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    Investigation of Blade Vibration of Radial Impellers by Means of Telemetry and Holographic Interferometry 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004:;page 838
    Author(s): U. Haupt; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: On a high-pressure, high-mass flow, centrifugal compressor blade vibration measurements are carried out to determine the excitation mechanism in various operating ranges. For these experiments ...
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    Comparisons of the Relative Effect of Tip Clearance on Centrifugal Impellers 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004:;page 545
    Author(s): A. Engeda; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Why do some centrifugal impellers exhibit high sensitivity to tip clearance losses while others don’t? This may be understood by considering the geometric and fluid mechanics design parameters ...
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    Analysis of Measurements in Vaned Diffusers of Centrifugal Compressors 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 001:;page 115
    Author(s): W. Stein; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In vaned diffusers of centrifugal compressors many different flow phenomena interfere with one another, and different geometric parameters influence the flow field. Variations of these parameters ...
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    Blade Vibration Measurements on Centrifugal Compressors by Means of Telemetry and Holographic Interferometry 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 001:;page 70
    Author(s): U. Haupt; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Blade vibration measurements have been carried out on a high-pressure, high mass-flow centrifugal compressor to determine the excitation mechanism. For the experimental investigation, semiconductor ...
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    A Distinction Between Different Types of Stall in a Centrifugal Compressor Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 001:;page 83
    Author(s): N. Kämmer; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow at the stall line of a centrifugal compressor with vaneless diffuser was investigated at different speeds. A distinction between three kinds of stall phenomena could be made. One type ...
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    The Vortex-Filament Nature of Reverse Flow on the Verge of Rotating Stall 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 004:;page 450
    Author(s): Y. N. Chen; U. Haupt; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: On the verge of rotating stall, very orderly reverse flow forms from the outlet of the rotor/impeller along the casing/shroud toward the inlet in axial/centrifugal compressors (Koch, 1970; Haupt, ...
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    On the Mechanism of Dangerous Blade Vibration Due to Blade Flow Interactions on Centrifugal Compressors 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004:;page 702
    Author(s): U. Haupt; D. F. Jin; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Severe blade flow interactions at part-load operation conditions were investigated on a centrifugal compressor with a vaned diffuser leading to material stresses beyond the allowable values. By ...
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    Discussion: “Rotating Waves as a Stall inception Indication in Axial Compressors” (Garnier, V. H., Epstein, A. H., and Greitzer, E. M., 1991, ASME J. Turbomach., 113, pp. 290–301) 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 301
    Author(s): Y. N. Chen; U. Haupt; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Matching of Turbocomponents Described by the Example of Impeller and Diffuser in a Centrifugal Compressor: Part I—Aerothermodynamic Coupling of Impeller and Diffuser. Part II—Optimized Stage Efficiency of a Centrifugal Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 003:;page 594
    Author(s): K. Bammert; W. Wittekindt; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An important task in the design of turbo machinery is the determination of the aerothermodynamic parameters necessary to assure optimum matching of the individual compressor components. With ...
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    Blade Excitation by Broad-Band Pressure Fluctuations in a Centrifugal Compressor 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 001:;page 129
    Author(s): U. Haupt; A. N. Abdel-Hamid; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The mechanism of blade excitation during the operation of a high-mass-flow, high-pressure-ratio centrifugal compressor has been investigated. This was carried out in the compressor operating range ...
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