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    A Comprehensive Investigation of Blade Row Interaction Effects on Stator Loss Utilizing Vane Clocking 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 007:;page 71004
    Author(s): Smith, Natalie R.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Blade row interactions drive the unsteady performance of high-pressure compressors. Vane clocking is the relative circumferential positioning of consecutive stationary vane rows with the same vane count. By altering the ...
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    Experimentally Measured Effectiveness of Different Shroud Swirl Brake Profiles in a Centrifugal Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 005:;page 51012-1
    Author(s): Wilkes, Jason; Smith, Natalie; Venkataraman, Balaji; Vagani, Marco; Goucher, Sara
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As centrifugal compressors are pushed to operate at higher pressures and higher power levels, destabilizing gas forces often increase the challenge of designing a stable rotordynamic system. While technical innovations ...
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    Considerations for Measuring Compressor Aerodynamic Excitations Including Rotor Wakes and Tip Leakage Flows 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 003:;page 31008
    Author(s): Smith, Natalie R.; Murray, III ,William L.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow field generated by the rotor provides unsteady aerodynamic excitations to the downstream stator, which can result in vibrations such as forced response. In this paper, measurements of the rotor wake and ...
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    Design of a Wide-Range Centrifugal Compressor Stage for Supercritical CO2 Power Cycles 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 009:;page 92602
    Author(s): Pelton, Robert; Jung, Sewoong; Allison, Tim; Smith, Natalie
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Supercritical carbon dioxide (sCO2) power cycles require high compressor efficiency at both the design point and over a wide operating range. Increasing the compressor efficiency and range helps maximize the power output ...
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    Humidity Effects on Experimental Compressor Performance—Corrected Conditions for Real Gases 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 003:;page 31011
    Author(s): Berdanier, Reid A.; Smith, Natalie R.; Fabian, John C.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of humid air on the performance of a multistage research compressor and new methods of humidity accounting to ensure appropriate representation of performance parameters are investigated in this paper. ...
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    Reconciling Compressor Performance Differences for Varying Ambient Inlet Conditions 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 012:;page 122603
    Author(s): Smith, Natalie R.; Berdanier, Reid A.; Fabian, John C.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Careful experimental measurements can capture small changes in compressor total pressure ratio (TPR), which arise with subtle changes in an experiment's configuration. Research facilities that use unconditioned atmospheric ...
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    Experimental Validation of a Wide-Range Centrifugal Compressor Stage for Supercritical CO2 Power Cycles 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 006:;page 61011
    Author(s): Allison, Timothy C.; Smith, Natalie R.; Pelton, Robert; Wilkes, Jason C.; Jung, Sewoong
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Successful implementation of sCO2 power cycles requires high compressor efficiency at both the design-point and over a wide operating range in order to maximize cycle power output and maintain stable operation over a wide ...
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    The Comparison of Aerodynamic Performance Data Acquired From Thermal Measurements and a Torquemeter on a Compressor Impeller 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004:;page 41011
    Author(s): Smith, Natalie R.; Allison, Timothy C.; Wilkes, Jason C.; Clarke, Christopher; Cave, Michael
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Full-thermal heat-soak of machinery is vital for acquiring accurate aerodynamic performance data, but this process often requires significant testing time to allow all facility components to reach a steady-state temperature. ...
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