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    Improved Understanding of Blow-Down in Filament Seals 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41004
    Author(s): Gervas Franceschini; Terry V. Jones; David R. H. Gillespie
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Brush seals are used to provide flow resistance between rotating and stationary components in gas turbines. Compliant filament seals, such as brush seals, exhibit a phenomenon called blow-down, ...
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    Detailed Heat Transfer Measurements in a Model of an Integrally Cast Cooling Passage 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21002
    Author(s): Ioannis Ieronymidis; Peter T. Ireland; Robert Kingston; David R. H. Gillespie
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements of the heat transfer coefficient (htc) distributions on the internal surfaces of a novel gas turbine blade cooling configuration were carried out using a transient liquid ...
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    Enhancement of Impingement Cooling in a High Cross Flow Channel Using Shaped Impingement Cooling Holes 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21001
    Author(s): Andrew C. Chambers; Peter T. Ireland; Robert Kingston; David R. H. Gillespie
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Impingement systems are common place in many turbine cooling applications. Generally these systems consist of a target plate that is cooled by the impingement of multiple orthogonal jets. While ...
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    A Novel Transient Liquid Crystal Technique to Determine Heat Transfer Coefficient Distributions and Adiabatic Wall Temperature in a Three-Temperature Problem 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003:;page 538
    Author(s): Andrew C. Chambers; Geoffrey M. Dailey; David R. H. Gillespie; Peter T. Ireland
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transient liquid crystal techniques are widely used for experimental heat transfer measurements. In many instances it is necessary to model the heat transfer resulting from the temperature ...
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    Computational Modeling of Tip Heat Transfer to a Superscale Model of an Unshrouded Gas Turbine Blade 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31023
    Author(s): Brian M. T. Tang; Brian C. Y. Cheong; Martin L. G. Oldfield; David R. H. Gillespie; Pepe Palafox
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Control of over-tip leakage flow between turbine blade tips and the stationary shroud is one of the major challenges facing gas turbine designers today. The flow imposes large thermal loads ...
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