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    Axial Compressor Aerodesign Evolution at General Electric 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 321
    Author(s): Leroy H. Smith; Consultant
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper traces the origins of the GE Design System and how it has evolved from early methods to underlie and supplement present CFD methods, which are not themselves discussed herein. The ...
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    Discussion: “Three-Dimensional Theory of Incompressible and Inviscid Flow Through Mixed Flow Turbomachines” (Schilhansl, M. J., 1965, ASME J. Eng. Power, 87, pp. 361–372) 

    Source: Journal of Engineering for Gas Turbines and Power:;1965:;volume( 087 ):;issue: 004:;page 372
    Author(s): Leroy H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Sweep and Dihedral Effects in Axial-Flow Turbomachinery 

    Source: Journal of Fluids Engineering:;1963:;volume( 085 ):;issue: 003:;page 401
    Author(s): Leroy H. Smith; Hsuan Yeh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate method for including the effects of sweep and dihedral when designing axial-flow turbomachinery blading is presented. Blades are said to have sweep when the flow direction is not ...
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