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    Turbine Separation Control Using Pulsed Vortex Generator Jets 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 198
    Author(s): Jeffrey P. Bons; Rolf Sondergaard; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The application of pulsed vortex generator jets to control separation on the suction surface of a low-pressure turbine blade is reported. Blade Reynolds numbers in the experimental, linear turbine ...
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    The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 001:;page 77
    Author(s): Jeffrey P. Bons; Rolf Sondergaard; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of pulsed vortex generator jets on a naturally separating low-pressure turbine boundary layer have been investigated experimentally. Blade Reynolds numbers in the linear turbine cascade ...
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    Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part II: The Application to a Highly Separated Turbine Blade Cascade Geometry 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31012
    Author(s): Darius D. Sanders; Rolf Sondergaard; Marc D. Polanka; Walter F. O’Brien; Douglas C. Rabe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There has been a need for improved prediction methods for low pressure turbine (LPT) blades operating at low Reynolds numbers. This is known to occur when LPT blades are subjugated to high ...
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    Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part I: Development of Prediction Methodology 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31011
    Author(s): Darius D. Sanders; Rolf Sondergaard; Marc D. Polanka; Walter F. O’Brien; Douglas C. Rabe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There is an increasing interest in design methods and performance prediction for aircraft engine turbines operating at low Reynolds numbers. In this regime, boundary layer separation may be more ...
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    An Investigation of Reynolds Lapse Rate for Highly Loaded Low Pressure Turbine Airfoils With Forward and Aft Loading 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51035
    Author(s): M. Eric Lyall; Rolf Sondergaard; Mark W. McQuilling; John P. Clark; Paul I. King
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental and computational study of the midspan low Reynolds number loss behavior for two highly loaded low pressure turbine airfoils, designated L2F and L2A, which ...
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