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    Predicting High Lift Low Pressure Turbine Cascades Flow Using Transition Sensitive Turbulence Closures 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005:;page 51007
    Author(s): Pacciani, Roberto; Marconcini, Michele; Arnone, Andrea; Bertini, Francesco
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the application of different transitionsensitive turbulence closures to the prediction of lowReynoldsnumber flows in highlift cascades operating in lowpressure turbine (LPT) conditions. Different ...
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    Integration of Machine Learning and Computational Fluid Dynamics to Develop Turbulence Models for Improved Low-Pressure Turbine Wake Mixing Prediction 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 012:;page 0121001-1
    Author(s): Akolekar, Harshal D.; Zhao, Yaomin; Sandberg, Richard D.; Pacciani, Roberto
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the development of accurate turbulence closures for low-pressure turbine (LPT) wake mixing prediction by integrating a machine-learning approach based on gene expression programming (GEP), with ...
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    Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091011-1
    Author(s): Pinelli, Lorenzo; Marconcini, Michele; Pacciani, Roberto; Gaetani, Paolo; Persico, Giacomo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article describes the transport and the interaction of pulsating entropy waves generated by combustor burners within a high-pressure turbine stage for aeronautical application. Experiments and computational fluid ...
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    The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 003:;page 31004-1
    Author(s): Pinelli, Lorenzo; Marconcini, Michele; Pacciani, Roberto; Notaristefano, Andrea; Gaetani, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: First stages of aeronautical high-pressure turbines are subjected to significant inlet distortions generated by the combustor system. These disturbances are characterized by velocity and temperature fluctuations convected ...
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    Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 005:;page 51009-1
    Author(s): Pacciani, Roberto; Marconcini, Michele; Arnone, Andrea; Bertini, Francesco; Spano, Ennio; Rosa Taddei, Simone; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this article, novel machine-learnt transition and turbulence models are applied to the prediction of boundary-layer transition and wake mixing in a low-pressure turbine (LPT) cascade, including unsteady inflow cases ...
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    The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 004:;page 41003-1
    Author(s): Pinelli, Lorenzo; Giannini, Giovanni; Marconcini, Michele; Pacciani, Roberto; Notaristefano, Andrea; Gaetani, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The study of component interactions in aeronautical engines is a key aspect to improve the aerodynamic, aeromechanical, and thermal performance and to reduce greenhouse gas and noise emissions. In this context, combustor ...
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    Large Eddy Simulation and RANS Analysis of the End-Wall Flow in a Linear Low-Pressure-Turbine Cascade—Part II: Loss Generation 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 005:;page 51004
    Author(s): Marconcini, Michele; Pacciani, Roberto; Arnone, Andrea; Michelassi, Vittorio; Pichler, Richard; Zhao, Yaomin; Sandberg, Richard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In low-pressure turbines (LPT) at design point, around 60–70% of losses are generated in the blade boundary layers far from end walls, while the remaining 30–40% is controlled by the interaction of the blade profile with ...
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    Computational and Experimental Study of Hot Streak Transport Within the First Stage of a Gas Turbine 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 008:;page 081002-1
    Author(s): Gaetani, Paolo; Persico, Giacomo; Pinelli, Lorenzo; Marconcini, Michele; Pacciani, Roberto
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper discusses the migration, the interaction with the blades, and the attenuation of hot streaks generated by combustor burners, during their propagation within the first turbine stage of aero-engines. Experiments ...
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    A Data-Driven Approach for Generalizing the Laminar Kinetic Energy Model for Separation and Bypass Transition in Low- and High-Pressure Turbines 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 009:;page 91005-1
    Author(s): Fang, Yuan; Zhao, Yaomin; Akolekar, Harshal D.; Ooi, Andrew S. H.; Sandberg, Richard D.; Pacciani, Roberto; Marconcini, Michele
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: No common laminar kinetic energy (LKE) transition model has to date been able to predict both separation-induced and bypass transition, both phenomena commonly found in low-pressure turbines and high-pressure turbines. ...
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