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    Heat Transfer in Rotating Serpentine Passages With Selected Model Orientations for Smooth or Skewed Trip Walls 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 738
    Author(s): B. V. Johnson; G. D. Steuber; F. C. Yeh; J. H. Wagner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of model orientation as well as buoyancy and Coriolis forces on heat transfer in turbine blade internal coolant passages. Turbine blades have ...
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    Heat Transfer in Rotating Serpentine Passages With Trips Skewed to the Flow 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001:;page 113
    Author(s): B. V. Johnson; G. D. Steuber; F. C. Yeh; J. H. Wagner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of buoyancy and Coriolis forces on heat transfer in turbine blade internal coolant passages. The experiments were conducted with a large-scale, ...
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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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