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    Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004:;page 743
    Author(s): M. F. Blair
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results from an experimental study of large-scale, two-dimensional incompressible transitional boundary layer flows are presented. Tests were conducted on a heated flat wall with a zero pressure ...
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    Boundary-Layer Transition in Accelerating Flows With Intense Freestream Turbulence: Part 1—Disturbances Upstream of Transition Onset 

    Source: Journal of Fluids Engineering:;1992:;volume( 114 ):;issue: 003:;page 313
    Author(s): M. F. Blair
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Hot-wire anemometry was employed to examine the laminar-to-turbulent transition of low-speed, two-dimensional boundary layers for two (moderate) levels of flow acceleration and various levels of ...
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    Boundary-Layer Transition in Accelerating Flows With Intense Freestream Turbulence: Part 2—The Zone of Intermittent Turbulence 

    Source: Journal of Fluids Engineering:;1992:;volume( 114 ):;issue: 003:;page 322
    Author(s): M. F. Blair
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Hot-wire anemometry was employed to examine the laminar-to-turbulent transition of low-speed, two-dimensional boundary layers for two (moderate) levels of flow acceleration and various levels of ...
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    An Experimental Study Heat Transfer in a Large-Scale Turbine Rotor Passage 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001:;page 1
    Author(s): M. F. Blair
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of the heat transfer distribution in a turbine rotor passage was conducted in a large-scale, ambient temperature, rotating turbine model. Heat transfer was measured for ...
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    The Effects of Turbulence and Stator/Rotor Interactions on Turbine Heat Transfer: Part I—Design Operating Conditions 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 001:;page 87
    Author(s): M. F. Blair; R. P. Dring; H. D. Joslyn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined experimental and analytical program was conducted to examine the effects of inlet turbulence, stator–rotor axial spacing, and relative circumferential spacing of first and second stators ...
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    The Effects of Turbulence and Stator/Rotor Interactions on Turbine Heat Transfer: Part II—Effects of Reynolds Number and Incidence 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 001:;page 97
    Author(s): M. F. Blair; R. P. Dring; H. D. Joslyn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Part I of this paper presents airfoil heat transfer data obtained in a rotating turbine model at its design rotor incidence. This portion of the paper presents heat transfer data obtained in ...
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    Development of a Large-Scale Wind Tunnel for the Simulation of Turbomachinery Airfoil Boundary Layers 

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004:;page 678
    Author(s): M. F. Blair; D. A. Bailey; R. H. Schlinker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The procedures employed for the design of a closed-circuit, boundary layer wind tunnel are described. The tunnel was designed for the generation of large-scale, two-dimensional boundary layers ...
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    An Experimental Investigation of Film Cooling on a Turbine Rotor Blade 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 001:;page 81
    Author(s): R. P. Dring; M. F. Blair; H. D. Joslyn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling has been studied on the rotor blade of a large scale (low speed) model of a high pressure turbine first stage. Film coolant was discharged from single holes on the pressure and ...
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    Effect of Streamline Curvature on Film Cooling 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001:;page 77
    Author(s): R. E. Mayle; M. F. Blair; D. A. Bailey; F. C. Kopper
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of streamline curvature on film cooling effectiveness are discussed. Experiments for air discharged through a slot and into a turbulent boundary layer along a flat, convex, and ...
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    An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 257
    Author(s): R. A. Graziani; M. F. Blair; J. R. Taylor; R. E. Mayle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Local rates of heat transfer on the endwall, suction, and pressure surfaces of a large scale turbine blade cascade were measured for two inlet boundary layer thicknesses and for a Reynolds ...
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