurements to determine flow characteristics in complex passages in and around objects to be obtained without locating intrusive transducers that will disturb the flow field and without distortion of the optical paths. An advantage of the INL system is its large size, leading to improved spatial and temporal resolutions compared with similar facilities at smaller scales. A three-dimensional particle image velocimetry system was used to collect the data. Inlet-jet Reynolds numbers (based on the jet diameter and the time-mean bulk velocity) are approximately 4300 and 12,400. Uncertainty analyses and a discussion of the standard problem are included. The measurements reveal developing, nonuniform, turbulent flow in the inlet jets and complicated flow patterns in the model lower plenum. Data include three-dimensional vector plots, data displays along the coordinate planes (slices), and presentations that describe the component flows at specific regions in the model. Information on inlet conditions is also presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of Flow Phenomena in a Lower Plenum Model of a Prismatic Gas-Cooled Reactor
    typeJournal Paper
    journal volume132
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3078784
    journal fristpage22901
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsGas cooled reactors
    keywordsJets
    keywordsComputational fluid dynamics
    keywordsUncertainty
    keywordsTurbulence
    keywordsDesign
    keywordsFluids
    keywordsRefractive index
    keywordsVery high temperature reactors AND Computer software
    treeJournal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 002
    contenttypeFulltext
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