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    The Aerodynamic and Mechanical Performance of a High-Pressure Turbine Stage in a Transient Wind Tunnel 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 132
    Author(s): A. G. Sheard; R. W. Ainsworth
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new transient facility for the study of time mean and unsteady aerodynamics and heat transfer in a high-pressure turbine has been commissioned and results are available. A detailed study has ...
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    Effects of Rotation on Blade Surface Heat Transfer: An Experimental Investigation 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 530
    Author(s): R. W. Moss; R. W. Ainsworth; T. Garside
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements of turbine blade surface heat transfer in a transient rotor facility are compared with predictions and equivalent cascade data. The rotating measurements involved both forward and ...
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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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    The Use of Semi-Conductor Sensors for Blade Surface Pressure Measurement in a Model Turbine Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 002:;page 261
    Author(s): R. W. Ainsworth; T. A. Nunn; A. J. Dietz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The development of semi-conductor sensors particularly aimed at gas turbine technology applications is outlined. Methods of manufacture and means of utilizing some of the inherent advantages of ...
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    Time-Resolved Vane-Rotor Interaction in a High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 1
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; C. K. Horwood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the time-varying aerodynamic interaction mechanisms that have been observed within a transonic high-pressure turbine stage; these are inferred from the time-resolved behavior ...
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    Surface Heat Transfer Fluctuations on a Turbine Rotor Blade Due to Upstream Shock Wave Passing 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 002:;page 105
    Author(s): A. B. Johnson; M. J. Oliver; M. J. Rigby; M. L. G. Oldfield; R. W. Ainsworth
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theoretical model to explain observed rapid large-scale surface heat transfer rate fluctuations associated with the impingement of nozzle guide vane trailing edge shock waves on a transonic ...
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    Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part I: Vane-Rotor and Rotor-Vane Interaction 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 33
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; N. W. Harvey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The composition of the time-resolved surface pressure field around a high-pressure rotor blade caused by the presence of neighboring blade rows is investigated, with the individual effects of ...
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    Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part II: Vane-Vane Interaction and Discussion of Results 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 40
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; N. W. Harvey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The composition of the time-resolved surface pressure field around a high-pressure rotor blade caused by the presence of neighboring blade rows is investigated with the individual effects of ...
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    An Axial Turbobrake 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002:;page 419
    Author(s): M. I. Goodisman; R. C. Kingcombe; T. V. Jones; A. J. Brooks; R. W. Ainsworth; M. L. G. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The “Axial Turbobrake” (patent applied for) is a novel turbomachine that can be used to absorb power generated by test turbines. Unlike a compressor, there is no pressure recovery through the ...
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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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