This paper has the aim to investigate the correlation between some ballistic geometrical parameters of a SRM and the calibration of AGAR Q1D model of the pressure oscillations. The correlation permits to share the same model calibration between SRMs of different scales prone to pressure during their steady state, improving the prediction capability of the model. The numerical reconstructions performed on two aft-finocyl SRMs, P80 the first stage of the European launch vehicle VEGA, and POD-Y the mid- scale demonstrator for the pressure oscillations of the possible future evolutions of P80 SRM, confirm the effectiveness of this approach and the goodness of the AGAR model, both numerical results being in very good agreement with experimental data.

Vortex-sound modelling in aft-finocyl solid rocket motors / Rossi, G.; Laureti, M.; Favini, B.; Cavallini, E.; Neri, A.. - ELETTRONICO. - (2017). (Intervento presentato al convegno 7 TH European conference for aeronautics and aerospace sciences (eucass) tenutosi a Milano nel 3-6 luglio 2017) [10.13009/EUCASS2017-432].

Vortex-sound modelling in aft-finocyl solid rocket motors

G. Rossi;M. Laureti;B. Favini;E. Cavallini;
2017

Abstract

This paper has the aim to investigate the correlation between some ballistic geometrical parameters of a SRM and the calibration of AGAR Q1D model of the pressure oscillations. The correlation permits to share the same model calibration between SRMs of different scales prone to pressure during their steady state, improving the prediction capability of the model. The numerical reconstructions performed on two aft-finocyl SRMs, P80 the first stage of the European launch vehicle VEGA, and POD-Y the mid- scale demonstrator for the pressure oscillations of the possible future evolutions of P80 SRM, confirm the effectiveness of this approach and the goodness of the AGAR model, both numerical results being in very good agreement with experimental data.
2017
7 TH European conference for aeronautics and aerospace sciences (eucass)
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Vortex-sound modelling in aft-finocyl solid rocket motors / Rossi, G.; Laureti, M.; Favini, B.; Cavallini, E.; Neri, A.. - ELETTRONICO. - (2017). (Intervento presentato al convegno 7 TH European conference for aeronautics and aerospace sciences (eucass) tenutosi a Milano nel 3-6 luglio 2017) [10.13009/EUCASS2017-432].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1017966
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