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    Heat Transfer Measurements in an Annular Cascade of Transonic Gas Turbine Blades Using the Transient Liquid Crystal Technique 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 003:;page 425
    Author(s): R. F. Martinez-Botas; G. D. Lock; T. V. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer measurements have been made in the Oxford University Cold Heat Transfer Tunnel employing the transient liquid crystal technique. Complete contours of the heat transfer coefficient ...
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    Large-Scale Testing to Validate the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003:;page 593
    Author(s): D. A. Rowbury; M. L. G. Oldfield; G. D. Lock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses large-scale, low-speed experiments that explain unexpected flow-interaction phenomena witnessed during annular cascade studies into the influence of external crossflow on film ...
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    A Method for Correlating the Influence of External Crossflow on the Discharge Coefficients of Film Cooling Holes 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 258
    Author(s): D. A. Rowbury; M. L. G. Oldfield; G. D. Lock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An empirical means of predicting the discharge coefficients of film cooling holes in an operating engine has been developed. The method quantifies the influence of the major dimensionless ...
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    Effect of Radial Location of Nozzles on Heat Transfer in Preswirl Cooling Systems 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002:;page 21023
    Author(s): V. U. Kakade; G. D. Lock; M. Wilson; J. M. Owen; J. E. Mayhew
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper investigates heat transfer in a rotating disk system using preswirled cooling air from nozzles at high and low radius. The experiments were conducted over a range of rotational ...
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    Aerothermal Investigation of Tip Leakage Flow in a Film Cooled Industrial Turbine Rotor 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21016
    Author(s): S. K. Krishnababu; G. D. Booth; G. D. Lock; W. N. Dawes; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A numerical investigation of the flow and heat transfer characteristics of tip leakage in a typical film cooled industrial gas turbine rotor is presented in this paper. The computations were ...
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    Computational Prediction of Heat Transfer to Gas Turbine Nozzle Guide Vanes With Roughened Surfaces 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 343
    Author(s): S. M. Guo; G. D. Lock; S. N. Dancer; T. V. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The local Mach number and heat transfer coefficient over the aerofoil surfaces and endwalls of a transonic gas turbine nozzle guide vane have been calculated. The computations were performed ...
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    Free Vortex Theory for Efficiency Calculations From Annular Cascade Data 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002:;page 247
    Author(s): A. J. Main; M. L. G. Oldfield; G. D. Lock; T. V. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a new three-dimensional theory to calculate the efficiency or loss of nozzle guide vane annular cascades from experimental area traverse measurements of the compressible ...
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    The Influence of Film Cooling on the Efficiency of an Annular Nozzle Guide Vane Cascade 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 001:;page 145
    Author(s): C. R. B. Day; G. D. Lock; M. L. G. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper examines the effect of aerofoil surface film cooling on the aerodynamic efficiency of an annular cascade of transonic nozzle guide vanes. A dense foreign gas (SF6 /Ar mixture) is ...
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    A Converging Slot-Hole Film-Cooling Geometry—Part 1: Low-Speed Flat-Plate Heat Transfer and Loss 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 453
    Author(s): J. E. Sargison; S. M. Guo; G. D. Lock; A. J. Rawlinson; M. L. G. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents experimental measurements of the performance of a new film-cooling hole geometry—the converging slot-hole or console. This novel, patented geometry has been designed to improve ...
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    A Converging Slot-Hole Film-Cooling Geometry—Part 2: Transonic Nozzle Guide Vane Heat Transfer and Loss 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 461
    Author(s): J. E. Sargison; S. M. Guo; G. D. Lock; A. J. Rawlinson; M. L. G. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first experimental measurements on an engine representative nozzle guide vane, of a new film-cooling hole geometry, a converging slot-hole or console. The patented console ...
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