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    Reconsideration of the Annulus Flow Problem in Axial Turbomachinery 

    Source: Journal of Fluids Engineering:;1962:;volume( 084 ):;issue: 004:;page 579
    Author(s): G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The theory pertaining to the annulus flow problem in axial turbomachinery is reviewed and a simplified analysis which is essentially concerned with the effect of streamline curvature is worked ...
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    Discussion: “On Vortex Wind Power” (So, Ronald M. C., 1978, ASME J. Fluids Eng., 100, pp. 79–82) 

    Source: Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 002:;page 250
    Author(s): G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Erratum: “An Analysis of Axial Compressor Cascade Aerodynamics: Parts I and II” (Journal of Basic Engineering, 1959, 81, pp. 362–378 and pp. 379–386) 

    Source: Journal of Fluids Engineering:;1962:;volume( 084 ):;issue: 004:;page 619
    Author(s): G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A General Solution to the Laminar Flow in Wakes 

    Source: Journal of Applied Mechanics:;1962:;volume( 029 ):;issue: 003:;page 589
    Author(s): G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Incidence and Deviation-Angle Correlations for Compressor Cascades” (Lieblein, Seymour, 1960, ASME J. Basic Eng., 82, pp. 575–584) 

    Source: Journal of Fluids Engineering:;1960:;volume( 082 ):;issue: 003:;page 584
    Author(s): G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Generalized Multistage Axial Compressor Characteristics 

    Source: Journal of Fluids Engineering:;1961:;volume( 083 ):;issue: 004:;page 709
    Author(s): G. L. Mellor; T. Root
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Presented below is a method of calculating the off-design performance of multistage axial compressor characteristics that differs in concept from previous methods. A set of resulting calculations ...
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    The Simulation of Axial Compressor Performance Using an Annulus Wall Boundary Layer Theory 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 003:;page 305
    Author(s): T. F. Balsa; G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes the development of a computer program to simulate axial compressor performance. The program incorporates a well-established technique for cascade performance prediction and a ...
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    Numerical Solution of Two-Dimensional Turbulent Separated Flows Using a Reynolds Stress Closure Model 

    Source: Journal of Fluids Engineering:;1985:;volume( 107 ):;issue: 004:;page 467
    Author(s): M. C. Celenligil; G. L. Mellor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbulent boundary layer separation is studied using the turbulence closure model suggested by Mellor and Yamada. An explicit central finite-differencing scheme is used to solve the governing ...
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    An Axial Compressor End-Wall Boundary Layer Theory 

    Source: Journal of Fluids Engineering:;1971:;volume( 093 ):;issue: 002:;page 300
    Author(s): G. L. Mellor; G. M. Wood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The essential ingredient missing in existing prediction methods for the performance of multistage axial compressors is that which would account for the effect of end-wall boundary layers. It is, ...
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