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    Discussion: “Three-Dimensional Flows and Loss Reduction in Axial Compressors” (Dong, Y., Gallimore, S. J., and Hodson, H. P., 1987, ASME J. Turbomach., 109, pp. 354–361) 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 361
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Boundary Layer Transition and Separation on a Compressor Rotor Airfoil 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 001:;page 251
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Radial Transport and Momentum Exchange in an Axial Compressor 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 477
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this work was to examine radial transport in axial compressors from two perspectives. The first was to compare the mixing coefficient based on a secondary flow model (using ...
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    Radial Mixing in an Axial Turbine 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 262
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this work was to examine radial mixing in an axial turbine from a number of different perspectives. These include: (1) its impact on the spanwise distributions of the force ...
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    Sizing Criteria for Laser Anemometry Particles 

    Source: Journal of Fluids Engineering:;1982:;volume( 104 ):;issue: 001:;page 15
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Three-Dimensional Boundary-Layer Computation on the Stationary End-Walls of Centrifugal Turbomachinery” (Davis, W. R., 1976, ASME J. Fluids Eng., 98, pp. 431–441) 

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003:;page 441
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Blockage in Axial Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003:;page 712
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Momentum-Integral Analysis of the Three-Dimensional Turbine End-Wall Boundary Layer 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004:;page 386
    Author(s): R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis is presented which is a combination of existing momentum-integral equations and existing studies of profile shapes for incompressible three-dimensional turbulent boundary layers. These, ...
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    Discussion: “Effects of Inlet Temperature Gradients on Turbomachinery Performance” (Lakshminarayana, B., 1975, ASME J. Eng. Power, 97, pp. 64–71) 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001:;page 71
    Author(s): R. P. Dring; M. Salita
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Through-Flow Models for Mass and Momentum-Averaged Variables 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 362
    Author(s): C. Hirsch; R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The turbomachinery through-flow equations are reformulated for mass and momentum-averaged quantities. The background of this analysis is the need for an improved assessment of the accuracy of ...
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