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    Two-Phase Air/Oil Flow in Aero Engine Bearing Chambers: Characterization of Oil Film Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003:;page 578
    Author(s): A. Glahn; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: For the design of secondary air and lubrication oil systems, a sufficient knowledge of two-phase flow and heat transfer phenomena under bearing chamber flow conditions is required. The ...
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    Influence of High Rotational Speeds on Heat Transfer and Oil Film Thickness in Aero-Engine Bearing Chambers 

    Source: Journal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 002:;page 395
    Author(s): S. Wittig; A. Glahn; J. Himmelsbach
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Increasing the thermal loading of bearing chambers in modern aero-engines requires advanced techniques for the determination of heat transfer characteristics. In the present study, film thickness ...
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    Feasibility Study on Oil Droplet Flow Investigations Inside Aero Engine Bearing Chambers—PDPA Techniques in Combination With Numerical Approaches 

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 004:;page 749
    Author(s): A. Glahn; M. Kurreck; M. Willmann; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper deals with oil droplet flow phenomena in aero engine bearing chambers. An experimental investigation of droplet sizes and velocities utilizing a Phase Doppler Particle Analyzer ...
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    Main Gas Ingestion in a Turbine Stage for Three Rim Cavity Configurations 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31023
    Author(s): D. W. Zhou; C.-Z. Wang; J. A. Glahn; R. P. Roy
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were carried out in a model air turbine stage to study the influence of rotor-stator rim cavity configuration on the ingestion of mainstream gas into the cavity. The three rim ...
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    Droplet Generation by Disintegration of Oil Films at the Rim of a Rotating Disk 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001:;page 117
    Author(s): A. Glahn; S. Busam; M. F. Blair; K. L. Allard; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fundamental study has been performed to examine oil film disintegration mechanisms at the rim of a rotating disk. The configuration investigated is an abstraction of one of the droplet ...
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    Disintegration of Oil Jets Emerging From Axial Passages at the Face of a Rotating Cylinder 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 004:;page 1003
    Author(s): K. L. Allard; S. Busam; A. Glahn; M. F. Blair; O. Schäfer; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fundamental study has been performed to examine the disintegration of oil films emerging from axial passages at the face of a rotating cylinder. The investigation has been conducted in ...
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    Disintegration of Oil Films Emerging From Radial Holes in a Rotating Cylinder 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 004:;page 1011
    Author(s): K. L. Allard; S. Busam; A. Glahn; M. F. Blair; O. Schäfer; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fundamental study has been performed to examine the disintegration of oil films emerging from radial holes in a rotating hollow cylinder. The configuration investigated is an abstraction of ...
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