All Stories

  1. Experimental Flowpath Characterization of the T2 Shock Tunnel Mach 7.0 Hybrid Axisymmetric Contour Nozzle

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

    Lucas Galembeck, Marco Antonio Sala Minucci

  2. Combustion energy for hypersonic facilities

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

    Lucas Galembeck, Vilma Mauro, Ivo Alves, Israel Rego