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    Transient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001::page 52
    Author:
    D. E. Metzger
    ,
    R. S. Bunker
    ,
    G. Bosch
    DOI: 10.1115/1.2927737
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental technique has been developed for measurement of local convection heat transfer characteristics on rotating surfaces, utilizing thin liquid crystal surface coatings in a thermal transient test procedure. The encapsulated liquid crystal coatings used are sprayed directly on the test surface and their response is observed and processed during the transient with automated computer vision and data acquisition systems. Heat transfer coefficients are calculated from the thermal transient response of the test surface, as determined from the color indication from the thin coating. A significant advantage of the method, especially for convection in disk/shroud cavities that may contain recirculating fluid regions, is that appropriate thermal boundary conditions are naturally imposed on all of the boundary surfaces. The method is also relatively fast and inexpensive, and allows the geometry of the disk and stator surfaces to be changed easily, without the expenses of mounting discrete heat flux and temperature sensors and equipment to transfer information to a stationary frame of reference. Application of the experimental technique is demonstrated with detailed radially local surface Nusselt number distributions acquired for cases involving jet impingement onto a smooth disk, rotating in close proximity to a parallel plane stator disk. A single circular jet, with nozzle exit flush mounted in the stator, is oriented normal to the disk surface at various radii and flow rates. Local Nusselt numbers are presented nondimensionally as functions of both disk and flow Reynolds numbers. The results indicate that the local radial heat transfer distribution can be controlled by varying the impingement radius, but maximum radially averaged heat transfer is obtained with impingement at the disk center.
    keyword(s): Heat transfer , Liquid crystals , Rotating Disks , Disks , Stators , Convection , Flow (Dynamics) , Nozzles , Computers , Temperature sensors , Heat flux , Heat transfer coefficients , Data acquisition systems , Boundary-value problems , Cavities , Functions , Geometry , Fluids , Coating processes , Reynolds number , Structural frames AND Transients (Dynamics) ,
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      Transient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109444
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    • Journal of Turbomachinery

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    contributor authorD. E. Metzger
    contributor authorR. S. Bunker
    contributor authorG. Bosch
    date accessioned2017-05-08T23:37:02Z
    date available2017-05-08T23:37:02Z
    date copyrightJanuary, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28608#52_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109444
    description abstractAn experimental technique has been developed for measurement of local convection heat transfer characteristics on rotating surfaces, utilizing thin liquid crystal surface coatings in a thermal transient test procedure. The encapsulated liquid crystal coatings used are sprayed directly on the test surface and their response is observed and processed during the transient with automated computer vision and data acquisition systems. Heat transfer coefficients are calculated from the thermal transient response of the test surface, as determined from the color indication from the thin coating. A significant advantage of the method, especially for convection in disk/shroud cavities that may contain recirculating fluid regions, is that appropriate thermal boundary conditions are naturally imposed on all of the boundary surfaces. The method is also relatively fast and inexpensive, and allows the geometry of the disk and stator surfaces to be changed easily, without the expenses of mounting discrete heat flux and temperature sensors and equipment to transfer information to a stationary frame of reference. Application of the experimental technique is demonstrated with detailed radially local surface Nusselt number distributions acquired for cases involving jet impingement onto a smooth disk, rotating in close proximity to a parallel plane stator disk. A single circular jet, with nozzle exit flush mounted in the stator, is oriented normal to the disk surface at various radii and flow rates. Local Nusselt numbers are presented nondimensionally as functions of both disk and flow Reynolds numbers. The results indicate that the local radial heat transfer distribution can be controlled by varying the impingement radius, but maximum radially averaged heat transfer is obtained with impingement at the disk center.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTransient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement
    typeJournal Paper
    journal volume113
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927737
    journal fristpage52
    journal lastpage59
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsLiquid crystals
    keywordsRotating Disks
    keywordsDisks
    keywordsStators
    keywordsConvection
    keywordsFlow (Dynamics)
    keywordsNozzles
    keywordsComputers
    keywordsTemperature sensors
    keywordsHeat flux
    keywordsHeat transfer coefficients
    keywordsData acquisition systems
    keywordsBoundary-value problems
    keywordsCavities
    keywordsFunctions
    keywordsGeometry
    keywordsFluids
    keywordsCoating processes
    keywordsReynolds number
    keywordsStructural frames AND Transients (Dynamics)
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 001
    contenttypeFulltext
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