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    Film Cooling on Highly Loaded Blades With Main Flow Separation—Part II: Overall Film Cooling Effectiveness 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11044
    Author(s): Gomes, Reinaldo A.; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling experiments were run at the high speed cascade wind tunnel of the University of the Federal Armed Forces Munich. The investigations were carried out with a linear cascade of highly loaded turbine blades. The ...
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    Film Cooling on Highly Loaded Blades With Main Flow Separation—Part I: Heat Transfer 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11043
    Author(s): Gomes, Reinaldo A.; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling experiments were run at the high speed cascade wind tunnel of the University of the Federal Armed Forces Munich. The investigations were carried out with a linear cascade of highly loaded turbine blades. The ...
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    Effects of Periodic Unsteady Inflow on Film Cooling and Heat Transfer on Highly Loaded High Pressure Turbine Blades With Flow Separation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 002:;page 21014
    Author(s): Gomes, Reinaldo A.; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling experiments were run at the highspeed cascade wind tunnel of the University of the Federal Armed Forces Munich. The investigations were carried out on a linear cascade of highly loaded turbine blades. The main ...
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    Hot Film Measurements on a Low Pressure Turbine Linear Cascade With Bypass Transition 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 009:;page 91007
    Author(s): Gomes, Reinaldo A.; Stotz, Stephan; Blaim, Franz; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transition of the state of the boundary layer from laminar to turbulent plays an important role in the aerodynamic loss generation on turbine airfoils. An accurate simulation of the transition process and of the state of ...
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