All Stories

  1. Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel

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

    Mr Donald A Durston, Raymond S Castner

  2. Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flow with Shock Interactions

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

    Mr Donald A Durston

  3. Experimental and Computational Sonic Boom Assessment of Boeing N+2 Low Boom Models

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

    Mr Donald A Durston

  4. Computational and Experimental Assessment of Models for the First AIAA Sonic Boom Prediction Workshop

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

    Mr Donald A Durston