All Stories

  1. Bow Shock/Vortex Interaction: Effect of Reducing the Vortex Height on Structure of the Generated Flow Field

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

    Dr Hamideh Pourhashem

  2. Interaction of Vortex with Bow Shock Wave: Computational Model, Experimental Validation, Enhanced Mixing

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

    Dr Hamideh Pourhashem

  3. Study of Shock Wave/Vortex Interaction for Supersonic Mixing Enhancement

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

    Dr Hamideh Pourhashem

  4. Effect of Downstream Microjet Fluidic Injection on Mixing Characteristics of Supersonic Jet

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

    Dr Hamideh Pourhashem, Dr Iraj M Kalkhoran

  5. Numerical Investigation of Supersonic Jet Noise Suppression via Downstream Microjet Fluidic Injection

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

    Dr Hamideh Pourhashem, Dr Iraj M Kalkhoran