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    Separated Flow in a Low-Speed Two-Dimensional Cascade: Part I—Flow Visualization and Time-Mean Velocity Measurements 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 409
    Author(s): A. M. Yocum; W. F. O’Brien
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study was conducted for the purpose of providing a more fundamental understanding of separated flow in cascades and to provide performance data for fully stalled blade rows. Cascades of ...
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    Sensitivity Analysis and Optimum Design Method for Reduced Rotor-Stator-Strut Flow Interaction 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 004:;page 401
    Author(s): G. Cerri; W. F. O’Brien
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A potential flow model based on the Douglas–Neumann formulation that can handle interaction problems has been used to analyze the pressure distribution produced by a stator-strut system at the ...
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    Separated Flow in a Low-Speed Two-Dimensional Cascade: Part II—Cascade Performance 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 421
    Author(s): A. M. Yocum; W. F. O’Brien
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study was conducted for the purpose of providing a more fundamental understanding of separated flow in cascades and to provide performance data for fully stalled blade rows. Cascades of ...
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    An Empirically Based Simulation Model for Heavy-Duty Gas Turbine Engines Using Treated Residual Fuel 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001:;page 167
    Author(s): J. C. Blanton; W. F. O’Brien
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An empirically based engine simulation model was developed to analyze the operation of a heavy-duty gas turbine on ash-bearing fuel. The effect of the ash in the combustion products on turbine ...
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    Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 003:;page 386
    Author(s): D. C. Rabe; W. F. O’Brien; A. J. Wennerstrom
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The passage shock wave–endwall boundary layer interaction in a transonic compressor was investigated with a laser transit anemometer. The transonic compressor used in this investigation was developed ...
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    A Shock Loss Model for Supersonic Compressor Cascades 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 001:;page 28
    Author(s): G. S. Bloch; W. F. O’Brien; W. W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Loss models used in compression system performance prediction codes are often developed from the study of two-dimensional cascades. In this paper, compressible fluid mechanics has been applied ...
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