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    Numerical and Experimental Investigation of Return Channel Vane Aerodynamics With Two-Dimensional and Three-Dimensional Vanes 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 001:;page 11010
    Author(s): Hildebrandt, A.; Schilling, F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper deals with the numerical and experimental investigation of the effect of return channel (RCH) dimensions of a centrifugal compressor stage on the aerodynamic performance. Three different return channel ...
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    One-Dimensional and Three-Dimensional Design Strategies for Pressure Slope Optimization of High-Flow Transonic Centrifugal Compressor Impellers 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 005:;page 51002
    Author(s): Hildebrandt, A.; Ceyrowsky, T.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with the numerical and theoretical investigations of the effect of geometrical dimensions and one-dimensional (1D)-design parameters on the impeller pressure slope of a transonic centrifugal compressor ...
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    Secondary Flows in the Return System of a Centrifugal Compressor Stage 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 009:;page 091002-1
    Author(s): Rossbach, T.; Bisping, J.; Grates, D. R.; Jeschke, P.; Hildebrandt, A.; Franz, H.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an analysis of the flow in the return system of a centrifugal compressor with a flow coefficient of 0.15. Based on the detailed experimental and numerical data, the areas of high losses and potentials ...
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