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    Phantom Cooling Effects on Rotor Blade Surface Heat Flux in a Transonic Full Scale 1 + 1/2 Stage Rotating Turbine 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003:;page 31016-1
    Author(s): Anthony, Richard J.; Finnegan, John; Clark, John P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and numerical investigation of phantom cooling effects on cooled and uncooled rotating high pressure turbine blades in a full scale 1 + 1/2 stage turbine test is presented. Objectives set to capture, separate, ...
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    Unsteady Aerodynamic Interaction in a Closely Coupled Turbine Consistent With Contrarotation 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 006:;page 61004
    Author(s): Ooten, Michael K.; Anthony, Richard J.; Lethander, Andrew T.; Clark, John P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The focus of the study presented here was to investigate the interaction between the blade and downstream vane of a stageandonehalf transonic turbine via computation fluid dynamic (CFD) analysis and experimental data. A ...
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    Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part I: Airfoil Design 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 008:;page 81005
    Author(s): Eric Lyall, M.; King, Paul I.; Clark, John P.; Sondergaard, Rolf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the reasoning for and the design process of contouring a high lift frontloaded low pressure turbine (LPT) airfoil near the endwall to reduce the endwall loss. The test airfoil, L2F, was designed to the ...
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    The Effect of Manufacturing Variations on Unsteady Interaction in a Transonic Turbine 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 006:;page 61007
    Author(s): Clark, John P.; Beck, Joseph A.; Kaszynski, Alex A.; Still, Angela; Ni, Ron-Ho
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This effort focuses on the comparison of unsteadiness due to as-measured turbine blades in a transonic turbine to that obtained with blueprint geometries via computational fluid dynamics (CFD). A Reynolds-averaged Navier–Stokes ...
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    On the Development of High-Lift, High-Work Low-Pressure Turbines 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 012:;page 121011-1
    Author(s): Clark, John P.; Paniagua, Guillermo; Cukurel, Beni
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Here, we describe a combined design, numerical, and experimental program intended substantially to increase the lift and work of low-pressure turbine stages. This exercise is critically dependent upon the appropriate ...
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    Effects of Downstream Vane Bowing and Asymmetry on Unsteadiness in a Transonic Turbine 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 010:;page 101006
    Author(s): Clark, John P.; Anthony, Richard J.; Ooten, Michael K.; Finnegan, John M.; Dean Johnson, P.; Ni, Ron-Ho
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Accurate predictions of unsteady forcing on turbine blades are essential for the avoidance of high-cycle-fatigue issues during turbine engine development. Further, if one can demonstrate that predictions of unsteady ...
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    Response of Separated Boundary Layers to Steady and Pulsated Flow Injection 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 006:;page 61001-1
    Author(s): Nowak, Hunter D.; Lluesma-Rodriguez, Federico; Rahbari, Iman; Clark, John P.; Paniagua, Guillermo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new class of power generation devices that experiences increased losses due to bulk flow separation in segments of their expected in-flight regime is emerging. As such, active flow control becomes increasingly relevant ...
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