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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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    Effect of a Combined Hot-Streak and Swirl Profile on Cooled 1.5-Stage Turbine Aerodynamics: An Experimental and Computational Study 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 002:;page 021011-1
    Author(s): Adams, Maxwell G.; Beard, Paul F.; Stokes, Mark R.; Wallin, Fredrik; Chana, Kam S.; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recently developed lean-burn combustors offer reduced NOx emissions for gas turbines. The flow at exit of lean-burn combustors is dominated by hot streaks and residual swirl, which have been shown—individually—to impact ...
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    Commissioning of a Combined Hot-Streak and Swirl Profile Generator in a Transonic Turbine Test Facility 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 003:;page 031008-1
    Author(s): Adams, Maxwell G.; Povey, Thomas; Hall, Benjamin F.; Cardwell, David N.; Chana, Kam S.; Beard, Paul F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: By enhancing the premixing of fuel and air prior to combustion, recently developed lean-burn combustor systems have led to reduced NOx and particulate emissions in gas turbines. Lean-burn combustor exit flows are typically ...
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