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    Coupled Lagrangian Monte Carlo PDF–CFD Computation of Gas Turbine Combustor Flowfields With Finite-Rate Chemistry

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003::page 519
    Author:
    A. K. Tolpadi
    ,
    D. L. Burrus
    ,
    I. Z. Hu
    ,
    S. M. Correa
    DOI: 10.1115/1.2817015
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A coupled Lagrangian Monte Carlo Probability Density Function (PDF)-Eulerian Computational Fluid Dynamics (CFD) technique is presented for calculating steady three-dimensional turbulent reacting flow in a gas turbine combustor. PDF transport methods model turbulence-combustion interactions more accurately than conventional turbulence models with an assumed shape PDF. The PDF transport equation was solved using a Lagrangian particle tracking Monte Carlo (MC) method. The PDF modeled was over composition only. This MC module has been coupled with CONCERT, which is a fully elliptic three-dimensional body-fitted CFD code based on pressure correction techniques. In an earlier paper (Tolpadi et al., 1995), this computational approach was described, but only fast chemistry calculations were presented in a typical aircraft engine combustor. In the present paper, reduced chemistry schemes were incorporated into the MC module that enabled the modeling of finite rate effects in gas turbine flames and therefore the prediction of CO and NOx emissions. With the inclusion of these finite rate effects, the gas temperatures obtained were also more realistic. Initially, a two scalar scheme was implemented that allowed validation against Raman data taken in a recirculating bluff body stabilized CO/H2 /N2 -air flame. Good agreement of the temperature and major species were obtained. Next, finite rate computations were performed in a single annular aircraft engine combustor by incorporating a simple three scalar reduced chemistry scheme for Jet A fuel. This three scalar scheme was an extension of the two scalar scheme for CO/H2 /N2 fuel. The solutions obtained using the present approach were compared with those obtained using the fast chemistry PDF transport approach (Tolpadi et al., 1995) as well as the presumed shape PDF method. The calculated exhaust gas temperature using the finite rate model showed the best agreement with measurements made by a thermocouple rake. In addition, the CO and NOx emission indices were also computed and compared with corresponding data.
    keyword(s): Combustion chambers , Computational fluid dynamics , Gas turbines , Chemistry , Computation , Scalars , Temperature , Turbulence , Fuels , Flames , Shapes , Aircraft engines , Emissions , Thermocouples , Probability , Combustion , Measurement , Particulate matter , Density , Pressure , Flow (Dynamics) , Equations , Exhaust systems AND Modeling ,
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      Coupled Lagrangian Monte Carlo PDF–CFD Computation of Gas Turbine Combustor Flowfields With Finite-Rate Chemistry

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/118643
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. K. Tolpadi
    contributor authorD. L. Burrus
    contributor authorI. Z. Hu
    contributor authorS. M. Correa
    date accessioned2017-05-08T23:53:22Z
    date available2017-05-08T23:53:22Z
    date copyrightJuly, 1997
    date issued1997
    identifier issn1528-8919
    identifier otherJETPEZ-26766#519_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118643
    description abstractA coupled Lagrangian Monte Carlo Probability Density Function (PDF)-Eulerian Computational Fluid Dynamics (CFD) technique is presented for calculating steady three-dimensional turbulent reacting flow in a gas turbine combustor. PDF transport methods model turbulence-combustion interactions more accurately than conventional turbulence models with an assumed shape PDF. The PDF transport equation was solved using a Lagrangian particle tracking Monte Carlo (MC) method. The PDF modeled was over composition only. This MC module has been coupled with CONCERT, which is a fully elliptic three-dimensional body-fitted CFD code based on pressure correction techniques. In an earlier paper (Tolpadi et al., 1995), this computational approach was described, but only fast chemistry calculations were presented in a typical aircraft engine combustor. In the present paper, reduced chemistry schemes were incorporated into the MC module that enabled the modeling of finite rate effects in gas turbine flames and therefore the prediction of CO and NOx emissions. With the inclusion of these finite rate effects, the gas temperatures obtained were also more realistic. Initially, a two scalar scheme was implemented that allowed validation against Raman data taken in a recirculating bluff body stabilized CO/H2 /N2 -air flame. Good agreement of the temperature and major species were obtained. Next, finite rate computations were performed in a single annular aircraft engine combustor by incorporating a simple three scalar reduced chemistry scheme for Jet A fuel. This three scalar scheme was an extension of the two scalar scheme for CO/H2 /N2 fuel. The solutions obtained using the present approach were compared with those obtained using the fast chemistry PDF transport approach (Tolpadi et al., 1995) as well as the presumed shape PDF method. The calculated exhaust gas temperature using the finite rate model showed the best agreement with measurements made by a thermocouple rake. In addition, the CO and NOx emission indices were also computed and compared with corresponding data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCoupled Lagrangian Monte Carlo PDF–CFD Computation of Gas Turbine Combustor Flowfields With Finite-Rate Chemistry
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2817015
    journal fristpage519
    journal lastpage526
    identifier eissn0742-4795
    keywordsCombustion chambers
    keywordsComputational fluid dynamics
    keywordsGas turbines
    keywordsChemistry
    keywordsComputation
    keywordsScalars
    keywordsTemperature
    keywordsTurbulence
    keywordsFuels
    keywordsFlames
    keywordsShapes
    keywordsAircraft engines
    keywordsEmissions
    keywordsThermocouples
    keywordsProbability
    keywordsCombustion
    keywordsMeasurement
    keywordsParticulate matter
    keywordsDensity
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsEquations
    keywordsExhaust systems AND Modeling
    treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 003
    contenttypeFulltext
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