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    Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 815
    Author(s): K. Willenborg; S. Kim; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of Reynolds number and pressure ratio on the operating characteristics of a stepped labyrinth seal was experimentally determined. The geometries investigated represent designs of a ...
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    Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001:;page 133
    Author(s): K. Willenborg; V. Schramm; S. Kim; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of a honeycomb facing on the heat transfer of a stepped labyrinth seal with geometry typical for modern jet engines was investigated. Heat transfer measurements were obtained for ...
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    Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001:;page 140
    Author(s): V. Schramm; K. Willenborg; S. Kim; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports numerical predictions and measurements of the flow field in a stepped labyrinth seal. The theoretical work and the experimental investigations were successfully combined to ...
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    Experimental Analysis of Air∕Oil Separator Performance 

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 006:;page 62503
    Author(s): K. Willenborg; S. Tebby; P. Gorse; K. Dullenkopf; T. Ratcliffe; M. Klingsporn; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Within the European research project (Advanced Transmission and Oil System Concepts), a systematic study of the separation efficiency of a typical aeroengine air∕oil separator design was conducted. ...
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