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    Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data—Part 1: Methodology and Sensitivity Analysis 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 008:;page 081002-1
    Author(s): Lou, Fangyuan; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field in a compressor is circumferentially non-uniform due to the wakes from upstream stators, the potential field from both upstream and downstream stators, and blade row interactions. This non-uniform flow impacts ...
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    Compressor Stall Warning Using Nonlinear Feature Extraction Algorithms 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 012:;page 0121005-1
    Author(s): Lou, Fangyuan; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stall is a type of flow instability in compressors that sets the low-flow limit for compressor operation. During the past few decades, efforts to develop a reliable stall warning system have had limited success. This paper ...
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    A New Approach to Modeling Slip and Work Input for Centrifugal Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 002:;page 021013-1
    Author(s): Harrison, Herbert M.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new method of modeling slip factor and work input for centrifugal compressor impellers is presented. Rather than using geometry to predict the behavior of the flow at the impeller exit, the new method leverages governing ...
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    Utilization of Fast Response Pressure Measurements to Non-Intrusively Monitor Blade Vibration in Axial Compressors 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 003
    Author(s): Leng, Yujun; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A novel non-intrusive method has been developed to monitor rotor blade vibration using unsteady casing pressure. The present blade vibration monitoring technique utilizes casing unsteady pressure sensors that can detect ...
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    On Choosing the Optimal Impeller Exit Velocity Triangles in Preliminary Design 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 011:;page 111011
    Author(s): Lou, Fangyuan;Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Impeller discharge flow plays an important role in centrifugal compressor performance and operability for two reasons. First, it determines the work factor and relative diffusion for the impeller. Second, it sets the flow ...
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    The Effect of Gas Models on Compressor Efficiency Including Uncertainty 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 001:;page 12601
    Author(s): Lou, Fangyuan; Fabian, John; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Since isentropic efficiency is widely used in evaluating the performance of compressors, it is essential to accurately calculate this parameter from experimental measurements. Quantifying realistic bounds of uncertainty ...
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    The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005:;page 52605
    Author(s): Berdanier, Reid A.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large rotor tip clearances and the associated tip leakage flows are known to have a significant effect on overall compressor performance. However, detailed experimental data reflecting these effects for a multistage ...
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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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    Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser—Part I: Surge Signature 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 005:;page 51003-1
    Author(s): Lou, Fangyuan; Harrison, Herbert M.; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The identification of stall inception mechanisms and stability-limiting components in a centrifugal compressor is required for the development of effective surge suppression approaches. Part I of this two-part paper ...
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    Details of Shrouded Stator Hub Cavity Flow in a Multistage Axial Compressor Part 2: Leakage Flow Characteristics in Stator Wells 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11027-1
    Author(s): Kamdar, Nitya; Lou, Fangyuan; Key, Nicole L.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow in shrouded stator cavities can be quite complex with axial, radial, and circumferential variations. As the leakage flow recirculates and is re-injected into the main flow path upstream of the stator, it deteriorates ...
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