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    Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 12
    Author(s): Y. W. Kim; D. E. Metzger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In unshrouded axial turbine stages, a small but generally unavoidable clearance between the blade tips and the stationary outer seal allows a clearance gap leakage flow to be driven across the ...
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    Transient Liquid Crystal Technique for Convective Heat Transfer on Rough Surfaces 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 14
    Author(s): D. N. Barlow; Y. W. Kim; L. W. Florschuetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The local heat transfer coefficients are obtained on a rough planar surface simulating in-service turbine stator vane sections. A transient experimental technique is presented that permits the ...
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    Darryl E. Metzger Memorial Session Paper: A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 1
    Author(s): Y. W. Kim; J. P. Downs; W. Abdel-Messeh; G. D. Steuber; S. Tanrikut; F. O. Soechting
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The clearance gap between the stationary outer air seal and blade tips of an axial turbine allows a clearance gap leakage flow to be driven through the gap by the pressure-to-suction side ...
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