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    Closure to “Discussion of ‘The Effects of Wake Mixing on Compressor Aerodynamics’” (1991, ASME J. Turbomach., 113, p. 607) 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 607
    Author(s): R. P. Dring; D. A. Spear
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Effects of Wake Mixing on Compressor Aerodynamics 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 600
    Author(s): R. P. Dring; D. A. Spear
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A methodology based on wake mixing has been developed that enables more accurate predictions of compressor airfoil pressure distributions when the airfoil is operating downstream of an airfoil ...
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    1995 ASME Gas Turbine Award Paper: Development and Application of a Multistage Navier–Stokes Solver: Part I—Multistage Modeling Using Bodyforces and Deterministic Stresses 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 205
    Author(s): C. M. Rhie; A. J. Gleixner; D. A. Spear; C. J. Fischberg; R. M. Zacharias
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A multistage compressor performance analysis method based on the three-dimensional Reynolds-averaged Navier-Stokes equations is presented in this paper. This method is an average passage approach ...
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    Advanced Transonic Fan Design Procedure Based on a Navier–Stokes Method 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 002:;page 291
    Author(s): C. M. Rhie; R. M. Zacharias; D. E. Hobbs; K. P. Sarathy; B. P. Biederman; C. R. Lejambre; D. A. Spear
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fan performance analysis method based upon three-dimensional steady Navier–Stokes equations is presented in this paper. Its accuracy is established through extensive code validation effort. ...
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