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    Thermal Damping in Cavitating Nozzle Flows

    Source: Journal of Fluids Engineering:;2002:;volume( 124 ):;issue: 004::page 969
    Author:
    Can F. Delale
    DOI: 10.1115/1.1511163
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent investigations of bubbly cavitating nozzle flows using the polytropic law for the partial gas pressure have shown flow instabilities that lead to flashing flow solutions. Here, we investigate the stabilizing effect of thermal damping on these instabilities. For this reason we consider the energy equation within the bubble, assumed to be composed of vapor and gas, in the uniform pressure approximation with low vapor concentration. The partial vapor pressure is fixed by the vapor saturation pressure corresponding to the interface temperature, which is evaluated by assuming the thin boundary layer approximation within the liquid. Consequently, the partial gas pressure is evaluated by its relation to the heat flux through the interface in the uniform pressure approximation. The model is then coupled to the steady-state cavitating nozzle flow equations replacing the polytropic law for the partial gas pressure. The instabilities found in steady cavitating nozzle flows are seen to be stabilized by thermal damping with or without the occurrence of bubbly shock waves.
    keyword(s): Pressure , Flow (Dynamics) , Vapors , Bubbles , Nozzles , Approximation , Equations , Damping , Temperature , Steady state , Flashing AND Flow instability ,
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      Thermal Damping in Cavitating Nozzle Flows

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    contributor authorCan F. Delale
    date accessioned2017-05-09T00:07:39Z
    date available2017-05-09T00:07:39Z
    date copyrightDecember, 2002
    date issued2002
    identifier issn0098-2202
    identifier otherJFEGA4-27179#969_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126902
    description abstractRecent investigations of bubbly cavitating nozzle flows using the polytropic law for the partial gas pressure have shown flow instabilities that lead to flashing flow solutions. Here, we investigate the stabilizing effect of thermal damping on these instabilities. For this reason we consider the energy equation within the bubble, assumed to be composed of vapor and gas, in the uniform pressure approximation with low vapor concentration. The partial vapor pressure is fixed by the vapor saturation pressure corresponding to the interface temperature, which is evaluated by assuming the thin boundary layer approximation within the liquid. Consequently, the partial gas pressure is evaluated by its relation to the heat flux through the interface in the uniform pressure approximation. The model is then coupled to the steady-state cavitating nozzle flow equations replacing the polytropic law for the partial gas pressure. The instabilities found in steady cavitating nozzle flows are seen to be stabilized by thermal damping with or without the occurrence of bubbly shock waves.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermal Damping in Cavitating Nozzle Flows
    typeJournal Paper
    journal volume124
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.1511163
    journal fristpage969
    journal lastpage976
    identifier eissn1528-901X
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsVapors
    keywordsBubbles
    keywordsNozzles
    keywordsApproximation
    keywordsEquations
    keywordsDamping
    keywordsTemperature
    keywordsSteady state
    keywordsFlashing AND Flow instability
    treeJournal of Fluids Engineering:;2002:;volume( 124 ):;issue: 004
    contenttypeFulltext
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