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    Heat Transfer by a Square Array of Round Air Jets Impinging Perpendicular to a Flat Surface Including the Effect of Spent Air 

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 001:;page 73
    Author(s): D. M. Kercher; W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The results of an experimental investigation on the average surface heat transfer co-efficients under a perforated plate of multiple, square array, round impinging air jets are presented. Correlation ...
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    Heat Transfer and Turbulence in a Turbulated Blade Cooling Circuit 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001:;page 169
    Author(s): N. Abuaf; D. M. Kercher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerothermal performance of a typical turbine blade three-pass turbulated cooling circuit geometry was investigated in a 10X plexiglass test model. The model closely duplicated the blade’s ...
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    Darryl E. Metzger Memorial Session Paper: Experimental Heat Transfer and Friction in Channels Roughened With Angled, V-Shaped, and Discrete Ribs on Two Opposite Walls 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 20
    Author(s): M. E. Taslim; D. M. Kercher; T. Li
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental investigations have shown that the enhancement in heat transfer coefficients for air flow in a channel roughened with angled ribs is on the average higher than that roughened with ...
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    Experimental Heat Transfer Investigation of Stationary and Orthogonally Rotating Asymmetric and Symmetric Heated Smooth and Turbulated Channels 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001:;page 124
    Author(s): H. A. El-Husayni; D. M. Kercher; M. E. Taslim
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted to determine the effects of variations in wall thermal boundary conditions on local heat transfer coefficients in stationary and orthogonally rotating ...
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    An Experimental Investigation of Heat Transfer in an Orthogonally Rotating Channel Roughened With 45 deg Criss-Cross Ribs on Two Opposite Walls 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003:;page 346
    Author(s): M. E. Taslim; D. M. Kercher; L. A. Bondi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blade cooling is imperative in advanced aircraft engines. The extremely hot gases that operate within the turbine section require turbine blades to be cooled by a complex cooling circuit. ...
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    Short Duration Heat Transfer Studies at High Free-Stream Temperatures 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001:;page 156
    Author(s): D. M. Kercher; R. E. Sheer; R. M. C. So
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes short duration heat transfer measurements on a flat plate and a gas turbine nozzle airfoil at high free-stream temperatures. A shock tube generated the high-temperature and ...
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