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    Method for Determining Adiabatic Film Effectiveness in Presence of Thermal Boundary Layer 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 005:;page 51010-1
    Author(s): Parker, James; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we present a new method for determining adiabatic film effectiveness in film cooling experiments with nonuniform inlet temperature distributions, in particular the situation of an inlet thermal boundary ...
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    Impact of Temperature Ratio on Overall Cooling Performance: Low-Order-Model-Based Analysis of Experiment Design 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 009:;page 91006-1
    Author(s): Naidu, Aravin Dass; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes low-order-model-based analysis of the design of an experiment to be used for parametric studies of adiabatic film and overall cooling effectiveness for fully cooled systems (internal and film) under ...
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    Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 001:;page 11008-1
    Author(s): Cartlidge, James; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper we study the relationship between overall cooling effectiveness (or so-called metal effectiveness) and mainstream-to-coolant total temperature ratio (TR), for typical high-pressure nozzle guide vane (HPNGV) ...
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    Method for Accurately Evaluating Flow Capacity of Individual Film-Cooling Rows of Engine Components 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 011:;page 111004
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A laboratory experimental method and an analysis technique are presented for evaluation of individual film-cooling row flow capacity characteristics. The method is particularly suited to complex systems such as hot section ...
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    Cooling Optimization Theory—Part II: Optimum Internal Heat Transfer Coefficient Distribution 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 008:;page 81003
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine cooling system design is constrained by a maximum allowable wall temperature (dictated by the material, the life requirements of the component, and a given stress distribution), the desire to minimize coolant ...
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    Cooling Optimization Theory—Part I: Optimum Wall Temperature, Coolant Exit Temperature, and the Effect of Wall/Film Properties on Performance 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 008:;page 81002
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine cooling system design is constrained by a maximum allowable wall temperature (dictated by the material and the life requirements of the component), minimum coolant mass flow rate (the requirement to minimize ...
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    Reverse Pass Cooling Systems for Improved Performance 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 011:;page 111004
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Total heat transfer between a hot and a cold stream of gas across a nonporous conductive wall is greatest when the two streams flow in opposite directions. This countercurrent arrangement outperforms the cocurrent arrangement ...
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    Exploitation of Acoustic Effects in Film Cooling 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 010:;page 102602
    Author(s): Collins, Matthew; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There have been numerous studies of the behavior of shaped film cooling holes for turbine applications. It is known that the introduction of coolant is an unsteady process, and a handful of studies have described and ...
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    An Energy Based Method for Predicting the Additive Effect of Multiple Film Cooling Rows 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 012:;page 122607
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There have been numerous studies reporting film effectiveness for film rows in isolation, which have led to correlations that are used for preliminary design. Many applications require multiple film cooling rows. Although ...
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    Laboratory Infrared Thermal Assessment of Laser-Sintered High-Pressure Nozzle Guide Vanes to Derisk Engine Design Programs 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 004:;page 41009
    Author(s): Kirollos, Benjamin; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The continuing maturation of metal laser-sintering technology (direct metal laser sintering (DMLS)) presents the opportunity to derisk the engine design process by experimentally down-selecting high-pressure nozzle guide ...
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