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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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    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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    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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    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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    Unsteady Flow in a Centrifugal Compressor With Different Types of Vaned Diffusers 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 003:;page 293
    Author(s): U. Haupt; A. N. Abdel-Hamid; M. Rautenberg; U. Seidel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to investigate the characteristics of self-excited flow oscillations in a high-performance centrifugal compressor system with a straight channel radial vaned diffuser. ...
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    Discussion: “Detection of a Rotating Stall Precursor in Isolated Axial Flow Compressor Rotors” (Inoue, M., Kuroumaru, M., Iwamoto, T., and Ando, Y., 1991, ASME J. Turbomach., 113, pp. 281–287) 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 288
    Author(s): Y. N. Chen; U. Haupt; U. Seidel; M. Rautenberg
    Publisher: The American Society of Mechanical Engineers (ASME)
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