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    The Dynamics of the Horseshoe Vortex and Associated Endwall Heat Transfer—Part II: Time-Mean Results 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 004:;page 755
    Author(s): T. J. Praisner; C. R. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Time-mean endwall heat transfer and flow-field data in the endwall region are presented for a turbulent juncture flow formed with a symmetric bluff body. The experimental technique employed ...
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    Predicting Transition in Turbomachinery—Part I: A Review and New Model Development 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 1
    Author(s): T. J. Praisner; J. P. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Here we report on an effort to include an empirically based transition modeling capability in a Reynolds Averaged Navier-Stokes solver. Well known empirical models for both attached- and ...
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    The Dynamics of the Horseshoe Vortex and Associated Endwall Heat Transfer—Part I: Temporal Behavior 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 004:;page 747
    Author(s): T. J. Praisner; C. R. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Instantaneous flow topology and the associated endwall heat transfer in the leading-edge endwall region of a symmetric airfoil are presented. An experimental technique was employed that allowed ...
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    Measurements of Losses and Reynolds Stresses in the Secondary Flow Downstream of a Low-Speed Linear Turbine Cascade 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61015
    Author(s): G. D. MacIsaac; T. J. Praisner; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental measurements of the mean and turbulent flow field were preformed downstream of a low-speed linear turbine cascade. The influence of turbulence on the production of secondary losses ...
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    Effects of an Upstream Cavity on the Secondary Flow in a Transonic Turbine Cascade 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51009
    Author(s): H. M. Abo El Ella; S. A. Sjolander; T. J. Praisner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper examines experimentally the effects of an upstream cavity on the flow structures and secondary losses in a transonic linear turbine cascade. The cavity approximates the endwall geometry ...
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    Measurements of Secondary Losses in a Turbine Cascade With the Implementation of Nonaxisymmetric Endwall Contouring 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11013
    Author(s): D. C. Knezevici; T. J. Praisner; E. Allen-Bradley; S. A. Sjolander; E. A. Grover
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approach to endwall contouring has been developed with the goal of reducing secondary losses in highly loaded axial flow turbines. The present paper describes an experimental assessment of ...
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    Predicting Transition in Turbomachinery—Part II: Model Validation and Benchmarking 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 14
    Author(s): T. J. Praisner; J. P. Clark; E. A. Grover; M. J. Rice
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The ability to predict boundary layer transition locations accurately on turbomachinery airfoils is critical both to evaluate aerodynamic performance and to predict local heat-transfer coefficients ...
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