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    Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 189
    Author(s): Ralph J. Volino; Lennart S. Hultgren
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed velocity measurements were made along a flat plate subject to the same dimensionless pressure gradient as the suction side of a modern low-pressure turbine airfoil. Reynolds numbers ...
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    Predictions of Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions Using an Intermittency Transport Equation 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 003:;page 455
    Author(s): Y. B. Suzen; Senior Engineer Associate; Lennart S. Hultgren; Aerospace Engineer; David E. Ashpis; Aerospace Engineer; P. G. Huang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new transport equation for the intermittency factor was proposed to predict separated and transitional boundary layers under low-pressure turbine airfoil conditions. The intermittent behavior of ...
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