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    Discussion: “New Skin Friction and Entrainment Correlations for Turbulent Boundary Layers” (Ferziger, J. H., Lyrio, A. A., and Bardina, J. G., 1982, ASME J. Fluids Eng., 104, pp. 537–540) 

    Source: Journal of Fluids Engineering:;1982:;volume( 104 ):;issue: 004:;page 540
    Author(s): H. L. Moses
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Turbulent Boundary Layers in Diffusers Exhibiting Partial Stall 

    Source: Journal of Fluids Engineering:;1967:;volume( 089 ):;issue: 003:;page 655
    Author(s): H. L. Moses; J. R. Chappell
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An investigation of turbulent boundary-layer separation in internal flow is presented, with experimental results for a variable angle, two-dimensional diffuser. A simple analytical model is adopted, ...
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    Response of a Fluidic Air Gauge 

    Source: Journal of Fluids Engineering:;1969:;volume( 091 ):;issue: 003:;page 475
    Author(s): H. L. Moses; D. A. Small; G. A. Cotta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The response of the back pressure signal resulting from nozzle flow suddenly restricted by a downstream surface is described. Experimental results are presented for the periodic signal from a ...
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    Recent Advances in Simulating Unsteady Flow Phenomena Brought About by Passage of Shock Waves in a Linear Turbine Cascade 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004:;page 687
    Author(s): J. C. Collie; B. A. Gregory; H. L. Moses; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-pressure-ratio turbines have flows dominated by shock structures that pass downstream into the next blade row in an unsteady fashion. Recent numerical results have indicated that these ...
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    A Statistical Approach to the Experimental Evaluation of Transonic Turbine Airfoils in a Linear Cascade 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 366
    Author(s): M. L. Shelton; R. L. Doughty; T. Kiss; B. A. Gregory; H. L. Moses
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In aircraft engine design (and in other applications), small improvements in turbine efficiency may be significant. Since analytical tools for predicting transonic turbine losses are still being ...
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