All Stories

  1. Resolvent Analysis of Shock Buffet on Infinite Wings

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Wei He

  2. Wake Dynamics of Finite Aspect Ratio Wings. Part III: TriGlobal Linear Stability Analysis

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Vassilis Theofilis, Kunihiko Taira, Dr Wei He

  3. Wake Dynamics of Finite Aspect Ratio Wings. Part II: Computational Study

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Vassilis Theofilis, Kunihiko Taira, Dr Wei He

  4. Wake Dynamics of Finite Aspect Ratio Wings. Part I: An Experimental Study

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Kunihiko Taira, Prof Vassilis Theofilis, Dr Wei He

  5. Stability of Low-Reynolds-Number Separated Flow Around an Airfoil Near a Wavy Ground

    Article • AIAA Journal, January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Wei He, Prof Vassilis Theofilis

  6. Ground effects on the stability of separated flow around a NACA 4415 airfoil at low Reynolds numbers

    Article • Aerospace Science and Technology, January 2018, Elsevier

    Dr Wei He

  7. Linear instability of low Reynolds number massively separated flow around three NACA airfoils

    Article • Journal of Fluid Mechanics, December 2016, Cambridge University Press

    Professor Rafael S. Gioria, Dr Wei He

  8. Linear instability in the wake of an elliptic wing

    Article • Theoretical and Computational Fluid Dynamics, July 2016, Springer Science + Business Media

    Dr Wei He

  9. Modal and non-modal global instability analyses of low-Re massively separated flow around a NACA 0015 airfoil

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Professor Rafael S. Gioria, Prof Vassilis Theofilis, Dr Wei He

  10. On Global Linear Instability Mechanisms of Flow Around Airfoils at Low Reynolds Number and High Angle of Attack

    Article • Procedia IUTAM, January 2015, Elsevier

    Professor Rafael S. Gioria, Dr Wei He

  11. Effect of the Trailing Edge Geometry on the Unsteadiness of the Flow Around a Stalled NACA 0015 Airfoil

    Article • January 2015, Springer Science + Business Media

    Dr Wei He