ALESSIO GIZZI; VIVIANA FERRETTI; MICHELE URBANO MARTINI; DANIELE LIUZZI; DANIELE DRIGO

DOI Number: 10.13009/EUCASS2023-040

One of the main needs in modem combustion chamber design technique is to foresee the maximum temperature condition on the components subjected to high thermal stresses. In this frame, a model to investigate on the temperature of the injector dome is proposed and analysed in detail. The model consists of two iterative steps integrating the reacting domain and the cold one. The numerical model is composed of a hot domain, in which reacting CFD simulations are performed in the OpenFOAM environment, and of a cold domain, in which RANS compressible steady-state CFD simulations are performed by Ansys Fluent 2023 Rl ([[5]J[6]).

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In Categories: 1. Aerospace Europe Conference 2023, 1.Events, 10. Propulsion Physics
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