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    Modeling of Surge Characteristics in Turbo Heat Pumps 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 004:;page 41015
    Author(s): Hye Rim Kim; Seung Jin Song
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new analytical model of surge dynamics in turbo heat pumps. Turbo heat pumps use refrigerants as the working fluid and consist of a centrifugal compressor, condenser, ...
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    Lateral Forces From Single Gland Rotor Labyrinth Seals in Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003:;page 626
    Author(s): Bum Ho Song; Seung Jin Song
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Even though interest in labyrinth seal flows has increased recently, an analytical model capable of predicting turbine flow response to labyrinth seals is still lacking. Therefore, this paper ...
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    Nonuniform Flow in a Compressor Due to Asymmetric Tip Clearance 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 004:;page 751
    Author(s): Seung Jin Song; Seung Ho Cho
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an analytical study of flow redistribution in a compressor stage due to asymmetric tip clearance distribution. The entire stage is modeled as an actuator disk and it is ...
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    Clearance Effects on the Onset of Instability in a Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 003:;page 31002
    Author(s): Matthias Schleer; Seung Jin Song; Reza S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This report intends to shed an insight into the effect of large relative tip clearances on the onset of instability in a highly loaded centrifugal compressor. Time-resolved pressure measurements ...
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    Performance Degradation due to Blade Surface Roughness in a Single-Stage Axial Turbine 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 001:;page 137
    Author(s): Yong Il Yun; Il Young Park; Seung Jin Song
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blades experience significant surface degradation with service. Previous studies indicate that an order-of-magnitude or greater increase in roughness height is typical, and these elevated ...
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    Influence of Flow Coefficient, Stagger Angle, and Tip Clearance on Tip Vortex in Axial Compressors 

    Source: Journal of Fluids Engineering:;2006:;volume( 128 ):;issue: 006:;page 1274
    Author(s): Yong Sang Yoon; Hyoun-Woo Shin; Seung Jin Song
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments have been performed on the low speed research compressor (LSRC) at General Electric Aircraft Engines to investigate the effects of flow coefficient, stagger angle, and tip clearance ...
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    Impact of Surface Roughness on Compressor Cascade Performance 

    Source: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 006:;page 64502
    Author(s): Seung Chul Back; June Hyuk Sohn; Seung Jin Song
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental investigation of roughness effects on aerodynamic performance in a low-speed linear compressor cascade. Equivalent sandgrain roughnesses of 12 μm, 180 μm, 300 ...
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    Investigation of Three-Dimensional Unsteady Flows in a Two-Stage Shrouded Axial Turbine Using Stereoscopic PIV—Kinematics of Shroud Cavity Flow 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001:;page 11021
    Author(s): Yong Il Yun; Luca Porreca; Seung Jin Song; Reza S. Abhari; Anestis I. Kalfas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental study of the behavior of leakage flow across shrouded turbine blades. Stereoscopic particle image velocimetry and fast response aerodynamic probe measurements ...
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    Effects of Reynolds Number and Surface Roughness Magnitude and Location on Compressor Cascade Performance 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51013
    Author(s): Seung Chul Back; Garth V. Hobson; Seung Jin Song; Knox T. Millsaps
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation has been conducted to characterize the influence of Reynolds number and surface roughness magnitude and location on compressor cascade performance. Flow field surveys ...
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