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    Effect of Free-Stream Turbulence on Flat-Plate Heat Flux Signals: Spectra and Eddy Transport Velocities 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 461
    Author(s): R. W. Moss; M. L. G. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of the eddy structure in a flat-plate turbulent boundary layer with significant levels of free-stream turbulence is presented. This is relevant to the enhancement of ...
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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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    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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    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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