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    Second Law Analysis of Aerodynamic Losses: Results for a Cambered Vane With and Without Film Cooling 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 004:;page 41013
    Author(s): Ligrani, Phil; Sik Jin, Jae
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results of second law analysis of experimentallymeasured aerodynamic losses are presented for a cambered vane with and without film cooling, including comparisons with similar results from a symmetric airfoil. Included are ...
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    Miniature Viscous Disk Pump: Performance Variations From Non-Newtonian Elastic Turbulence 

    Source: Journal of Fluids Engineering:;2017:;volume( 139 ):;issue: 002:;page 21104
    Author(s): Ligrani, Phil; Lund, Benjamin; Fatemi, Arshia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Within the present investigation, a miniature viscous disk pump (VDP) is utilized to characterize and quantify non-Newtonian fluid elastic turbulence effects, relative to Newtonian flow behavior. Such deviations from ...
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    Deviations Due to Non Newtonian Influences Within a Miniature Viscous Disk Pump 

    Source: Journal of Fluids Engineering:;2013:;volume( 135 ):;issue: 003:;page 31205
    Author(s): Ligrani, Phil; Jiang, Hui; Lund, Benjamin; Jin, Jae Sik
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A miniature viscous disk pump (VDP) is utilized to characterize and quantify nonNewtonian fluid deviations due to nonNewtonian influences relative to Newtonian flow behavior. Such deviations from Newtonian behavior are ...
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    Full Coverage Film Cooling: Heat Transfer Coefficients and Film Effectiveness for a Sparse Hole Array at Different Blowing Ratios and Contraction Ratios 

    Source: Journal of Heat Transfer:;2015:;volume( 137 ):;issue: 003:;page 32201
    Author(s): Ligrani, Phil; Goodro, Matt; Fox, Michael D.; Moon, Hee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present experimental investigation considers a full coverage film cooling arrangement with different streamwise static pressure gradients. The film cooling holes in adjacent streamwise rows are staggered with respect ...
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    Full Coverage Film Cooling: Film Effectiveness and Heat Transfer Coefficients for Dense Hole Arrays at Different Hole Angles, Contraction Ratios, and Blowing Ratios 

    Source: Journal of Heat Transfer:;2013:;volume( 135 ):;issue: 003:;page 31707
    Author(s): Ligrani, Phil; Goodro, Matt; Fox, Mike; Moon, Hee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results are presented for a fullcoverage film cooling arrangement which simulates a portion of a gas turbine engine, with appropriate streamwise static pressure gradient. The test surface utilizes varying ...
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    Double Wall Cooling of a Full-Coverage Effusion Plate, Including Internal Impingement Array Cooling 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 005:;page 51901
    Author(s): Ligrani, Phil; Ren, Zhong; Liberatore, Federico; Patel, Rajeshriben; Srinivasan, Ram; Ho, Yin-Hsiang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: New experimental data are provided for full-coverage effusion cooling and impingement array cooling, as applied simultaneously onto the respective external and internal surfaces of a single instrumented test plate. For the ...
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    Effects of Jet To Target Plate Distance and Reynolds Number on Jet Array Impingement Heat Transfer 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005:;page 51013
    Author(s): Lee, Junsik; Ren, Zhong; Haegele, Jacob; Potts, Geoffrey; Sik Jin, Jae; Ligrani, Phil; Fox, Michael D.; Moon, Hee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Data which illustrate the effects of jettotarget plate distance and Reynolds number on the heat transfer from an array of jets impinging on a flat plate are presented. Considered are Reynolds numbers Rej ranging from 8200 ...
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    Double Wall Cooling of a Full-Coverage Effusion Plate With Main Flow Pressure Gradient, Including Internal Impingement Array Cooling 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 004:;page 41002
    Author(s): Vanga, Sneha Reddy; Ritchie, David; Click, Austin; Ren, Zhong; Ligrani, Phil; Liberatore, Federico; Patel, Rajeshriben; Srinivasan, Ram; Ho, Yin-Hsiang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study provides new effusion cooling data for both the surfaces of the full-coverage effusion cooling plate. For the effusion-cooled surface, presented are spatially resolved distributions of surface adiabatic ...
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    Double Wall Cooling of a Full Coverage Effusion Plate With Cross Flow Supply Cooling and Main Flow Pressure Gradient 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 003:;page 31015
    Author(s): Ligrani, Phil; Ren, Zhong; Vanga, Sneha Reddy; Allgaier, Christopher; Liberatore, Federico; Patel, Rajeshriben; Srinivasan, Ram; Ho, Yin-Hsiang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimentally measured results are presented for different experimental conditions for a test plate with double wall cooling, composed of full-coverage effusion-cooling on the hot side of the plate, and cross-flow cooling ...
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    Effects of Double Wall Cooling Configuration and Conditions on Performance of Full-Coverage Effusion Cooling 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 005:;page 51009
    Author(s): Rogers, Nathan; Ren, Zhong; Buzzard, Warren; Sweeney, Brian; Tinker, Nathan; Ligrani, Phil; Hollingsworth, Keith; Liberatore, Fred; Patel, Rajeshriben; Ho, Shaun; Moon, Hee-Koo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results are presented for a double wall cooling arrangement which simulates a portion of a combustor liner of a gas turbine engine. The results are collected using a new experimental facility designed to test ...
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