All Stories

  1. Quadrant-Splitting Analysis of Coherent Motions in the Turbulent Boundary Layer of a NACA0012 at High Angle of Attack

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Leandro Silva

  2. Pressure Gradient Effects on Coherent Structures and Anisotropy of a Turbulent Boundary Layer Over a NACA0012 Airfoil at 12 Deg. Angle of Attack

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    William R Wolf, Leandro Silva

  3. Adverse Pressure Gradient Effects on Extreme Events and Intermittency in the Turbulent Boundary Layer of a NACA0012 at 12 Deg. Angle of Attack

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Ricardo Vinuesa, Leandro Silva