All Stories

  1. Experimental and Computational Investigation of Valve Motion in a Resonant Pulse Combustor

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

    Shaye Yungster, Hugh Perkins

  2. Computational Fluid Dynamic Optimization of an Experimental Rotating Detonation Rocket Engine Nozzle

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Shaye Yungster, Hugh Perkins

  3. RDE Nozzle Computational Design Methodology Development and Application

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

    Shaye Yungster, Hugh Perkins

  4. Computational Study of Compact Ejector-Enhanced Resonant Pulse Combustors

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

    Shaye Yungster

  5. Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure

    Article • Journal of Propulsion and Power, January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Hugh Perkins, Shaye Yungster

  6. Numerical Evaluation of an Ejector-Enhanced Resonant Pulse Combustor with a Poppet Inlet Valve and a Converging Exhaust Nozzle

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

    Hugh Perkins, Shaye Yungster

  7. Parametric Study of Pulse-Combustor-Driven Ejectors at High-Pressure

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hugh Perkins, Shaye Yungster

  8. Effect of Fuel Injection and Mixing Characteristics on Pulse-Combustor Performance at High-Pressure

    Article • July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hugh Perkins, Shaye Yungster