All Stories

  1. Direct Numerical Simulations of Bypass Transition over Distributed Roughness

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

    Ardeshir Hanifi

  2. Experimental and theoretical study of swept-wing boundary-layer instabilities. Unsteady crossflow instability

    Article • Physics of Fluids, June 2019, American Institute of Physics

    Ardeshir Hanifi

  3. Global Transient-Growth Analysis of Hypersonic Flow on the HIFiRE-5 Elliptic Cone Model

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

    Ardeshir Hanifi, Prof Vassilis Theofilis

  4. Receptivity coefficients of vortex-vibrational type at excitation of 3D Tollmien-Schlichting waves in a boundary layer on a swept wing

    Article • January 2019, American Institute of Physics

    Ardeshir Hanifi

  5. Control of Instabilities in an Unswept Wing Boundary Layer

    Article • AIAA Journal, May 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Ardeshir Hanifi

  6. Control of a swept-wing boundary layer using ring-type plasma actuators

    Article • Journal of Fluid Mechanics, April 2018, Cambridge University Press

    Ardeshir Hanifi

  7. Effect of Upstream Flow Deformation Using Plasma Actuators on Crossflow Transition Induced by Unsteady Vortical Free-Stream Disturbances

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Markus J Kloker, Ardeshir Hanifi