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    Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 704
    Author(s): A. A. Ameri
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental and computational studies have been performed to investigate the detailed distribution of convective heat transfer coefficients on the first-stage blade tip surface for a geometry ...
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    Transition Modeling Effects on Turbine Rotor Blade Heat Transfer Predictions 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 307
    Author(s): A. A. Ameri; A. Arnone
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of transition modeling on the heat transfer predictions from rotating turbine blades was investigated. Three-dimensional computations using a Reynolds-averaged Navier–Stokes code were ...
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    Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 31
    Author(s): R. J. Boyle; A. A. Ameri
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of five different C-type grid geometries on the predicted heat transfer and aerodynamic performance of a turbine stator is examined. Predictions were obtained using two flow analysis ...
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    Heat Transfer and Flow on the First-Stage Blade Tip of a Power Generation Gas Turbine: Part 2—Simulation Results 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002:;page 272
    Author(s): A. A. Ameri; R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined experimental and computational study has been performed to investigate the detailed distribution of convective heat transfer coefficients on the first-stage blade tip surface for a ...
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    Effect of Squealer Tip on Rotor Heat Transfer and Efficiency 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 753
    Author(s): A. A. Ameri; E. Steinthorsson; D. L. Rigby
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Calculations were performed to simulate the tip flow and heat transfer on the GE-E3 first-stage turbine, which represents a modern gas turbine blade geometry. Cases considered were a smooth ...
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    Effects of Tip Clearance and Casing Recess on Heat Transfer and Stage Efficency in Axial Turbines 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 004:;page 683
    Author(s): A. A. Ameri; E. Steinthorsson; D. L. Rigby
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Calculations were performed to assess the effect of the tip leakage flow on the rate of heat transfer to blade, blade tip, and casing. The effect on exit angle and efficiency was also ...
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