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    Discussion: “Calculation Procedures for Potential and Viscous Flow Solutions for Engine Inlets” (Albers, J. A., and Stockman, N. O., 1975, ASME J. Eng. Power, 97, pp. 1–8) 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001:;page 9
    Author(s): U. W. Schaub
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Effect of Rotor Design Tip Speed on Aerodynamic Performance of a Model VTOL Lift Fan Under Static and Crossflow Conditions” (Stockman, N. O., Loeffler, I. S., and Liebein, S., 1973, ASME J. Eng. Power, 95, pp. 293–300) 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 003:;page 322
    Author(s): U. W. Schaub
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Turbulent Wakes in Pressure Gradients 

    Source: Journal of Applied Mechanics:;1963:;volume( 030 ):;issue: 004:;page 518
    Author(s): P. G. Hill; U. W. Schaub; Y. Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The application of moderate pressure gradients can exercise a large influence on the decay of wakes produced by obstructions in a flow field. In fact, a positive pressure gradient may arrest ...
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    An Experimental Assessment of the Influence of Downstream Conditions on the Performance of a Transonic Turbine Nozzle of High Turning 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 286
    Author(s): U. W. Schaub; J.-P. Huot; S. H. Moustapha; R. G. Williamson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present work was conducted to extend information derived in a previous study where it was found that the performance of a transonic turbine nozzle of high turning angle was significantly ...
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