All Stories

  1. An Evaluation of Actuator Line Method for Aeracoustic Applications

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Ardeshir Hanifi, Dr. André V. G. Cavalieri

  2. Very-low-dissipation, physics-based, and parameter-free shock capturing for discontinuous Galerkin methods

    Article • Physics of Fluids, December 2024, American Institute of Physics

    Ardeshir Hanifi, Dr. Mihai Mihaescu, Francesco Mario D'Afiero

  3. Direct numerical simulation of transition under free-stream turbulence and the influence of large integral length scales

    Article • Physics of Fluids, July 2024, American Institute of Physics

    Ardeshir Hanifi

  4. Wavepackets Driving Trailing Edge Noise. Part II – Resolvent-Based Model

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

    Dr. André V. G. Cavalieri, Ardeshir Hanifi, Dr Kilian Oberleithner

  5. Wavepackets Driving Trailing Edge Noise. Part I – Direct Simulation and Experiments

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

    Dr Kilian Oberleithner, Dr. André V. G. Cavalieri, Ardeshir Hanifi

  6. Direct Numerical Simulations of Bypass Transition over Distributed Roughness

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

    Ardeshir Hanifi

  7. 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

  8. 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

  9. 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

  10. Control of Instabilities in an Unswept Wing Boundary Layer

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

    Ardeshir Hanifi

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

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

    Ardeshir Hanifi

  12. 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