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    High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 009:;page 91009-1
    Author(s): Gloerfelt, Xavier; Cinnella, Paola
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-fidelity numerical simulations based on wall-resolved large-eddy simulations (LESs) are used to investigate the vortex shedding dynamics in a linear turbine cascade. The profile geometry is the well-documented LS59 ...
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    Preliminary Design Method for Dense-Gas Supersonic Axial Turbine Stages 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 011:;page 112605
    Author(s): Bufi, Elio A.; Cinnella, Paola
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fast preliminary design methodology for supersonic organic Rankine cycle (ORC) stator and rotor axial turbine blades with low degree of reaction is presented. First, the stator and rotor blade mean-line profiles are ...
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    Roughness Effects on Dense-Gas Turbine Flow: Comparison of Experiments and Simulations 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81010-1
    Author(s): Gloerfelt, Xavier; Hake, Leander; Bienner, Aurélien; Matar, Camille; Cinnella, Paola; aus der Wiesche, Stefan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article presents a combined numerical and experimental study of the high-subsonic organic vapor flow in a linear turbine cascade. The profile geometry is the well-documented LS59 highly loaded rotor blade and the ...
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