All Stories

  1. Phenomenological Reduced-order Modeling of Sub-critical Combustion in Cryogenic Rocket Engines: an Application to the Prediction of High-frequency Combustion Instabilities

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

    Dr Sebastien Ducruix, Marie THERON

  2. Reduced Order Modeling Approach to Combustion Instabilities of Liquid Rocket Engines

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

    Dr Sebastien Ducruix

  3. A 2D-axisymmetric analytical model for the estimation of indirect combustion noise in nozzle flows

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

    Dr Sebastien Ducruix, Alexis Giauque