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  1. Effect of the Contour Shock on Restricted Shock Separation in Rocket Nozzles

    Article • Journal of Propulsion and Power, March 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Kyll Schomberg

  2. Suppressing Restricted Shock Separation in a Subscale Rocket Nozzle Using Contour Geometry

    Article • Journal of Propulsion and Power, September 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Kyll Schomberg

  3. Design of High-Area-Ratio Nozzle Contours Using Circular Arcs

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

    Kyll Schomberg

  4. Safer rocket nozzle design

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

    Kyll Schomberg

  5. Design of High Area Nozzle Contours Using Circular Arcs

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

    Kyll Schomberg

  6. Geometric Analysis of the Linear Expansion-Deflection Nozzle at Highly Overexpanded Flow Conditions

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

    Kyll Schomberg