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    Heat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003::page 339
    Author:
    W. D. Morris
    ,
    G. Ghavami-Nasr
    DOI: 10.1115/1.2927881
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of rotation on local heat transfer in a rectangular-sectioned duct has been experimentally studied for the case where the duct rotates about an axis orthogonal to its own central axis. The coolant used was air with the flow direction in the radially outward direction. This rotating flow geometry is encountered in the internal cooling of gas turbine rotor blades. Local Nusselt number variations along the duct have been determined over the trailing and leading surfaces. In general terms Coriolis-induced secondary flows are shown to enhance local heat transfer over the trailing surface compared to a stationary duct forced convection situation. The converse is true on the leading surface where significant impediment to local heat transfer can occur. Centripetal buoyancy is shown to influence the heat transfer response with heat transfer being improved on both leading and trailing surfaces as the wall-to-coolant temperature difference is increased with other controlling parameters held constant. Correlating equations are proposed and the results compared with those of other workers in the field.
    keyword(s): Rotation , Channels (Hydraulic engineering) , Measurement , Heat transfer , Ducts , Flow (Dynamics) , Coolants , Forced convection , Gas turbines , Rotors , Blades , Buoyancy , Temperature , Equations , Geometry AND Cooling ,
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      Heat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109372
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    • Journal of Turbomachinery

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    contributor authorW. D. Morris
    contributor authorG. Ghavami-Nasr
    date accessioned2017-05-08T23:36:55Z
    date available2017-05-08T23:36:55Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28613#339_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109372
    description abstractThe influence of rotation on local heat transfer in a rectangular-sectioned duct has been experimentally studied for the case where the duct rotates about an axis orthogonal to its own central axis. The coolant used was air with the flow direction in the radially outward direction. This rotating flow geometry is encountered in the internal cooling of gas turbine rotor blades. Local Nusselt number variations along the duct have been determined over the trailing and leading surfaces. In general terms Coriolis-induced secondary flows are shown to enhance local heat transfer over the trailing surface compared to a stationary duct forced convection situation. The converse is true on the leading surface where significant impediment to local heat transfer can occur. Centripetal buoyancy is shown to influence the heat transfer response with heat transfer being improved on both leading and trailing surfaces as the wall-to-coolant temperature difference is increased with other controlling parameters held constant. Correlating equations are proposed and the results compared with those of other workers in the field.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Measurements in Rectangular Channels With Orthogonal Mode Rotation
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927881
    journal fristpage339
    journal lastpage345
    identifier eissn1528-8900
    keywordsRotation
    keywordsChannels (Hydraulic engineering)
    keywordsMeasurement
    keywordsHeat transfer
    keywordsDucts
    keywordsFlow (Dynamics)
    keywordsCoolants
    keywordsForced convection
    keywordsGas turbines
    keywordsRotors
    keywordsBlades
    keywordsBuoyancy
    keywordsTemperature
    keywordsEquations
    keywordsGeometry AND Cooling
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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