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    Development of Secondary Flow and Vorticity in Curved Ducts, Cascades, and Rotors, Including Effects of Viscosity and Rotation 

    Source: Journal of Fluids Engineering:;1982:;volume( 104 ):;issue: 004:;page 505
    Author(s): M. Pouagare; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is concerned with the numerical solution of the secondary vorticity equations in curved ducts, cascades, and rotors. The classical approach of splitting the flow into primary and ...
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    Study of Three-Dimensional Viscous Flows in an Axial Compressor Cascade Including Tip Leakage Effects Using a SIMPLE-Based Algorithm 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 51
    Author(s): M. Pouagare; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A multisweep space-marching solver based on a modified version of the SIMPLE algorithm was employed to study the three-dimensional flow field through a linear cascade. Three cases were tested: ...
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    Three-Dimensional Flow Field in the Tip Region of a Compressor Rotor Passage—Part I: Mean Velocity Profiles and Annulus Wall Boundary Layer 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004:;page 760
    Author(s): B. Lakshminarayana; M. Pouagare; R. Davino
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field in the annulus wall and tip region of a compressor rotor was measured using a triaxial, hot-wire probe rotating with the rotor. The flow was surveyed across the entire passage ...
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    Three-Dimensional Flow Field in the Tip Region of a Compressor Rotor Passage—Part II: Turbulence Properties 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004:;page 772
    Author(s): B. Lakshminarayana; R. Davino; M. Pouagare
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The turbulence properties in the annulus wall region of an axial flow compressor rotor was measured using a triaxial, hot-wire probe rotating with the rotor. The flow was surveyed across the ...
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    An Experimental Study of the Compressor Rotor Blade Boundary Layer 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 364
    Author(s): M. Pouagare; J. M. Galmes; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The three-dimensional turbulent boundary layer developing on a rotor blade of an axial flow compressor was measured using a minature “x” configuration hot-wire probe. The measurements were carried ...
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