Phenomenological reduced-order modeling of subcritical combustion in cryogenic rocket engines: an application to the prediction of high-frequency combustion instabilities

Autor: Guillaume Storck, Sébastien Ducruix, Luc-Henry Dorey, Marie Théron

Publikováno v: AIAA Propulsion and Energy 2020 Forum
AIAA Propulsion and Energy 2020 Forum, Aug 2020, Virtual event, United States. pp.AIAA 2020-3830, ⟨10.2514/6.2020-3830⟩

International audience; The set of equations governing reacting two-phase flows in liquid-propellant rocket engines is simplified and linearized around a steady base flow. In the particular case of a liquid/gas coaxial injector, models for the atomiz

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::030c86890ec2daa2a1e0df576963db9a
https://hal.archives-ouvertes.fr/hal-03177668/document