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    Calibration of a Computational Fluid Dynamics Methodology for the Simulation of Roughness Effects on Friction and Heat Transfer in Additive Manufactured Components 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 008:;page 81002-1
    Author(s): Mazzei, Lorenzo; Da Soghe, Riccardo; Bianchini, Cosimo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is well known from the literature that surface roughness significantly affects friction and heat transfer. This is even more evident for additive manufactured (AM) components, which are taking an increasingly important ...
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    Numerical Benchmark of Nonconventional RANS Turbulence Models for Film and Effusion Cooling 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 004:;page 41026
    Author(s): Bianchini, Cosimo; Andrei, Luca; Andreini, Antonio; Facchini, Bruno
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Over the course of the years, several turbulence models specifically developed to improve the predicting capabilities of conventional twoequations Reynoldsaveraged Navier–Stokes (RANS) models have been proposed. They ...
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    Effects of Impeller Squealer Tip on Centrifugal Compressor Performance 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 003:;page 32603
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; Tommaso Rubino, Dante; Toni, Lorenzo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes the main results sorted out from a design of experiment (DoE) based on a validated computational fluid dynamics (CFD). Several tip recessed geometries applied to an unshrouded impeller were considered ...
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    Numerical Characterization of Flow and Heat Transfer in Preswirl Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 007:;page 71901
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; D'Errico, Jacopo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with a numerical study aimed at the validation of a computational procedure for the aerothermal characterization of preswirl systems employed in axial gas turbines. The numerical campaign focused on an ...
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    Effect of Temperature Ratio on Jet Impingement Heat Transfer in Active Clearance Control Systems 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 008:;page 81009
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; D’Errico, Jacopo; Tarchi, Lorenzo
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Impinging jet arrays are typically used to cool several gas turbine parts. Some examples of such applications can be found in the internal cooling of high-pressure turbine airfoils or in the turbine blade tip clearances ...
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    On the Extrapolation of Rim Sealing Performance From Test Bench to Real Engine: A Numerical Survey 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 004:;page 41001-1
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; Mazzei, Lorenzo; Bonini, Alessio; Innocenti, Luca; Di Benedetto, Daniele; Orsini, Lorenzo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The main annulus hot gas ingress into turbine wheel-spaces is still one of the most challenging problems designers face. During the decades, several experimental test benches were developed worldwide to improve the knowledge ...
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    Thermofluid Dynamic Analysis of a Gas Turbine Transition Piece 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 006:;page 62602
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; Andreini, Antonio; Mazzei, Lorenzo; Riccio, Giovanni; Marini, Alessandro; Ciani, Alessandro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The transitionpiece of a gas turbine engine is subjected to high thermal loads as it collects high temperature combustion products from the gas generator to a turbine. This generally produces high thermal stress levels in ...
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    Investigation on the Effect of a Realistic Flow Field on the Adiabatic Effectiveness of an Effusion Cooled Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 005:;page 51501
    Author(s): Andrei, Luca; Andreini, Antonio; Bianchini, Cosimo; Facchini, Bruno; Mazzei, Lorenzo; Turrini, Fabio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Effusion cooling represents the state of the art of liner cooling technology for modern combustors. This technique consists of an array of closely spaced discrete film cooling holes and contributes to lower the metal ...
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    Heat Transfer Augmentation Due to Coolant Extraction on the Cold Side of Active Clearance Control Manifolds 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 002:;page 21507
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; Andreini, Antonio; Facchini, Bruno; Mazzei, Lorenzo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Jet array is an arrangement typically used to cool several gas turbine parts. Some examples of such applications can be found in the impingement cooled region of gas turbine airfoils or in the turbine blade tip clearances ...
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    Metal Temperature Prediction of a Dry Low NOx Class Flame Tube by Computational Fluid Dynamics Conjugate Heat Transfer Approach 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 003:;page 31501
    Author(s): Da Soghe, Riccardo; Bianchini, Cosimo; Andreini, Antonio; Mazzei, Lorenzo; Riccio, Giovanni; Marini, Alessandro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Combustor liner of present gas turbine engines is subjected to high thermal loads as it surrounds high temperature combustion reactants and is hence facing the related radiative load. This generally produces high thermal ...
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