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    The Development of Fast Response Aerodynamic Probes for Flow Measurements in Turbomachinery 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 625
    Author(s): R. W. Ainsworth; J. L. Allen; J. J. M. Batt
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The advent of a new generation of transient rotating turbine simulation facilities, where engine values of Reynolds and Mach number are matched simultaneously together with the relevant rotational ...
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    A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 001:;page 88
    Author(s): R. M. Watt; N. C. Baines; J. P. Simons; M. George; J. L. Allen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of thermal barrier coating surface roughness on the aerodynamic performance of gas turbine aerofoils has been investigated for the case of a profile typical of current first-stage ...
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    Developments in Instrumentation and Processing for Transient Heat Transfer Measurement in a Full-Stage Model Turbine 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 001:;page 20
    Author(s): R. W. Ainsworth; J. L. Allen; M. R. D. Davies; J. E. Doorly; C. J. P. Forth; M. A. Hilditch; M. L. G. Oldfield; A. G. Sheard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transient heat transfer measurement techniques have long been used in two-dimensional stationary cascade tests designed to model turbine conditions used in Oxford. More recently, experiments studying ...
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