All Stories

  1. Numerical Description of the Turbulent Combustion of Methane-oxygen at 20 atm using the ReduceSens Mechanism

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Saulo Alfredo Gómez Salcedo, Dr Amilcar Pimenta

  2. Liquid Rocket Engine - Modeling

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

    Dr Amilcar Pimenta

  3. Injector Design

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

    Dr Amilcar Pimenta

  4. Study of the ablative and microstructural properties of graphite nozzles coated with sic.

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

    Dr Amilcar Pimenta

  5. Dimensioning a Simplex Swirl Injector

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

    Dr Amilcar Pimenta