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    Liquid Particle Dynamics and Rate of Evaporation in the Rotating Field of Centrifugal Compressors

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001::page 80
    Author:
    O. Pinkus
    DOI: 10.1115/1.3227402
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A model is presented which consists of injecting a liquid coolant into the gas or superheated vapor of centrifugal compressors via slots in the rotating blades. The aim of the injection is minimization of required compression work. The three-dimensional analysis determines the relative velocities and trajectories of the liquid particles, and their rate of vaporization as a function of the prevailing flow field and inlet conditions. Inertia, viscous drag, centrifugal and Coriolis forces are all included. The analysis rests on the assumption of low volumetric liquid/gas ratios so that the aerodynamics of the flow is not appreciably disturbed. The computer-obtained results show that for optimum conditions, and to avoid collision with the blades, it is desirable that injection occur at the suction side of the blades and close to the hub, that low rather than high initial particle velocities are preferred, and that small droplet sizes are required both to avoid blade erosion and to assure the highest rate of vaporization.
    keyword(s): Compressors , Particle dynamics , Evaporation , Blades , Flow (Dynamics) , Particulate matter , Coriolis force , Suction , Aerodynamics , Vapors , Drag (Fluid dynamics) , Coolants , Collisions (Physics) , Compression , Superheating , Rotating blades , Computers , Erosion AND Inertia (Mechanics) ,
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      Liquid Particle Dynamics and Rate of Evaporation in the Rotating Field of Centrifugal Compressors

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    http://yetl.yabesh.ir/yetl1/handle/yetl/97128
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorO. Pinkus
    date accessioned2017-05-08T23:15:36Z
    date available2017-05-08T23:15:36Z
    date copyrightJanuary, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26779#80_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97128
    description abstractA model is presented which consists of injecting a liquid coolant into the gas or superheated vapor of centrifugal compressors via slots in the rotating blades. The aim of the injection is minimization of required compression work. The three-dimensional analysis determines the relative velocities and trajectories of the liquid particles, and their rate of vaporization as a function of the prevailing flow field and inlet conditions. Inertia, viscous drag, centrifugal and Coriolis forces are all included. The analysis rests on the assumption of low volumetric liquid/gas ratios so that the aerodynamics of the flow is not appreciably disturbed. The computer-obtained results show that for optimum conditions, and to avoid collision with the blades, it is desirable that injection occur at the suction side of the blades and close to the hub, that low rather than high initial particle velocities are preferred, and that small droplet sizes are required both to avoid blade erosion and to assure the highest rate of vaporization.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLiquid Particle Dynamics and Rate of Evaporation in the Rotating Field of Centrifugal Compressors
    typeJournal Paper
    journal volume105
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227402
    journal fristpage80
    journal lastpage87
    identifier eissn0742-4795
    keywordsCompressors
    keywordsParticle dynamics
    keywordsEvaporation
    keywordsBlades
    keywordsFlow (Dynamics)
    keywordsParticulate matter
    keywordsCoriolis force
    keywordsSuction
    keywordsAerodynamics
    keywordsVapors
    keywordsDrag (Fluid dynamics)
    keywordsCoolants
    keywordsCollisions (Physics)
    keywordsCompression
    keywordsSuperheating
    keywordsRotating blades
    keywordsComputers
    keywordsErosion AND Inertia (Mechanics)
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001
    contenttypeFulltext
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