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    Miniature Single-Disk Viscous Pump (Single-DVP), Performance Characterization 

    Source: Journal of Fluids Engineering:;2006:;volume( 128 ):;issue: 003:;page 602
    Author(s): Danny Blanchard; Phil Ligrani; Bruce Gale
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The development and testing of a rotating single-disk viscous pump are described. This pump consists of a 10.16mm diameter spinning disk, and a pump chamber, which are separated by a small ...
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    Performance and Development of a Miniature Rotary Shaft Pump 

    Source: Journal of Fluids Engineering:;2005:;volume( 127 ):;issue: 004:;page 752
    Author(s): Danny Blanchard; Phil Ligrani; Bruce Gale
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The development and performance of a novel miniature pump called the rotary shaft pump (RSP) is described. The impeller is made by boring a 1.168 mm hole in one end of a 2.38 mm dia shaft ...
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    Confined, Milliscale Unsteady Laminar Impinging Slot Jets: Effects of Slot Width on Surface Stagnation Point Nusselt Numbers 

    Source: Journal of Electronic Packaging:;2012:;volume( 134 ):;issue: 004:;page 41004
    Author(s): Dae Hee Lee; Jong Ryeol Bae; Mira Ryu; Phil Ligrani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of slot width for confined, laminar impinging slot jets of millimeter-scale are considered, including experimental measurements of spatially resolved distributions of local Nusselt ...
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    Suction-Side Gill Region Film Cooling: Effects of Hole Shape and Orientation on Adiabatic Effectiveness and Heat Transfer Coefficient 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31022
    Author(s): Justin Chappell; Phil Ligrani; Sri Sreekanth; Terry Lucas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The performance of suction-side gill region film cooling is investigated using the University of Utah transonic wind tunnel and a simulated turbine vane in a two-dimensional cascade. The effects ...
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    Full-Coverage Film Cooling: Film Effectiveness and Heat Transfer Coefficients for Dense and Sparse Hole Arrays at Different Blowing Ratios 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61039
    Author(s): Phil Ligrani; Mike Fox; Hee-Koo Moon; Matt Goodro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results are presented for a full coverage film cooling arrangement which simulates a portion of a gas turbine engine, with appropriate streamwise static pressure gradient and varying ...
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    Aerodynamic Performance of Suction-Side Gill Region Film Cooling 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31020
    Author(s): Justin Chappell; Phil Ligrani; Sri Sreekanth; Terry Lucas; Edward Vlasic
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The performance of suction-side gill region film cooling is investigated using the University of Utah transonic wind tunnel and a simulated turbine vane in a two-dimensional cascade. The effects ...
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    Instabilities of Nonreturn Valves in Low-Speed Air Systems 

    Source: Journal of Fluids Engineering:;2008:;volume( 130 ):;issue: 012:;page 121105
    Author(s): Mark Potter; Matthew Plackett; Marko Bacic; Phil Ligrani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Practical observations of the nonreturn valve wear in aero-engine cabin-bleed systems suggest that such valves are subject to unstable behavior. A theoretical model for the prediction of nonreturn ...
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    Separate Effects of Mach Number and Reynolds Number on Jet Array Impingement Heat Transfer 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002:;page 269
    Author(s): Jongmyung Park; Phil Ligrani; Mike Fox; Hee-Koo Moon; Matt Goodro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Limited available data suggest a substantial impact of Mach number on the heat transfer from an array of jets impinging on a surface at fixed Reynolds number. Many jet array heat transfer ...
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    Effect of Temperature Ratio on Jet Array Impingement Heat Transfer 

    Source: Journal of Heat Transfer:;2009:;volume( 131 ):;issue: 001:;page 12201
    Author(s): Matt Goodro; Jongmyung Park; Phil Ligrani; Mike Fox; Hee-Koo Moon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper consider the effects of temperature ratio on the heat transfer from an array of jets impinging on a flat plate. At a constant Reynolds number of 18,000 and a constant Mach number ...
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