TY - GEN
T1 - On the importance of modeling size and velocity polydispersion of alumina droplets with robust and accurate numerical schemes for the prediction of solid rocket motors instabilities
AU - Dupif, Valentin
AU - Dupays, Joel
AU - Massot, Marc
AU - Laurent, Frederique
PY - 2017/1/1
Y1 - 2017/1/1
N2 - The proposed contribution aims at presenting a robust method of high accuracy to model and simulate the dynamics of moderately inertial polydisperse spray of droplets in industrial configuration. The choice of an Eulerian framework to model the spray is motivated by the efficiency of the related numerical methods to solve two-way coupled effects and their abilities for high performance computing. Aiming at solving moderately high inertia droplets and realistic sprays, the proposed modeling takes into account both local size and velocity dispersions and therefore enables trajectories of droplets of comparable size to cross. In order to provide second order accuracy in every conditions, drag, heat exchange and evaporation are computed simultaneously by a dedicated procedure. Inspired from previous works, this methods is extended to take into account velocity polydispersion, assumed under the form of a anisotropic Gaussian distribution. Thanks to an operator splitting, this method is coupled with an efficient scheme for droplets and gas transport in the physical space already presented by the authors. The efficiency of the method proposed at predicting instabilities is assessed in the field of solid rocket propulsion.
AB - The proposed contribution aims at presenting a robust method of high accuracy to model and simulate the dynamics of moderately inertial polydisperse spray of droplets in industrial configuration. The choice of an Eulerian framework to model the spray is motivated by the efficiency of the related numerical methods to solve two-way coupled effects and their abilities for high performance computing. Aiming at solving moderately high inertia droplets and realistic sprays, the proposed modeling takes into account both local size and velocity dispersions and therefore enables trajectories of droplets of comparable size to cross. In order to provide second order accuracy in every conditions, drag, heat exchange and evaporation are computed simultaneously by a dedicated procedure. Inspired from previous works, this methods is extended to take into account velocity polydispersion, assumed under the form of a anisotropic Gaussian distribution. Thanks to an operator splitting, this method is coupled with an efficient scheme for droplets and gas transport in the physical space already presented by the authors. The efficiency of the method proposed at predicting instabilities is assessed in the field of solid rocket propulsion.
UR - https://www.scopus.com/pages/publications/85086688798
U2 - 10.2514/6.2017-5020
DO - 10.2514/6.2017-5020
M3 - Conference contribution
AN - SCOPUS:85086688798
SN - 9781624105111
T3 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
BT - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
Y2 - 10 July 2017 through 12 July 2017
ER -