All Stories

  1. CFD Optimization of Ejector Flaps in a One-Sided Mixer Ejector Nozzle

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

    Raymond S Castner

  2. Supersonic Inlet Test for a Quiet Supersonic Transport Technology Demonstrator in the NASA Glenn 8-foot by 6-foot Supersonic Wind Tunnel

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

    Raymond S Castner

  3. Lessons Learned from Applying Design Thinking in a NASA Rapid Design Study in Aeronautics

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

    Raymond S Castner

  4. 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

  5. Wedge Shock and Nozzle Exhaust Plume Interaction in a Supersonic Jet Flow

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

    Raymond S Castner

  6. Computational and Experimental Study of Supersonic Nozzle Flow and Aft-Deck Interactions

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

    Dr. Sudheer N Nayani, Raymond S Castner

  7. Cart3D Analysis of Plume and Shock Interaction Effects on Sonic Boom

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

    Raymond S Castner

  8. Computational and Experimental Study of Supersonic Nozzle Flow and Shock Interactions

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

    Dr. Sudheer N Nayani, Raymond S Castner

  9. Airframe-Nozzle-Plume Interactions in the Context of Low Sonic Boom Design

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

    Raymond S Castner

  10. Plume and Shock Interaction Effects on Sonic Boom in the 1-foot by 1-foot Supersonic Wind Tunnel

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

    Raymond S Castner

  11. Wedge Shock and Nozzle Exhaust Plume Interaction in a Supersonic Jet Flow

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

    Raymond S Castner