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    Study of Near-Stall Flow Behavior in a Modern Transonic Fan With Compound Sweep 

    Source: Journal of Fluids Engineering:;2012:;volume( 134 ):;issue: 007:;page 71101
    Author(s): Chunill Hah; Hyoun-Woo Shin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed flow behavior in a modern transonic fan with a compound sweep is investigated in this paper. Both unsteady Reynolds-averaged Navier-Stokes (URANS) and large eddy simulation (LES) methods ...
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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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    A Stochastic Model for a Compressor Stability Measure 

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003:;page 730
    Author(s): Manuj Dhingra; Andrew Breeze-Stringfellow; Hyoun-Woo Shin; Yedidia Neumeier; J. V. R. Prasad; Peter N. Szucs
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A stability measure rooted in the unsteady characteristics of the flow field over the compressor rotor has been previously developed. The present work explores the relationship between the ...
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