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    Effects of Regular and Random Roughness on the Heat Transfer and Skin Friction Coefficient on the Suction Side of a Gas Turbine Vane 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 004:;page 41012
    Author(s): Jason E. Dees; David G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Skin friction coefficients and heat transfer coefficients are measured for a range of regular and random roughnesses on the suction side of a simulated gas turbine vane. The skin friction ...
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    Heat Transfer Augmentation Downstream of Rows of Various Dimple Geometries on the Suction Side of a Gas Turbine Airfoil 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31010
    Author(s): Jason E. Dees; Ronald S. Bunker; David G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer coefficients were measured downstream of a row of shaped film cooling holes, as well as elliptical, diffuser, and teardrop shaped dimples, simulating depressions due to film coolant ...
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    Momentum and Thermal Boundary Layer Development on an Internally Cooled Turbine Vane 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61004
    Author(s): Jason E. Dees; David G. Bogard; Gustavo A. Ledezma; Gregory M. Laskowski; Anil K. Tolpadi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent advances in computing power have made conjugate heat transfer simulations of turbine components increasingly popular; however, limited experimental data exist with which to evaluate these ...
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    Experimental Measurements and Computational Predictions for an Internally Cooled Simulated Turbine Vane 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61003
    Author(s): Jason E. Dees; David G. Bogard; Gustavo A. Ledezma; Gregory M. Laskowski; Anil K. Tolpadi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study the conjugate heat transfer effects for an internally cooled vane were studied experimentally and computationally. Experimentally, a large scale model vane was used with an internal ...
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    Turbine Airfoil Net Heat Flux Reduction With Cylindrical Holes Embedded in a Transverse Trench 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 001:;page 11012
    Author(s): Katharine L. Harrison; Ronald S. Bunker; John R. Dorrington; Jason E. Dees; David G. Bogard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling adiabatic effectiveness and heat transfer coefficients for cylindrical holes embedded in a 1d transverse trench on the suction side of a simulated turbine vane were investigated to ...
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