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    Modeling of a Steam Turbine Including Partial Arc Admission for Use in a Process Simulation Software Environment 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 011:;page 112605
    Author(s): Liese, Eric
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A dynamic process model of a steam turbine, including partial arc admission operation, is presented. Models were made for the first stage and last stage, with the middle stages assumed to have a constant pressure ratio and ...
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    Using Dynamic Simulation to Evaluate Attemperator Operation in a Natural Gas Combined Cycle With Duct Burners in the Heat Recovery Steam Generator 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 001:;page 11801
    Author(s): Liese, Eric; Zitney, Stephen E.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A generic training simulator of a natural gas combined cycle (NGCC) was modified to match operations at a real plant. The objective was to use the simulator to analyze cycling operations of the plant. Initial operation of ...
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    Impact of Different Volume Sizes on Dynamic Stability of a Gas Turbine-Fuel Cell Hybrid System 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 005
    Author(s): Abrassi, Alessio; Traverso, Alberto; Tucker, David; Liese, Eric
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A dynamic model is developed for a microgas turbine (MGT), characterized by an intrinsic free-spool configuration, coupled to large volumes. This is inspired by an experimental facility at the National Energy Technology ...
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    A Thermodynamic Model to Quantify the Impact of Cooling Improvements on Gas Turbine Efficiency 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 003:;page 31007
    Author(s): Uysal, Selcuk Can; Liese, Eric; Nix, Andrew C.; Black, James
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cooling of turbine hot-gas-path components can increase engine efficiency, reduce emissions, and extend engine life. As cooling technologies evolved, numerous blade cooling geometries have been and continue to be proposed ...
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