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    Discussion: “Casing Wall Boundary-Layer Development Through an Isolated Compressor Rotor” (Hunter, I. H., and Cumpsty, N. A., 1982, ASME J. Eng. Power, 104, pp. 805–817) 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004:;page 817
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Some Comments on Reynolds Number 

    Source: Journal of Engineering for Gas Turbines and Power:;1964:;volume( 086 ):;issue: 003:;page 225
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The physical laws that govern fluid motions are examined to gain justification for the grouping of physical variables that we call Reynolds number. First, a perfect incompressible viscous fluid ...
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    M. J. Hartmann Memorial Session Paper: NASA/GE Fan and Compressor Research Accomplishments 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 555
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fan and compressor research projects carried out at GE Aircraft Engines under NASA sponsorship are described in this paper. Four 1400-fps-tip-speed rotors designed with different airfoil shapes ...
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    Wake Dispersion in Turbomachines 

    Source: Journal of Fluids Engineering:;1966:;volume( 088 ):;issue: 003:;page 688
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The motion of a wake as it passes through a blade row that moves relative to the wake generator is considered. Viscosity is neglected, and it is shown that the wake is modified by a ...
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    Unducted Fan Aerodynamic Design 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 313
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method being used to design unducted fans, which are counterrotating propellers with unusually high disk loadings, is described. The quasi-three-dimensional approach employed is similar to that ...
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    Discussion: “An Asymptotic Analysis of Mixing Loss” (Fritsch, G., and Giles, M. B., 1995, ASME J. Turbomach., 117, pp. 367–374) 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 003:;page 374
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Leading Edge Separation Bubbles on Turbomachine Blades” (Walraevens, R. E., and Cumpsty, N. A., 1995, ASME J. Turbomach., 117, pp. 115–125) 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 125
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “The Role of Tip Clearance in High-Speed Fan Stall” (Adamczyk, J. J., Celestina, M. L., and Greitzer, E. M., 1993, ASME J. Turbomach., 115, pp. 28–38) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 39
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Performance of Compressor Blade Rows in a Sloping Flowpath” (Harmon, H. A., Mikolajczak, A. A., and Marchant, D., 1972, ASME J. Eng. Power, 94, pp. 61–68) 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 001:;page 68
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Radial-Equilibrium Equation of Turbomachinery 

    Source: Journal of Engineering for Gas Turbines and Power:;1966:;volume( 088 ):;issue: 001:;page 1
    Author(s): L. H. Smith
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An equation is derived that describes the radial variation of circumferential-average flow properties inside of a turbomachine blade row. A physical interpretation is given for each of the several ...
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