Julien LABAUNE, Ancelin ROCAMORA, Aymeric BOURLET, Christophe LAUX, Fabien THOLIN

DOI Number: N/A

Conference number: HiSST-2025-027

The primary objective of this study is to establish a numerical strategy for simulating a supersonic combustion chamber where plasma is utilized to ignite combustion. Following a description of the methodology based on the quasi-neutrality hypothesis for simulating the plasma, simulations are conducted in non-reactive and reactive conditions. Qualitative comparisons are made with an experiment for non-reactive case. A second simulation aims to predict outcomes for future experimental investigations.

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In Categories: 1.Events, 1.HiSST 2025, Propulsion Systems & Components
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