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    Bend Geometries in Internal Cooling Channels for Improved Thermal Performance 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31028
    Author(s): Saha, Krishnendu; Acharya, Sumanta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The pressure drop and heat transfer in a two pass internal cooling channel with two different bend geometries is experimentally studied with the goal of improving the thermal performance factor (TPF) in the coolant channel. ...
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    Effect of Bend Geometry on Heat Transfer and Pressure Drop in a Two Pass Coolant Square Channel for a Turbine 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21035
    Author(s): Saha, Krishnendu; Acharya, Sumanta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a comparative numerical study of turbulent flow inside a twopass internal cooling channel with different bend geometries. The goal is to find a geometry that reduces the bend related pressure loss and ...
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    Heat Transfer Enhancement Using Angled Grooves as Turbulence Promoters 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 008:;page 81004
    Author(s): Saha, Krishnendu; Acharya, Sumanta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study is conducted on a simulated internal cooling channel of a turbine airfoil using angled grooves and combination of groovesribs to enhance the heat transfer from the wall. The grooves are angled at 45 ...
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    Heat Transfer Enhancement and Thermal Performance of Lattice Structures for Internal Cooling of Airfoil Trailing Edges 

    Source: Journal of Thermal Science and Engineering Applications:;2013:;volume( 005 ):;issue: 001:;page 11001
    Author(s): Saha, Krishnendu; Acharya, Sumanta; Nakamata, Chiyuki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the detailed heat transfer coefficient and pressure drop through two different lattice structures suitable for use in the trailing edge of gas turbine airfoil. The lattice structures are located in the ...
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