Journal of Projectiles, Rockets, Missiles and Guidance

Simulation Analysis of the Internal Flow Characteristics for SRM with Tail-pipe Nozzle

MAO Jiyin, DU Yong, TIAN Yunfeng, GAO Hongwei, LI Jinfu

JPRMG, 2024, 44(4): 46-52. DOI: 10.15892/j.cnki.djzdxb.2024.04.006

Fig.9 Curves of airflow density and temperature on tail-pipe region's axis

Other figure/table from this article

Fig.1 Grid diagram of flow field in SRM with tail-pipe
Fig.2 Grid diagram of flow field in SRM with no tail-pipe
Table 1 Main design parameters of gas
Fig.3 Average pressure simulation curve of combustion chamber
Fig.4 Pressure distribution in tail-pipe SRM at different times
Fig.5 Pressure distribution in no tail-pipe SRM at different times
Table 2 Comparison data of balance thrust
Fig.6 Gasflow velocity distribution in tail-pipe region of equilibrium state
Fig.7 Density distribution of particle flow
Fig.8 Curves of airflow velocity and pressure on tail-pipe region's axis
Fig.10 Distribution of particles inside the combustion
Fig.11 Distribution of particles with different diameters inside the tail-pipe