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    Principles of Aeroelasticity 

    Source: Journal of Applied Mechanics:;1963:;volume( 030 ):;issue: 001:;page 160
    Author(s): R. L. Bisplinghoff; Martin Goland; H. Ashley
    Publisher: The American Society of Mechanical Engineers (ASME)
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    On the Calculation of Unsteady Nonlinear Three-Dimensional Supersonic Flow Past Wings 

    Source: Journal of Fluids Engineering:;1968:;volume( 090 ):;issue: 004:;page 581
    Author(s): J. J. Kacprzynski; R. Sankaranarayanan; H. Ashley
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive study is made of factors influencing the accuracy of predicted thickness effects on the flow due to oscillatory motion of a sweptback wing in supersonic flight. For a delta ...
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    Considerations of Gravity Effects on VAWT Rotor Configurations Which Minimize Flatwise Moments and Stresses 

    Source: Journal of Solar Energy Engineering:;1993:;volume( 115 ):;issue: 003:;page 143
    Author(s): A. J. Eggers; H. Ashley; R. V. Digumarthi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Anticipating that composite materials will permit greater freedom when future VAWT rotor blades are configured, this paper further examines the benefits of adopting true Troposkien shapes for ...
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    Effects of Blade Bending on Aerodynamic Control of Fluctuating Loads on Teetered HAWT Rotors 

    Source: Journal of Solar Energy Engineering:;1996:;volume( 118 ):;issue: 004:;page 239
    Author(s): A. J. Eggers; H. Ashley; S. M. Rock; K. Chaney; R. Digumarthi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Active aerodynamic control, in the form of closed-loop actuation of blade-tip ailerons or all-moveable blades, is investigated as a means of increasing the structural fatigue life of HAWT rotors. ...
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