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    Rotor Wake Generated Unsteady Aerodynamic Response of a Compressor Stator 

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004:;page 664
    Author(s): S. Fleeter; R. L. Jay; W. A. Bennett
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted to determine the fluctuating pressure distribution on a stationary vane row, with the primary source of excitation being the wakes from the upstream ...
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    Wake Induced Time-Variant Aerodynamics Including Rotor-Stator Axial Spacing Effects 

    Source: Journal of Fluids Engineering:;1981:;volume( 103 ):;issue: 001:;page 59
    Author(s): S. Fleeter; R. L. Jay; W. A. Bennett
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The overall objective of this experimental program was to quantify the effects of rotor-stator axial spacing on the fundamental time-variant aerodynamics relevant to forced response in turbomachinery. ...
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    The Time-Variant Aerodynamic Response of a Stator Row Including the Effects of Airfoil Camber 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 334
    Author(s): S. Fleeter; W. A. Bennett; R. L. Jay
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted to quantitatively determine the validity and applicability of state-of-the-art transverse gust cascade analyses. This was accomplished by obtaining fundamental ...
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    Investigation of Unsteady Flow Through a Transonic Turbine Stage: Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 91
    Author(s): M. G. Dunn; W. A. Bennett; R. A. Delaney; K. V. Rao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents time-averaged and phase-resolved measurements of the surface pressure data for the vane and blade of a transonic single-stage research turbine. The data are compared and ...
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