61–80 of 179 hits
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    Plasma-Based Control of Transition on a Wing with Leading-Edge Excrescence

    Rizzetta, Donald P. / Visbal, Miguel R. | AIAA | 2015

    Dynamic Stall of a Finite-Aspect-Ratio Wing

    Visbal, Miguel R. / Garmann, Daniel J. | AIAA | 2018

    AIAA-2019-3334: Comparison of Pitch versus Plunge Maneuvers of a Finite Wing

    Visbal, Miguel R. / Garmann, Daniel J. | British Library Conference Proceedings | 2019

    High-Fidelity Simulations of Afterbody Vortex Flows

    Garmann, Daniel J. / Visbal, Miguel R. | AIAA | 2019

    Effect of Sweep on Dynamic Stall of a Pitching Finite-Aspect-Ratio Wing

    Visbal, Miguel R. / Garmann, Daniel J. | AIAA | 2019

    Further Investigations of Vortical Gust/Airfoil Interactions at a Transitional Reynolds Number (AIAA 2018-0823)

    Barnes, Caleb J. / Visbal, Miguel R. | British Library Conference Proceedings | 2018

    Mitigation of Laminar Separation Flutter Using Plasma-Based Actuators

    Barnes, Caleb J. / Visbal, Miguel R. | AIAA | 2018

    Understanding Abrupt Leading Edge Separation as a Mechanism for the Onset of Dynamic Stall (AIAA 2018-0356)

    Benton, Stuart I. / Visbal, Miguel R. | British Library Conference Proceedings | 2018

    Effects of Leading-Edge Geometry on the Onset of Dynamic Stall

    Benton, Stuart I. / Visbal, Miguel R. | AIAA | 2018

    Computational Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing (AIAA 2018-0357)

    Visbal, Miguel R. / Garmann, Daniel J. | British Library Conference Proceedings | 2018