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    Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091016-1
    Author(s): Koppe, Björn; Lange, Martin; Mailach, Ronald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For an axial compressor stator with tip gap, the boundary layer (BL) in the hub endwall region has a significant influence on the development and progression of the tip leakage vortex. Herein, the so-called BL skew, which ...
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    Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007:;page 71015-1
    Author(s): Chen, Xiangyi; Koppe, Björn; Lange, Martin; Chu, Wuli; Mailach, Ronald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Rotating instability (RI) can be regarded as a pre-stall signal because such phenomena are usually detected when a compressor operates at a near-stall point. Since RI is closely relevant to aerodynamic, acoustic, and ...
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    Effects of Rotation on the Flow Structure in a Compressor Cascade 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 008:;page 81006-1
    Author(s): Ventosa-Molina, Jordi; Koppe, Björn; Lange, Martin; Mailach, Ronald; Fröhlich, Jochen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In turbomachines, rotors and stators differ by the rotation of the former. Hence, half of each stage is directly influenced by rotation effects. The influence of rotation on the flow structure and its impact on the performance ...
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