All Stories

  1. Using Discrete and Distributed Roughness to Generate Stationary Crossflow Waves in a Mach 6 Quiet Tunnel

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

    Josh Edelman

  2. Hypersonic Crossflow Instability

    Article • Journal of Spacecraft and Rockets, March 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Josh Edelman

  3. Infrared Thermography data reduction technique for heat transfer measurements in hypersonic flow

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

    Josh Edelman, Mirko Zaccara

  4. Secondary Instabilities of Hypersonic Stationary Crossflow Waves

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

    Josh Edelman

  5. Crossflow Transition on a Pitched Cone at Mach 8

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

    Josh Edelman

  6. Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel on Hypersonic Boundary-Layer Transition

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

    Josh Edelman

  7. Boundary-Layer Transition Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel

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

    Josh Edelman

  8. Instability Measurements in the Boeing/AFOSR Mach-6 Quiet Tunnel

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

    Josh Edelman

  9. Instability and Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel

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

    Josh Edelman