All Stories

  1. Comparison of Hypermixer Geometries in an Axisymmetric Supersonic Combustion Flowpath

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Kyungrae Kang, Arthur Paganini, Chol-Bum "Mike" Kweon

  2. Optical Diagnostics of Cavity-Stabilized Combustion in an Axisymmetric Dual-Mode Supersonic Combustion Flowpath

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

    Arthur Paganini

  3. Numerical Simulation of Oxygen-Enhanced Combustion in an Arc-Heated Direct Connect Scramjet Facility

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

    Arthur Paganini

  4. Numerical and Experimental Investigation of a Mach 7 Reactive Flowpath

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

    Arthur Paganini, Clara Helm

  5. Development of an Optically Accessible Mach 3.5 Axisymmetric Direct Connect/Semi-Free Jet Supersonic Combustion Flowpath

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

    Arthur Paganini

  6. Flow visualization in a streamline-traced supersonic inlet

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

    Chol-Bum "Mike" Kweon, Arthur Paganini

  7. Transient Cavity Ignition And Periodic Flame Stabilization Modes In Rectangular Supersonic Flowpath

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

    Arthur Paganini