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    A Novel Large-Eddy Simulation-Based Process for NOx Emission Assessment in a Premixed Swirl Stabilized Combustion System 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11010-1
    Author(s): Meloni, R.; Andreini, A.; Nassini, P. C.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new computational fluid dynamics (CFD) approach for the assessment of NOx emission. The methodology is validated against the experimental data of a heavy-duty gas turbine annular combustor. Since the ...
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    A Dynamic Thickening Strategy for High-Fidelity Computational Fluid Dynamics Analyses of Multi-Regime Combustion 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 012:;page 121010-1
    Author(s): Ballotti, A.; Castellani, S.; Andreini, A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study, a dynamic thickening strategy for dynamic thickened flame model for large eddy simulations (DTFLES) application to multi-regime combustion is proposed. The main idea lies in using the numerical solution of ...
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    Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 008:;page 81007-1
    Author(s): Amerini, A.; Paccati, S.; Mazzei, L.; Andreini, A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Computational fluid dynamics (CFD) plays a crucial role in the design of cooling systems in gas turbine combustors due to the difficulties and costs related to experimental measurements performed in pressurized reactive ...
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    CO Emission Modeling in a Heavy Duty Annular Combustor Operating With Natural Gas 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11011-1
    Author(s): Meloni, R.; Gori, S.; Andreini, A.; Nassini, P. C.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes the development of a large-eddy simulation (LES)-based approach for the prediction of CO emission in an industrial gas turbine combustor. Since the operating point of the modern combustors is really ...
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    Development of a Virtual Chemistry Reaction Mechanism for H2/CH4 Turbulent Combustion Modelling 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 004:;page 41003-1
    Author(s): Castellani, S.; Andreini, A.; Meloni, R.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The identification of the combustion model is always guided by the compromise between accuracy and computational cost. While species transport models offer accuracy, their computational cost requirement can become prohibitive, ...
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    Unsteady Computational Fluid Dynamics Investigation of Effusion Cooling Process in a Lean Burn Aero-Engine Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 001:;page 11502
    Author(s): Mazzei, L.; Picchi, A.; Andreini, A.; Facchini, B.; Vitale, I.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work describes the main findings of a computational fluid dynamics (CFD) analysis intended to accurately investigate the flow field and wall heat transfer as a result of the mutual interaction between a swirling flow ...
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    Hybrid RANS-LES Modeling of the Aerothermal Field in an Annular Hot Streak Generator for the Study of Combustor–Turbine Interaction 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 002:;page 21508
    Author(s): Andreini, A.; Bacci, T.; Insinna, M.; Mazzei, L.; Salvadori, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The adoption of lean-burn technology in modern aero-engines influences the already critical aerothermal conditions at turbine entry, where the absence of dilution holes preserves the swirl component generated by burners ...
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    Modeling Strategies for Large Eddy Simulation of Lean Burn Spray Flames 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 005:;page 51501
    Author(s): Puggelli, S.; Bertini, D.; Mazzei, L.; Andreini, A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Over the last years, aero-engines are progressively evolving toward design concepts that permit improvements in terms of engine safety, fuel economy, and pollutant emissions. With the aim of satisfying the strict NOx ...
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    Impact of Predicted Combustor Outlet Conditions on the Aerothermal Performance of Film-Cooled High Pressure Turbine Vanes 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 005:;page 51011
    Author(s): Cubeda, S.; Mazzei, L.; Bacci, T.; Andreini, A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine inlet conditions in lean-burn aeroengine combustors are highly swirled and present nonuniform temperature distributions. Uncertainty and lack of confidence associated with combustor-turbine interaction affect ...
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    Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 006:;page 061008-1
    Author(s): Lenzi, T.; Palanti, L.; Picchi, A.; Bacci, T.; Mazzei, L.; Andreini, A.; Facchini, B.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film-cooling jets behavior in a combustor chamber is deeply affected by swirling flow interactions and unsteadiness; on the other hand, the jets behavior has a direct impact on different phenomena such as cooling capabilities ...
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