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    Numerical Simulation of Liquid Jet Atomization Including Turbulence Effects

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004::page 920
    Author:
    Huu P. Trinh
    ,
    C. P. Chen
    ,
    M. S. Balasubramanyam
    DOI: 10.1115/1.2747253
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes numerical implementation and validation of a newly developed hybrid model, T-blob/T-TAB, into an existing computational fluid dynamics (CFD) program for primary and secondary breakup simulation of liquid jet atomization. This model extends two widely used models, the Kelvin-Helmholtz (KH) instability of Reitz (the “blob” model) (1987, Atomization Spray Technol., 3, pp. 309–337) and the Taylor-Analogy-Breakup (TAB) secondary droplet breakup of and (1987, SAE Technical Paper No. 872089) to include liquid turbulence effects. In the primary breakup model, the level of the turbulence effect on the liquid breakup depends on the characteristic scales and flow conditions at the liquid nozzle exit. Transition to the secondary breakup was modeled based on energy balance, and an additional turbulence force acted on parent drops was modeled and integrated into the TAB governing equation. Several assessment studies are presented, and the results indicate that the existing KH and TAB models tend to underpredict the product drop size and spray angle, whereas the current model provides superior results when compared to the measured data.
    keyword(s): Turbulence , Computer simulation , Drops , Computational fluid dynamics , Sprays , Nozzles , Flow (Dynamics) , Equations AND Simulation ,
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      Numerical Simulation of Liquid Jet Atomization Including Turbulence Effects

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135657
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorHuu P. Trinh
    contributor authorC. P. Chen
    contributor authorM. S. Balasubramanyam
    date accessioned2017-05-09T00:23:34Z
    date available2017-05-09T00:23:34Z
    date copyrightOctober, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26973#920_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135657
    description abstractThis paper describes numerical implementation and validation of a newly developed hybrid model, T-blob/T-TAB, into an existing computational fluid dynamics (CFD) program for primary and secondary breakup simulation of liquid jet atomization. This model extends two widely used models, the Kelvin-Helmholtz (KH) instability of Reitz (the “blob” model) (1987, Atomization Spray Technol., 3, pp. 309–337) and the Taylor-Analogy-Breakup (TAB) secondary droplet breakup of and (1987, SAE Technical Paper No. 872089) to include liquid turbulence effects. In the primary breakup model, the level of the turbulence effect on the liquid breakup depends on the characteristic scales and flow conditions at the liquid nozzle exit. Transition to the secondary breakup was modeled based on energy balance, and an additional turbulence force acted on parent drops was modeled and integrated into the TAB governing equation. Several assessment studies are presented, and the results indicate that the existing KH and TAB models tend to underpredict the product drop size and spray angle, whereas the current model provides superior results when compared to the measured data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Simulation of Liquid Jet Atomization Including Turbulence Effects
    typeJournal Paper
    journal volume129
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2747253
    journal fristpage920
    journal lastpage928
    identifier eissn0742-4795
    keywordsTurbulence
    keywordsComputer simulation
    keywordsDrops
    keywordsComputational fluid dynamics
    keywordsSprays
    keywordsNozzles
    keywordsFlow (Dynamics)
    keywordsEquations AND Simulation
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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