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    Effects of Transient Heat Transfer on Compressor Stability 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 012:;page 121003
    Author(s): Kiss, A.; Spakovszky, Z.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of heat transfer between the compressor structure and the primary gas path flow on compressor stability are investigated during hot engine re-acceleration transients. A mean line analysis of an advanced, ...
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    Forced Response System Identification of Full Aero-Engine Rotordynamic Systems for Prognostics and Diagnostics 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 010:;page 101008
    Author(s): Hur, I.;Spakovszky, Z. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A first-of-its-kind forced-response system identification approach is introduced to measure rotordynamic damping of shaft modes in a full gas turbine aero-engine. The approach involves forced-response modal analysis in ...
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    An Investigation of Condensation Effects in Supercritical Carbon Dioxide Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 008:;page 82602
    Author(s): Lettieri, C.; Yang, D.; Spakovszky, Z.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Supercritical CO2 (SCO2) power cycles have demonstrated significant performance improvements in concentrated solar and nuclear applications. These cycles promise an increase in thermaltoelectric conversion efficiency of ...
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    Low Flow Coefficient Centrifugal Compressor Design for Supercritical CO2 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 008:;page 81008
    Author(s): Lettieri, C.; Baltadjiev, N.; Casey, M.; Spakovszky, Z.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a design strategy for very low flow coefficient multistage compressors operating with supercritical CO2 for carbon capture and sequestration (CCS) and enhanced oil recovery (EOR). At flow coefficients ...
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    Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 002:;page 21009
    Author(s): Shah, P.; Robinson, A.; Price, A.; Spakovszky, Z.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The feasibility of a drag management device that reduces engine thrust on approach by generating a swirling outflow from the fan (bypass) nozzle is assessed. Deployment of such “engine airbrakesâ€‌ (EABs) can assist in ...
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    Dynamic Model-Based Identification of Cavitation Compliance and Mass Flow Gain Factor in Rocket Engine Turbopump Inducers 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 002:;page 021011-1
    Author(s): Wan, Y.; Manfredi, M.; Pasini, A.; Spakovszky, Z.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cavitation dynamics continue to pose a significant risk in the development and operation of launch vehicle (LV) propulsion systems. In addition to generating unsteady loads that can directly damage turbopump hardware, ...
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    Origins and Structure of Spike Type Rotating Stall 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 005:;page 51007
    Author(s): Pullan, G.; Young, A. M.; Day, I. J.; Greitzer, E. M.; Spakovszky, Z. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we describe the structures that produce a spiketype route to rotating stall and explain the physical mechanism for their formation. The descriptions and explanations are based on numerical simulations, ...
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    The Role of Tip Leakage Flow in Spike-Type Rotating Stall Inception 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 006:;page 61010
    Author(s): Hewkin-Smith, M.; Pullan, G.; Grimshaw, S. D.; Greitzer, E. M.; Spakovszky, Z. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the role of tip leakage flow in creating the leading edge separation necessary for the onset of spike-type compressor rotating stall. A series of unsteady multipassage simulations, supported by ...
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