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    Automatic Simulation of a Sequence of Hot-Former Forging Processes by a Rigid-Thermoviscoplastic Finite Element Method 

    Source: Journal of Engineering Materials and Technology:;1998:;volume( 120 ):;issue: 004:;page 291
    Author(s): M. S. Joun; H. K. Moon; Rajiv Shivpuri
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fully automatic forging simulation technique in hot-former forging is presented in this paper. A rigid-thermoviscoplastic finite element method is employed together with automatic simulation ...
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    Heat Transfer in the Tip Region of Grooved Turbine Blades 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 002:;page 131
    Author(s): M. K. Chyu; H. K. Moon; D. E. Metzger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Local convective heat transfer at the tip region of grooved blades is experimentally investigated. The present study models the problem by flow over a shrouded, rectangular cavity, with the ...
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    Heat Transfer Enhancement Using a Convex-Patterned Surface 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 274
    Author(s): H. K. Moon; T. O’Connell; R. Sharma
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The heat transfer rate from a smooth wall in an internal cooling passage can be significantly enhanced by using a convex patterned surface on the opposite wall of the passage. This design ...
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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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    The Effects of Freestream Turbulence, Turbulence Length Scale, and Exit Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11030
    Author(s): J. S. Carullo; K. A. Thole; L. J. Zhang; H. K. Moon; S. Nasir; R. D. Cress; W. F. Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper experimentally investigates the effect of high freestream turbulence intensity, turbulence length scale, and exit Reynolds number on the surface heat transfer distribution of a turbine ...
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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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