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  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. 2-D Air-Breathing Lightcraft Engine Experiments in Hypersonic Conditions

    Article • January 2011, American Institute of Physics

    Marco Antonio Sala Minucci

  3. Experimental Analysis of a 2-D Lightcraft in Static and Hypersonic Conditions

    Article • January 2010, American Institute of Physics

    Marco Antonio Sala Minucci