Abstract
A numerical simulation of the two-phase viscous flow in an axial symmetric solid rocket motor is presented. A Eulerian-Lagrangian approach is employed in the computation to couple the gas-particle flow in the tail-pipe nozzle. The analysis is based on a TVD scheme and time-stepping Runge-Kutta method in conjunction with a Finite Volume Method. Calculated results for both one-and two-phase flows are given. The particle influence on the flow field and the rules of particles with different sizes flowing in the tail-pipe nozzle is studied.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
