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    Modeling Unsteady Transition and Its Effects on Profile Loss 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004:;page 691
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the effects of wake interactions on the transition processes of turbomachine blade boundary layers. A simple model of unsteady transition is proposed, which is then used ...
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    Discussion: “Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion” (Funazaki, K., 1996, ASME J. Turbomach., 118, pp. 337–344) 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 344
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Boundary Layer and Loss Measurements on the Rotor of an Axial-Flow Turbine 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002:;page 391
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic efficiency of an axial-flow turbine is significantly less than that predicted by measurements made on equivalent cascades which operate with steady inflow. This difference in ...
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    An Inviscid Blade-to-Blade Prediction of a Wake-Generated Unsteady Flow 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 337
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a time-marching calculation of the unsteady flow generated by the interaction of upstream wakes with a moving blade row. The inviscid equations of motion are solved using ...
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    Measurements of Wake-Generated Unsteadiness in the Rotor Passages of Axial Flow Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 467
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an investigation into the free-stream unsteadiness which is found in the rotor passages of axial flow turbines and which is caused by the interaction of the stator wakes ...
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    Boundary-Layer Transition and Separation Near the Leading Edge of a High-Speed Turbine Blade 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 127
    Author(s): H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The state of the boundary layers near the leading edge of a high-speed turbine blade has been investigated, in cascade, using an array of surface-mounted, constant-temperature, hot-film anemometers. ...
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    Unsteady Wake-Induced Boundary Layer Transition in High Lift LP Turbines 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 28
    Author(s): V. Schulte; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The development of the unsteady suction side boundary layer of a highly loaded LP turbine blade has been investigated in a rectilinear cascade experiment. Upstream rotor wakes were simulated ...
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    Prediction of the Becalmed Region for LP Turbine Profile Design 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 839
    Author(s): V. Schulte; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent attention has focused on the so-called “becalmed region” that is observed inside the boundary layers of turbomachinery blading and is associated with the process of wake-induced transition. ...
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    Measurement and Prediction of Tip Clearance Flow in Linear Turbine Cascades 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 376
    Author(s): F. J. G. Heyes; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a simple two-dimensional model for the calculation of the leakage flow over the blade tips of axial turbines. The results obtained from calculations are compared with data ...
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    Erratum: “Measurement and Prediction of Tip Clearance Flow in Linear Turbine Cascades” (Journal of Turbomachinery, 1993, 115, p. 376–382) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004:;page 698
    Author(s): F. J. G. Heyes; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
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