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    Radial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approaches 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31018
    Author(s): Mark G. Turner; Steven E. Gorrell; David Car
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper shows a comparison of an unsteady simulation using turbo and an average passage simulation for a two blade row configuration consisting of a wake generator followed by a transonic ...
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    Particle Image Velocimetry Analysis on the Effect of Stator Loading on Transonic Blade-Row Interactions 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61012
    Author(s): Scott B. Reynolds; Jordi Estevadeordal; Steven E. Gorrell
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were performed to investigate interactions between a loaded stator and transonic rotor. The blade row interaction (BRI) rig was used to simulate an embedded transonic fan stage with ...
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    High-Fidelity Numerical Analysis of Per-Rev-Type Inlet Distortion Transfer in Multistage Fans—Part I: Simulations With Selected Blade Rows 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41014
    Author(s): Jixian Yao; Steven E. Gorrell; Aspi R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Demands for improved performance and operability of advanced propulsion systems require an understanding of the physics of inlet flow distortion transfer and generation and the subsequent engine ...
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    Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidelity, Time-Accurate Computational Fluid Dynamics 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11014
    Author(s): Michael G. List; Steven E. Gorrell; Mark G. Turner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The blade-row interaction (BRI) rig at the Air Force Research Laboratory, Compressor Aero Research Laboratory, has been simulated at three axial gaps between the highly loaded upstream stator ...
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    High-Fidelity Numerical Analysis of Per-Rev-Type Inlet Distortion Transfer in Multistage Fans—Part II: Entire Component Simulation and Investigation 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41015
    Author(s): Jixian Yao; Steven E. Gorrell; Aspi R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Part I of this paper validated the ability of the unsteady Reynolds-Averaged Navier-Stokes (RANS) solver PTURBO to accurately simulate distortion transfer and generation through selected blade ...
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    Stator-Rotor Interactions in a Transonic Compressor— Part 1: Effect of Blade-Row Spacing on Performance 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 328
    Author(s): Steven E. Gorrell; Theodore H. Okiishi; William W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Usually less axial spacing between the blade rows of an axial flow compressor is associated with improved efficiency. However, mass flow rate, pressure ratio, and efficiency all decreased as ...
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    Stator-Rotor Interactions in a Transonic Compressor—Part 2: Description of a Loss-Producing Mechanism 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 336
    Author(s): Steven E. Gorrell; Theodore H. Okiishi; William W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A previously unidentified loss producing mechanism resulting from the interaction of a transonic rotor blade row with an upstream stator blade row is described. This additional loss occurs only ...
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    An Investigation of Wake-Shock Interactions in a Transonic Compressor With Digital Particle Image Velocimetry and Time-Accurate Computational Fluid Dynamics 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 004:;page 616
    Author(s): Steven E. Gorrell; Jordi Estevadeordal; Theodore H. Okiishi; David Car; Steven L. Puterbaugh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of varying axial gap on the unsteady flow field between the stator and rotor of a transonic compressor stage are important because they can result in significant changes in stage ...
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