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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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