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    Channel Height Effect on Heat Transfer and Friction in a Dimpled Passage 

    Source: Journal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;issue: 002:;page 307
    Author(s): H. K. Moon; T. O’Connell; B. Glezer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The heat transfer enhancement in cooling passages with dimpled (concavity imprinted) surface can be effective for use in heat exchangers and various hot section components (nozzle, blade, combustor ...
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    Heat Transfer and Flow Phenomena in a Swirl Chamber Simulating Turbine Blade Internal Cooling 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 004:;page 804
    Author(s): C. R. Hedlung; H.-K. Moon; B. Glezer; P. M. Ligrani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer and fluid mechanics results are given for a swirl chamber whose geometry models an internal passage used to cool the leading edge of a turbine blade. The Reynolds numbers ...
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    Local Heat Transfer and Flow Structure on and Above a Dimpled Surface in a Channel 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 115
    Author(s): G. I. Mahmood; H.-K. Moon; Consulting Engineer; B. Glezer; Head; Turbine Cooling and Heat Transfer Analysis; M. L. Hill; D. L. Nelson; P. M. Ligrani; Professor.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results, measured on and above a dimpled test surface placed on one wall of a channel, are given for Reynolds numbers from 1250 to 61,500 and ratios of air inlet stagnation ...
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