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    Measurement and Modeling of the Gas Turbine Blade Transition Process as Disturbed by Wakes 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003:;page 315
    Author(s): J. E. LaGraff; D. A. Ashworth; D. L. Schultz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer measurements have been made on a transonic turbine blade undergoing natural transition and with a simulation of the effect of NGV wake interactions. The use of wide bandwidth ...
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    Unsteady Interaction Effects on a Transitional Turbine Blade Boundary Layer 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 002:;page 162
    Author(s): D. A. Ashworth; J. E. LaGraff; D. L. Schultz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results are presented illustrating the detailed behavior of the suction surface boundary layer of a transonic gas turbine rotor in a two-dimensional cascade under the influence of both free-stream ...
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    Unsteady Aerodynamic and Heat Transfer Processes in a Transonic Turbine Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004:;page 1022
    Author(s): D. A. Ashworth; J. E. LaGraff; D. L. Schultz; K. J. Grindrod
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of the interaction of the wake from a nozzle guide vane with the rotor may be simulated in part by means of a stationary rotor and a moving wake system. This technique is applied ...
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