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    More on the Turbulent-Strip Theory for Wake-Induced Transition 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003:;page 428
    Author(s): R. E. Mayle; K. Dullenkopf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory for transition from laminar to turbulent flow with an unsteady, periodic passing of turbulent wakes in the free stream has recently been presented by the authors. The theory considers ...
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    A Theory for Wake-Induced Transition 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 188
    Author(s): R. E. Mayle; K. Dullenkopf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theory for transition from laminar to turbulent flow as the result of unsteady, periodic passing of turbulent wakes in the free stream is developed using Emmons’ transition model. Comparisons ...
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    Discussion: “Studies on Wake-Affected Heat Transfer Around the Circular Leading Edge of Blunt Body” (Funazaki, K., 1996, ASME J. Turbomach., 118, pp. 452–460) 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 460
    Author(s): R. E. Mayle; K. Dullenkopf
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Effects of Incident Turbulence and Moving Wakes on Laminar Heat Transfer in Gas Turbines 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001:;page 23
    Author(s): K. Dullenkopf; R. E. Mayle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of free-stream turbulence and moving wakes on augmenting heat transfer in accelerating laminar boundary layers is considered. First, the effect of free-stream turbulence is re-examined ...
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    Darryl E. Metzger Memorial Session Paper: An Account of Free-Stream-Turbulence Length Scale on Laminar Heat Transfer 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 003:;page 401
    Author(s): K. Dullenkopf; R. E. Mayle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of length scale in free-stream turbulence is considered for heat transfer in laminar boundary layers. A model is proposed that accounts for an “effective” intensity of turbulence ...
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    Discussion: “Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion” (Funazaki, K., 1996, ASME J. Turbomach., 118, pp. 337–344) 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 345
    Author(s): R. E. Mayle; K. Dullenkopf
    Publisher: The American Society of Mechanical Engineers (ASME)
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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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    Cooling Air Temperature Reduction in a Direct Transfer Preswirl System 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 004:;page 809
    Author(s): T. Geis; M. Dittmann; K. Dullenkopf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an experimental study of the cooling efficiency of a preswirl rotor-stator system equipped with a small number of preswirl nozzles of circular shape, located on a radius ...
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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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    The Effect of Incident Wake Conditions on the Mean Heat Transfer of an Airfoil 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003:;page 412
    Author(s): K. Dullenkopf; A. Schulz; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow phenomena of wakes shed by upstream blade rows is a well-known problem in turbomachinery, which influences blade forces, vibrations, losses, and heat transfer. With respect to the heat ...
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