In this work a Q1D multiphase model is presented and validated for thermoacoustic instability within solid rocket motors. The mathematical and physical approaches are derived starting from Eulerian-Eulerian multidimensional model, exploiting physical insights obtained via 2D numerical simulations to improve the Q1D modeling. In order to validate such methodology, numerical simulations have been performed on a simplified geometry known in literature to be prone to develop pressure fluctuations due multiphase effects. The presented solutions are fully in agreement with literature data concerning the thermoacoustic origin of the unstable behavior and the pressure oscillations amplitude. Such result ensures the model validation, which is the preliminary and obligatory step of a work-in-progress project aimed to provide a light but powerful tool to investigate pressure oscillations within solid rocket motors.
Thermoacoustics Q1D Modeling in Solid Rocket Motors / Grossi, Marco; Bianchi, Daniele; Favini, Bernardo. - (2021). (Intervento presentato al convegno AIAA Propulsion and Energy 2021 Forum tenutosi a Virtual Event) [10.2514/6.2021-3702].
Thermoacoustics Q1D Modeling in Solid Rocket Motors
Grossi, Marco
;Bianchi, Daniele;Favini, Bernardo
2021
Abstract
In this work a Q1D multiphase model is presented and validated for thermoacoustic instability within solid rocket motors. The mathematical and physical approaches are derived starting from Eulerian-Eulerian multidimensional model, exploiting physical insights obtained via 2D numerical simulations to improve the Q1D modeling. In order to validate such methodology, numerical simulations have been performed on a simplified geometry known in literature to be prone to develop pressure fluctuations due multiphase effects. The presented solutions are fully in agreement with literature data concerning the thermoacoustic origin of the unstable behavior and the pressure oscillations amplitude. Such result ensures the model validation, which is the preliminary and obligatory step of a work-in-progress project aimed to provide a light but powerful tool to investigate pressure oscillations within solid rocket motors.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.