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    Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 130
    Author(s): Vikrant Saxena; Hasan Nasir; Srinath V. Ekkad
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive investigation of the effect of various tip sealing geometries is presented on the blade tip leakage flow and associated heat transfer of a scaled up HPT turbine blade in a ...
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    Influence of Crossflow-Induced Swirl and Impingement on Heat Transfer in a Two-Pass Channel Connected by Two Rows of Holes 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 281
    Author(s): Gautam Pamula; Srinath V. Ekkad; Sumanta Acharya
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed heat transfer distributions are presented inside a two-pass coolant square channel connected by two rows of holes on the divider walls. The enhanced cooling is achieved by a combination ...
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    Effect of Jet Pulsation and Duty Cycle on Film Cooling From a Single Jet on a Leading Edge Model 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003:;page 564
    Author(s): Srinath V. Ekkad; Shichuan Ou; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of jet pulsation and duty cycle on film effectiveness and heat transfer was investigated on a film hole located on the circular leading edge of a blunt body. A transient infrared ...
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    Effect of Tip and Pressure Side Coolant Injection on Heat Transfer Distributions for a Plane and Recessed Tip 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 151
    Author(s): Hasan Nasir; Ronald S. Bunker; Srinath V. Ekkad
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study investigates the effects of coolant injection on adiabatic film effectiveness and heat transfer coefficients from a plane and recessed tip of a high pressure turbine first ...
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    A Transient Infrared Thermography Method for Simultaneous Film Cooling Effectiveness and Heat Transfer Coefficient Measurements From a Single Test 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 597
    Author(s): Srinath V. Ekkad; Shichuan Ou; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In film cooling situations, there is a need to determine both local adiabatic wall temperature and heat transfer coefficient to fully assess the local heat flux into the surface. Typical film ...
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    Film Cooling Measurements for Cratered Cylindrical Inclined Holes 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 001:;page 11005
    Author(s): Yiping Lu; Ronald S. Bunker; Alok Dhungel; Srinath V. Ekkad
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling performance is studied for cylindrical holes embedded in craters. Different crater geometries are considered for a typical crater depth. Cratered holes may occur when blades are ...
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    Effect of Trench Width and Depth on Film Cooling From Cylindrical Holes Embedded in Trenches 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 001:;page 11003
    Author(s): Yiping Lu; Ronald S. Bunker; Alok Dhungel; Srinath V. Ekkad
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study is an experimental investigation of film cooling from cylindrical holes embedded in transverse trenches. Different trench depths are considered with two trench widths. Trench ...
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    Detailed Heat Transfer Measurements Inside Rotating Ribbed Channels Using the Transient Liquid Crystal Technique 

    Source: Journal of Thermal Science and Engineering Applications:;2012:;volume( 004 ):;issue: 001:;page 11002
    Author(s): Justin A. Lamont; Mary Anne Alvin; Srinath V. Ekkad
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Coolant flow in rotating internal serpentine channels is highly complex due to the effects of the Coriolis force and centrifugal buoyancy. Detailed knowledge of the heat transfer over a surface ...
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    Effects of Rotation on Heat Transfer for a Single Row Jet Impingement Array With Crossflow 

    Source: Journal of Heat Transfer:;2012:;volume( 134 ):;issue: 008:;page 82202
    Author(s): Justin A. Lamont; Srinath V. Ekkad; Mary Anne Alvin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of the Coriolis force are investigated in rotating internal serpentine coolant channels in turbine blades. For complex flow in rotating channels, detailed measurements of the heat ...
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    Film Cooling From a Row of Holes Supplemented With Antivortex Holes 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21007
    Author(s): Alok Dhungel; Srinath V. Ekkad; James Heidmann; Yiping Lu; Wynn Phillips
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primary focus of this paper is to study the film cooling performance for a row of cylindrical holes each supplemented with two symmetrical antivortex holes, which branch out from the main ...
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