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    Discharge Coefficients of a Preswirl System in Secondary Air Systems 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 001:;page 119
    Author(s): M. Dittmann; T. Geis; V. Schramm; S. Kim; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The discharge behavior of a “direct-transfer” preswirl system has been investigated experimentally. The influences of the pressure ratio and the swirl ratio as well as the influence of the ...
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    Influence of Rub-Grooves on Labyrinth Seal Leakage 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 387
    Author(s): J. Denecke; V. Schramm; S. Kim; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation on the influence of stator rub-grooves on labyrinth seal leakage is presented in the present paper. In current labyrinth seal designs, abradable lands allow the ...
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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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