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    Large-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries

    Source: Journal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003::page 374
    Author:
    K. Mahesh
    ,
    G. Constantinescu
    ,
    S. Apte
    ,
    G. Iaccarino
    ,
    F. Ham
    ,
    P. Moin
    DOI: 10.1115/1.2179098
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large-eddy simulation (LES) has traditionally been restricted to fairly simple geometries. This paper discusses LES of reacting flows in geometries as complex as commercial gas turbine engine combustors. The incompressible algorithm developed by (J. Comput. Phys., 2004, 197, 215–240) is extended to the zero Mach number equations with heat release. Chemical reactions are modeled using the flamelet/progress variable approach of and (J. Fluid Mech., 2004, 504, 73–97). The simulations are validated against experiment for methane-air combustion in a coaxial geometry, and jet-A surrogate/air combustion in a gas-turbine combustor geometry.
    keyword(s): Density , Flow (Dynamics) , Turbulence , Combustion chambers , Equations , Geometry , Gas turbines , Eddies (Fluid dynamics) , Simulation AND Algorithms ,
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      Large-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries

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    http://yetl.yabesh.ir/yetl1/handle/yetl/133042
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    contributor authorK. Mahesh
    contributor authorG. Constantinescu
    contributor authorS. Apte
    contributor authorG. Iaccarino
    contributor authorF. Ham
    contributor authorP. Moin
    date accessioned2017-05-09T00:18:38Z
    date available2017-05-09T00:18:38Z
    date copyrightMay, 2006
    date issued2006
    identifier issn0021-8936
    identifier otherJAMCAV-26599#374_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133042
    description abstractLarge-eddy simulation (LES) has traditionally been restricted to fairly simple geometries. This paper discusses LES of reacting flows in geometries as complex as commercial gas turbine engine combustors. The incompressible algorithm developed by (J. Comput. Phys., 2004, 197, 215–240) is extended to the zero Mach number equations with heat release. Chemical reactions are modeled using the flamelet/progress variable approach of and (J. Fluid Mech., 2004, 504, 73–97). The simulations are validated against experiment for methane-air combustion in a coaxial geometry, and jet-A surrogate/air combustion in a gas-turbine combustor geometry.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLarge-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries
    typeJournal Paper
    journal volume73
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2179098
    journal fristpage374
    journal lastpage381
    identifier eissn1528-9036
    keywordsDensity
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsCombustion chambers
    keywordsEquations
    keywordsGeometry
    keywordsGas turbines
    keywordsEddies (Fluid dynamics)
    keywordsSimulation AND Algorithms
    treeJournal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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