141–160 of 179 hits
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    Dynamic Stall of a Swept Finite Wing for a Range of Reduced Frequencies

    Rockwood, Matthew / Medina, Albert / Garmann, Daniel J. et al. | AIAA | 2019

    Unsteady vortex structure over a delta wing

    Gordnier, Raymond E. / Visbal, Miguel R. | AIAA | 1994

    Parametric Study of Supersonic Flow Over a Wall-Mounted Hemisphere (AIAA 2018-1786)

    Morgan, Philip E. / Sherer, Scott E. / Visbal, Miguel R. | British Library Conference Proceedings | 2018

    High-Order Spectral Difference: Verification and Acceleration using GPU Computing

    Zimmerman, Ben J. / Wang, Zhi J. / Visbal, Miguel R. | AIAA | 2013

    An Overset-Mesh Approach for Wall-Modeled LES of High-Reynolds Number Airfoil Flow (AIAA 2018-0372)

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

    A Study of the Impact of Wide-Range Roughness Elements on Gortler Instabilities

    Sescu, Adrian / Pendyala, Ravi / Haywood, John et al. | AIAA | 2015

    Computational Study of Supersonic Flow Past Wall-Mounted Cylindrical Bodies (AIAA 2017-1433)

    Morgan, Philip E. / Sherer, Scott E. / Visbal, Miguel R. | British Library Conference Proceedings | 2017

    Large Eddy Simulations of Wall-Mounted Cylinder in Supersonic Flow Using OVERFLOW (AIAA 2017-0309)

    Sherer, Scott E. / Morgan, Philip E. / Visbal, Miguel R. | British Library Conference Proceedings | 2017

    Pitch-plunge Equivalence in Dynamic Stall of Ramp Motion Airfoils

    Miotto, Renato F. / Wolf, William / Gaitonde, Datta et al. | AIAA | 2021

      PITCH-PLUNGE EQUIVALENCE IN DYNAMIC STALL OF RAMP MOTION AIRFOILS

      Miotto, Renato F. / Wolf, William / Gaitonde, Datta et al. | TIBKAT | 2021

    Model Reduction and Analysis of Deep Dynamic Stall on a Plunging Airfoil using Dynamic Mode Decomposition (AIAA 2015-1058)

    Mohan, Arvind T. / Visbal, Miguel R. / Gaitonde, Datta V. | British Library Conference Proceedings | 2015

    High-Fidelity Simulations of a Flexible Heaving Finite-Aspect-Ratio Wing

    Barnes, Caleb J. / Visbal, Miguel R. / Gordnier, Raymond E. | AIAA | 2013

    A Study of the Impact of Wide-Range Roughness Elements on Gortler Instabilities (AIAA 2015-0275)

    Sescu, Adrian / Sassanis, Vasileios / Haywood, John et al. | British Library Conference Proceedings | 2015

    Origin of computed unsteadiness in the shear layer of delta wings

    Visbal, Miguel R. / Gordnier, Raymond E. | AIAA | 1995

    AIAA-2019-3335: Dynamic Stall of a Swept Finite Wing for a Range of Reduced Frequencies

    Rockwood, Matthew / Medina, Albert / Garmann, Daniel J. et al. | British Library Conference Proceedings | 2019

    Effect of Bending-Oscillations on a Streamwise-Oriented Vortex Interaction (AIAA 2015-3303)

    Barnes, Caleb J. / Visbal, Miguel R. / Huang, George P. | British Library Conference Proceedings | 2015

    Crossflow topology of vortical flows

    Visbal, Miguel R. / Gordnier, Raymond E. | AIAA | 1994

    Pitch rate and pitch-axis location effects on vortex breakdown onset

    Visbal, Miguel R. / Gordnier, Raymond E. | AIAA | 1995

    Large-eddy simulation of separation control for flow over a wall-mounted hump

    Morgan, Philip E. / Rizzetta, Donald P. / Visbal, Miguel R. | Tema Archive | 2007

    Computational and Experimental Investigation of a Nonslender Delta Wing

    Gordnier, Raymond E. / Visbal, Miguel R. / Gursul, Ismet et al. | AIAA | 2009