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    Turbulent Separation Analysis Ahead of a Step 

    Source: Journal of Fluids Engineering:;1972:;volume( 094 ):;issue: 003:;page 544
    Author(s): D. B. Taulbee; J. M. Robertson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The general nature of the flow separation of a turbulent boundary layer ahead of an inward-projecting normal step is shown to be well predicted by a rotational flow analysis (frozen vorticity ...
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    Prediction of Unsteady Rotor-Surface Pressure and Heat Transfer From Wake Passings 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 807
    Author(s): L. T. Tran; D. B. Taulbee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The research described in this paper is a numerical investigation of the effects of unsteady flow on gas turbine heat transfer, particularly on a rotor blade surface. The unsteady flow in a ...
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    Closure to “Discussion of ‘Prediction of Unsteady Rotor-Surface Pressure and Heat Transfer From Wake Passings’” (1993, ASME J. Turbomach., 115, pp. 362–364) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 364
    Author(s): L. T. Tran; D. B. Taulbee
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Second Order Boundary Layer Solutions on a Curved Surface 

    Source: Journal of Fluids Engineering:;1972:;volume( 094 ):;issue: 003:;page 649
    Author(s): W. F. Van Tassell; D. B. Taulbee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Solutions of the second order longitudinal curvature boundary layer equations near the stagnation point of a two-dimensional circular cylinder are presented. Four cases corresponding to 1 first ...
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    Air Mixing in a Model Lung Alveolus 

    Source: Journal of Biomechanical Engineering:;1978:;volume( 100 ):;issue: 004:;page 211
    Author(s): C. P. Yu; S. Rajaram; D. B. Taulbee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The quasi-steady creeping flow in a spherical model alveolus has been studied by solving the Stokes equations numerically in order to understand the airflow in the alveolar region of the human ...
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    Stagnation Point and Surface Heat Transfer for a Turbine Stage: Prediction and Comparison With Data 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 001:;page 28
    Author(s): D. B. Taulbee; M. G. Dunn; L. Tran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Predictions using turbulence models are reported for the time-averaged heat-flux distributions on the vane and blade surfaces of the Garrett TFE 731-2 HP and Teledyne CAE 702 HP turbines. To ...
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