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    Tuning of Generalized K-Omega Turbulence Model by Using Adjoint Optimization and Machine Learning for Gas Turbine Combustor Applications

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 008::page 81014-1
    Author:
    Klavaris, George
    ,
    Xu, Min
    ,
    Hill, Chris
    ,
    Menter, Florian
    ,
    Patwardhan, Saurabh
    ,
    Verma, Ishan
    DOI: 10.1115/1.4064367
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbulence modeling plays a crucial role in swirl-stabilized gas turbine combustors, typically relying on scale-resolved simulations (SRS) such as large eddy simulations (LES). However, LES is computationally expensive due to the need for fine mesh resolution and small time-steps required to capture the combustor's large-scale turbulence motion accurately. On the other hand, Reynolds-averaged Navier–Stokes (RANS) models while computationally efficient, lack fidelity in predicting complex flow characteristics such as swirl accurately. In this study, the GEKO model is used for simulating RANS predictions of turbulence in a swirling flow scenario, whereas high-fidelity LES predictions serve as target data enabling field inversion via gradient-based optimization using the Adjoint solver in ansysfluent. Machine learning via neural network (NN) Training is employed to establish correlations between turbulent flow features and optimal GEKO parameters, enabling the trained model's generalization. This approach allows computationally faster simulations of swirling flow using an optimized GEKO model matching the predictions of LES. This methodology is tested on the DLR PRECCINSTA burner considering a nonreacting, isothermal flow scenario. The velocity field variance between LES and GEKO-RANS solutions is defined as the objective function, with the turbulent kinetic energy (TKE) source coefficient serving as the tuning parameter. Results using the optimized GEKO model demonstrate qualitative and quantitative agreement with LES and experiments. The trained neural network (NN) model's generalization is tested on various flow conditions, including six additional Reynolds numbers and a reacting flow scenario, showcasing significant improvements over the baseline model solution. This optimized workflow holds promise for future studies involving different geometries with similar flow fields.
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      Tuning of Generalized K-Omega Turbulence Model by Using Adjoint Optimization and Machine Learning for Gas Turbine Combustor Applications

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4302913
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKlavaris, George
    contributor authorXu, Min
    contributor authorHill, Chris
    contributor authorMenter, Florian
    contributor authorPatwardhan, Saurabh
    contributor authorVerma, Ishan
    date accessioned2024-12-24T18:52:46Z
    date available2024-12-24T18:52:46Z
    date copyright2/26/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_146_08_081014.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302913
    description abstractTurbulence modeling plays a crucial role in swirl-stabilized gas turbine combustors, typically relying on scale-resolved simulations (SRS) such as large eddy simulations (LES). However, LES is computationally expensive due to the need for fine mesh resolution and small time-steps required to capture the combustor's large-scale turbulence motion accurately. On the other hand, Reynolds-averaged Navier–Stokes (RANS) models while computationally efficient, lack fidelity in predicting complex flow characteristics such as swirl accurately. In this study, the GEKO model is used for simulating RANS predictions of turbulence in a swirling flow scenario, whereas high-fidelity LES predictions serve as target data enabling field inversion via gradient-based optimization using the Adjoint solver in ansysfluent. Machine learning via neural network (NN) Training is employed to establish correlations between turbulent flow features and optimal GEKO parameters, enabling the trained model's generalization. This approach allows computationally faster simulations of swirling flow using an optimized GEKO model matching the predictions of LES. This methodology is tested on the DLR PRECCINSTA burner considering a nonreacting, isothermal flow scenario. The velocity field variance between LES and GEKO-RANS solutions is defined as the objective function, with the turbulent kinetic energy (TKE) source coefficient serving as the tuning parameter. Results using the optimized GEKO model demonstrate qualitative and quantitative agreement with LES and experiments. The trained neural network (NN) model's generalization is tested on various flow conditions, including six additional Reynolds numbers and a reacting flow scenario, showcasing significant improvements over the baseline model solution. This optimized workflow holds promise for future studies involving different geometries with similar flow fields.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTuning of Generalized K-Omega Turbulence Model by Using Adjoint Optimization and Machine Learning for Gas Turbine Combustor Applications
    typeJournal Paper
    journal volume146
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4064367
    journal fristpage81014-1
    journal lastpage81014-10
    page10
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 008
    contenttypeFulltext
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