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    Laminar and Transitional Boundary Layer Structures in Accelerating Flow With Heat Transfer 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 116
    Author(s): K. Rued; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The accurate prediction of heat transfer coefficients on cooled gas turbine blades requires consideration of various influence parameters. The present study continues previous work with special ...
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    Heat Transfer Measurements Downstream of a Two-Dimensional Jet Entering a Crossflow 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004:;page 572
    Author(s): S. Wittig; V. Scherer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Nusselt and Stanton numbers have been evaluated in and behind the recirculating zone produced by a two-dimensional jet entering a crossflow. The momentum flux ratio of the jet to the main ...
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    Swirl and Counterswirl Effects in Prefilming Airblast Atomizers 

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001:;page 105
    Author(s): M. Aigner; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The performance characteristics of prefilming airblast atomizers depend largely on the shear stresses in each of the two air supply channels. As an extension of previously reported results, ...
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    Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 54
    Author(s): K. Rued; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer and boundary layer measurements were derived from flows over a cooled flat plate with various free-stream turbulence intensities (Tu = 1.6–11 percent), favorable pressure gradients ...
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    Internal Flow Effects in Prefilming Airblast Atomizers: Mechanisms of Atomization and Droplet Spectra 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 003:;page 465
    Author(s): T. Sattelmayer; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fuel atomization with prefilming airblast nozzles has been investigated. The present analysis is directed toward a detailed investigation of the atomization processes and the clarification of the ...
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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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    Experimental and Numerical Investigation on the Evaporation of Shear-Driven Multicomponent Liquid Wall Films 

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003:;page 580
    Author(s): M. Gerendas; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: for the calculations of the multicomponent evaporation were implemented in a well tested elliptic finite-volume code GAP-2D (S. Wittig et al., 1992, “Motion and Evaporation of Shear-Driven Liquid Films in Turbulent Gas,” ASME J. Eng...
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    The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow 

    Source: Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001:;page 126
    Author(s): V. Scherer; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Convective heat transfer is examined in two typical examples of separated flows, namely, the flow over a backward-facing step and a two-dimensional jet entering a crossflow. Local Nusselt numbers ...
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    Discharge Coefficients of Rotating Short Orifices With Radiused and Chamfered Inlets 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 004:;page 803
    Author(s): M. Dittmann; K. Dullenkopf; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The secondary air system of modern gas turbine engines consists of numerous stationary or rotating passages to transport the cooling air, taken from the compressor, to thermally high loaded ...
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    Direct-Transfer Preswirl System: A One-Dimensional Modular Characterization of the Flow 

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 002:;page 383
    Author(s): M. Dittmann; K. Dullenkopf; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In high-efficiency gas turbine engines, the cooling air for the high-pressure turbine stage is expanded through stationary preswirl nozzles, transferred through the preswirl chamber, and delivered ...
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