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    A Multifidelity Aero-Thermal Design Approach for Secondary Air Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003:;page 031012-1
    Author(s): Amirante, Dario; Adami, Paolo; Hills, Nicholas J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents a multidisciplinary approach for aero-thermal and heat transfer analysis for internal flows. The versatility and potential benefit offered by the approach are described through the application to a ...
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    Importance of Nonequilibrium Modeling for Compressors 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 004:;page 41017-1
    Author(s): Spencer, Robert; Przytarski, Pawel; Adami, Paolo; Grothe, Patrick; Wheeler, Andrew
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper investigates the importance of nonequilibrium boundary-layer modeling for three compressor blade geometries, using RANS and high-fidelity simulations. We find that capturing nonequilibrium effects in RANS is ...
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    Numerical Investigation of Three-Dimensional Separation in an Axial Flow Compressor: The Influence of Freestream Turbulence Intensity and Endwall Boundary Layer State 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 002:;page 21011
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Regions of three-dimensional separations are an inherent flow feature of the suction surface-endwall corner in axial compressors. These corner separations can cause a significant total pressure loss and reduce the compressor's ...
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    Large Eddy Simulation of Boundary Layer Transition Mechanisms in a Gas-Turbine Compressor Cascade 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 006:;page 61008
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large eddy simulation (LES) is used to explore the boundary layer transition mechanisms in two rectilinear compressor cascades. To reduce numerical dissipation, a novel locally adaptive smoothing (LAS) scheme is added to ...
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    Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81002-1
    Author(s): Vasilopoulos, Ilias; Adami, Paolo; Voigt, Matthias; Meyer, Marcus; Mailach, Ronald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The two-part publication deals with roughness investigations on in-service high-pressure compressor (HPC) blades, both in terms of measurements and simulations. In this paper (Part II), first, stripe measurements of surface ...
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    Impact of Rotor-Casing Effusion Cooling on Turbine Performance and Operating Point: An Experimental, Computational, and Theoretical Study 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 003:;page 031005-1
    Author(s): Adams, Maxwell G.; Adami, Paolo; Collins, Matthew; Beard, Paul F.; Chana, Kam S.; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is known that a secondary effect of rotor-casing effusion cooling is to modify and potentially spoil the rotor over-tip leakage flow. Studies have shown both positive and negative impacts on high-pressure (HP) stage ...
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