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    Numerical Investigation of Stall Flutter 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 197
    Author(s): J. A. Ekaterinaris; M. F. Platzer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Unsteady, separated, high Reynolds number flow over an airfoil undergoing oscillatory motion is investigated numerically. The compressible form of the Reynolds-averaged governing equations is solved ...
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    Numerical Investigation of Airfoil Dynamic Stall in Simultaneous Harmonic Oscillatory and Translatory Motion 

    Source: Journal of Solar Energy Engineering:;1998:;volume( 120 ):;issue: 001:;page 75
    Author(s): J. A. Ekaterinaris; N. N. So̸rensen; F. Rasmussen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Wind turbine blades are subject to complex flow conditions. For operation in yaw and turbulent inflow, the blade sections appear to execute a motion more complex than a harmonic blade oscillation, ...
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    Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 608
    Author(s): H. M. Jang; J. A. Ekaterinaris; M. F. Platzer; T. Cebeci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Two methods are described for calculating pressure distributions and boundary layers on blades subjected to low Reynolds numbers and ramp-type motion. The first is based on an interactive scheme ...
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