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    Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 724
    Author(s): S. Ou; J. C. Han
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of film slot injection on leading edge heat transfer coefficient and film cooling effectiveness under high mainstream turbulence conditions was experimentally studied for flow across ...
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    Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 004:;page 515
    Author(s): J. C. Han; P. Zhang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study investigated the combined effects of the flow channel aspect ratio, the rib turbulator configuration, and the sharp 180-deg turn on the distributions of the local pressure ...
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    Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001:;page 123
    Author(s): J. C. Han; P. Zhang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this experimental investigation of the heat transfer characteristics of turbulent air flow in a three-pass square channel, the test section consisted of three straight square channels jointed ...
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    Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 137
    Author(s): J. C. Han; A. B. Mehendale
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments have been performed to investigate the film-cooling characteristics with steam injection through one row (7 tubes) and two rows (13 tubes) of holes, inclined at an angle of 35 deg, ...
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    Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 707
    Author(s): A. B. Mehendale; J. C. Han
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of high mainstream turbulence on leading edge film effectiveness and heat transfer coefficient was studied. High mainstream turbulence was produced by a passive grid and a jet ...
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    Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41001
    Author(s): A. Suryanarayanan; B. Ozturk; M. T. Schobeiri; J. C. Han
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film-cooling effectiveness is measured on a rotating turbine blade platform for coolant injection through discrete holes using pressure sensitive paint technique. Most of the existing literatures ...
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    Thermoelastic Fracture Mechanics for Nonhomogeneous Material Subjected to Unsteady Thermal Load 

    Source: Journal of Applied Mechanics:;2000:;volume( 067 ):;issue: 001:;page 87
    Author(s): B. L. Wang; J. C. Han; S. Y. Du
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article provides a comprehensive treatment of cracks in nonhomogeneous structural materials such as functionally graded materials. It is assumed that the material properties depend only on ...
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    Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 872
    Author(s): J. C. Han; C. P. Lee; Y. M. Zhang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of wall heat flux ratio on the local heat transfer augmentation in a square channel with two opposite in-line ribbed walls was investigated for Reynolds numbers from 15,000 to ...
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    Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 716
    Author(s): S. Ou; A. B. Mehendale; J. C. Han
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of film hole row location on leading edge film cooling effectiveness and heat transfer coefficient under high mainstream turbulence conditions was experimentally determined for flow ...
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    Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 799
    Author(s): S. V. Ekkad; J. C. Han; H. Du
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed heat transfer coefficient and film effectiveness distributions are presented on a cylindrical leading edge model using a transient liquid crystal technique. Tests were done in a low-speed ...
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