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    Local Heat Transfer Dependency on Thermal Boundary Condition in Ribbed Cooling Channel Geometries 

    Source: Journal of Heat Transfer:;2013:;volume( 135 ):;issue: 010:;page 101001
    Author(s): Cukurel, Beni; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study is geared toward quantifying the effects of imposed thermal boundary condition in cooling channel applications. In this regard, tests are conducted in a generic passage, with evenly distributed rib type ...
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    Film Cooling Extraction Effects on the Aero Thermal Characteristics of Rib Roughened Cooling Channel Flow 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21016
    Author(s): Cukurel, Beni; Selcan, Claudio; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study is geared towards quantifying the effects of film cooling holes on turbine internal cooling passages. In this regard, tests are conducted in a generic stationary model, with evenly distributed ribtype ...
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    Two Dimensional Heat Transfer Distribution of a Rotating Ribbed Channel at Different Reynolds Numbers 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 003:;page 31002
    Author(s): Mayo, Ignacio; Arts, Tony; El; Parres, Benjamin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The convective heat transfer distribution in a ribroughened rotating internal cooling channel was measured for different rotation and Reynolds numbers, representative of engine operating conditions. The test section consisted ...
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    Aerothermal Characterization of a Rotating Ribbed Channel at Engine Representative Conditions—Part II: Detailed Liquid Crystal Thermography Measurements 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010:;page 101009
    Author(s): Mayo, Ignacio; Lahalle, Aude; Gori, Gian Luca; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present twopart work deals with a detailed characterization of the flow field and heat transfer distribution in a model of a rotating ribbed channel performed in a novel setup which allows test conditions at high ...
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    Aerothermal Characterization of a Rotating Ribbed Channel at Engine Representative Conditions—Part I: High Resolution Particle Image Velocimetry Measurements 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010:;page 101008
    Author(s): Mayo, Ignacio; Luca Gori, Gian; Lahalle, Aude; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present work is part of a detailed aerothermal investigation in a model of a rotating internal cooling channel performed in a novel facility setup which allows test conditions at high rotation numbers (Ro). The test ...
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    Investigation of Thermal Effect on Bypass Transition on a High-Pressure Turbine Guide Vane 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 005:;page 51006
    Author(s): Cação Ferreira, Tânia S.; Vasilakopoulos, Nikolaos; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The role of gas-to-wall temperature ratio on bypass transition along a highly loaded turbine guide vane is investigated through time-resolved heat flux measurements for different flow conditions. The tests are conducted ...
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    Optimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part I: Numerical Method 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51015
    Author(s): Verstraete, Tom; Coletti, Filippo; Bulle, Jأ©rأ©my; Vanderwielen, Timothأ©e; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This twopart paper addresses the design of a Ubend for serpentine internal cooling channels optimized for minimal pressure loss. The total pressure loss for the flow in a Ubend is a critical design parameter, as it augments ...
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    Experimental Investigation of the Flow and Heat Transfer in a Helically Corrugated Cooling Channel 

    Source: Journal of Heat Transfer:;2018:;volume( 140 ):;issue: 007:;page 71702
    Author(s): Mayo, Ignacio; Cernat, Bogdan C.; Virgilio, Marco; Pappa, Alessio; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The detailed flow field and heat transfer were experimentally investigated in a channel with a circular cross section and equipped with a helical rib of low blockage ratio. Stereoscopic particle image velocimetry (S-PIV) ...
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    Optimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part II: Experimental Validation 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51016
    Author(s): Coletti, Filippo; Verstraete, Tom; Bulle, Jأ©rأ©my; Van der Wielen, Timothأ©e; Van den Berge, Nicolas; Arts, Tony
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This twopart paper addresses the design of a Ubend for serpentine internal cooling channels optimized for minimal pressure loss. The total pressure loss for the flow in a Ubend is a critical design parameter, as it augments ...
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