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    The Elliptic Solution of the Secondary Flow Problem 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003:;page 530
    Author(s): S. Abdallah; A. Hamed
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the elliptic solution of the inviscid incompressible secondary flow in curved passages. The three-dimensional flow field is synthesized between 3 sets of orthogonal nonstream ...
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    Internal Three-Dimensional Viscous Flow Solution Using the Streamlike Function 

    Source: Journal of Fluids Engineering:;1986:;volume( 108 ):;issue: 003:;page 348
    Author(s): A. Hamed; S. Abdallah
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new method for the three-dimensional elliptic solution of the Navier–Stokes equations. It is based on the streamlike-function vorticity formulation which was developed by ...
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    Computation of Inviscid Incompressible Flow Using the Primitive Variable Formulation 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 68
    Author(s): S. Abdallah; H. G. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primitive variable formulation originally developed for the incompressible Navier–Stokes equations is applied for the solution of the incompressible Euler equations. The unsteady momentum equation ...
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    Three-Dimensional Solutions for Inviscid Incompressible Flow in Turbomachines 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 391
    Author(s): S. Abdallah; C. F. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A primitive variable formulation is used for the solution of the incompressible Euler equation. In particular, the pressure Poisson equation approach using a nonstaggered grid is considered. In ...
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    Improved Approach to the Streamline Curvature Method in Turbomachinery 

    Source: Journal of Fluids Engineering:;1987:;volume( 109 ):;issue: 003:;page 213
    Author(s): S. Abdallah; R. E. Henderson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Quasi three dimensional blade-to-blade solutions for stators and rotors of turbomachines are obtained using the Streamline Curvature Method (SLCM). The first-order velocity gradient equation of the ...
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    Unified Equation of Motion (UEM) Approach as Applied to S1 Turbomachinery Problems 

    Source: Journal of Fluids Engineering:;1988:;volume( 110 ):;issue: 003:;page 251
    Author(s): S. Abdallah; C. F. Smith; M. W. McBride
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Incompressible, blade-to-blade (SI surface) flow solutions for stators and rotors of turbomachines are obtained utilizing an approach which combines the equations of motion into a single elliptic, ...
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